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US3684219A - Glider launcher for kites - Google Patents

Glider launcher for kites
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US3684219A
US3684219AUS99615AUS3684219DAUS3684219AUS 3684219 AUS3684219 AUS 3684219AUS 99615 AUS99615 AUS 99615AUS 3684219D AUS3684219D AUS 3684219DAUS 3684219 AUS3684219 AUS 3684219A
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strut
launching
kite
string
band
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Robert W King
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Abstract

A simple, lightweight, easily constructed and easily operated, spring-loaded glider launching attachment for a kite is disclosed which is formed primarily from flexible plastic tubing, paper clips or the like and rubber bands. Other embodiments are disclosed.

Description

United States Patent King 1 Aug. 15, 1972 [54] GLIDER LAUNCHER FOR KITES [72] Inventor: Robert W. King, 5620 Theobald,
Morton Grove, Ill. 60053 [22] Filed: Dec. 18, 1970 21 Appl. No.: 99,615
[52] US. Cl. ..244/ 155 [51] Int. Cl ..B64c 31/06 [58] Field of Search ..244/l53, 154, 155
[56] References Cited UNITED STATES PATENTS McKay ..244/155 R 2,822,998 2/l958 Toth ..244/l55 R Primary ExaminerRichard A. Schacher Att0rney-Harbaugh and Thomas ABSIRACT A simple, lightweight, easily constructed and easily operated, spring-loaded glider launching attachment for a kite is disclosed which is formed primarily from flexible plastic tubing, paper clips or the like and rubber bands. Other embodiments are disclosed.
9 Claims, 11 Drawing Figures PATENTEnAua 15m2 3 6-84 21 9 SHEET 1 or 2 INVENTOR: ROBERT W KING A frorneys PATENTEDAus 15 m2 3.684.219
saw 2 BF 2 //V VENTOR:
ROBERT 4 Kl/VG By $44M JZMM Attorneys GLIDER LAUNCHER FOR KITES BACKGROUND OF THE INVENTION Release means for kits structures whereby a toy parachute or glider can be attached to the kite frame for release after a predetermined time are known. Early structures used for this purpose were formed of metal and involved ratchets, spring biased triggers and detent balls for release by a control string. Various special means for attaching the fabric portion of the parachute are used. It is known to attach a glider to the main brace of a kite by means of a rubber band affixed to the brace at the top end and engaging a notch in the glider body at the other end. The other end of the glider in one such prior art device, disclosed in US. Pat. No. 2,669,403 is held by a pivotally mounted trigger that catches a second notch in the glider at one end and has a tapering arm extending to the windward side of the kite and engaged by a notched catch member extending from the main brace. In order to actuate the lever a release kite is sent up the control string to strike the tapering arm of the lever and force it from the notched catch. Inflatable means such as a balloon within a frame is also used to hold a parachute or glider upon a kite.
The prior art devices, though generally accomplishing their intended purposes have not been commercially acceptable and have not created an impact on the toy art. One reason may be that the weight and bulk of the latch structures destroys the aerodynamic capabilities of the kite, which in itself is difficult enough for a child to handle. Timed release means have to be manufactured with some degree of accuracy which adds to the expense and such means do not always last too long. A trigger kite that is designed to travel up the control string can catch on knots in the string, or be impeded by the steepness of the inclination of the string. Adjusting screws and the like for spring tensions require a screw driver and are difficult for children to use. The instant invention is conceived with a latch device which overcomes these difficulties.
SUMMARY OF THE INVENTION In accordance with this invention the attachment and adjustment of all parts is through the interengagement of tubular plastic members that can be easily affixed to a standard simple kite. Any part which is lost or broken can be duplicated from plastic tubing, paper clips or a hair pin and no special tools are necessary to adjust or repair the parts. The combination of parts which in one embodiment can be precut for assembly by a child, are adapted for use with any type of kits and are of such a nature that they are not damaged through ordinary accidents that occur with kites, such as being dashed to the ground by a wind gust or sudden calm.
In one embodiment of this invention the toy glider is attached at its front to the end of a rubber band under tension and a part of the rubber band is held on a launching strut, in a simple latch mechanism on one of the kite braces for release by an over-riding tripping string operated by the control string or line for the kite. A bifurcated mount is provided on the brace to releasably hold and longitudinally orient the glider body with the brace. This mount also provides a slide loop for the tripping string that attaches to the latch mechanism. In one form the latch comprises a block attached to the kite brace having a beveled wall to engage a loop of the rubber band. The latch proper is a piece of plastic tubing slidably engaged around the brace with a lip to engage over the loop of the rubber band whereby the tendency of the loop to work its way up the beveled wall cants the latch upon the brace and locks the members together. A pivotal latch is also disclosed having a rounded hub to disengage the rubber band. The trip string is tethered to the control string through a guide loop of plastic tubing and a second rubber band is affixed between the control string and the kite. Pulling the control string sharply, stretches the second rubber band to the point where the trip string is tautened and the slidable latch is released allowing the first rubber band to send the glider off from the kite. In another embodiment the loop of the first rubber band is engaged by a pivotally mounted trigger that engages within the slidable tubular latch attached to the trip string. In another embodiment the trip string is pivotally attached to the control string behind a keeper disc so that in the event the kite twirls in the air the harness will not become tangled. One end of another longer piece of plastic tubing is fitted over the top end of the main strut of the kite.
More particularly, a launching strut of the same size and shape as the strut used in the regular kite frame is used. A pair of simple tubular inter-locking latch members that slidably engage this strut are provided. This strut is mounted to the main strut of the kite frame by means of a short piece of a flexible tubular plastic keeper that encompasses the main strut and into which the launching strut is engaged. A holder for the tail of the glider that also slidably engages this strut to adjust for different lengths of glider bodies is provided. A longer piece of plastic tubing interconnects in a loop between the end of the main strut of the kite frame and the end of the launcher strut. This piece of tubing has holes near the ends and serves as a guide for the release string. A short piece of plastic tubing to hold the hot- 7 tom end of the launching strut along with rubber bands and string complete the assembly. In one modification a simple pivoting trigger mounted within a piece of tubular plastic and an interlocking slidable piece of plastic form the release mechanism. In another modification a paper clip can be used in place of the tail holder.
DESCRIPTION OF THE DRAWINGS:
Several illustrative embodiments of the invention are shown in the drawings in which:
FIG. 1 is a perspective view of the back side of a kite with the glider launcher attached;
FIG. 1A is a perspective view of the kite shown in FIG. 1 with a glider attached thereto;
FIG. 2 is a perspective view of the front side of the kits of this invention to show the harness or bridle arrangement used with all embodiments;
FIG. 3 is a gragmentary view, partially in section, showing the catch means of FIG. 1 ready for release of a glider;
FIG. 4 is a fragmentary cross sectional view of a modification of the base portion of the catch means formed of a section of plastic tubing and a block of wood or the like;
FIG. 5 is a fragmentary view of a launching strut of the kite with a tail holder formed of a paper clip and held thereto by means of a section of plastic tubing;
FIG. 6 is a perspective view of the back side of a kite with another form of trigger release and the tail holder of FIG. 3 thereon holding a glider ready for launching;
FIG. 6A is a fragmentary view of a launching strut of the kite shown in FIG. 6 showing the details of the trigger release and its relationship with the holder with a glider in launching position;
FIG. 6B is a fragmentary perspective view of an alternate form of trigger release for use with the embodiment shown in FIG. 6A;
FIG. 7 is a fragmentary partial cross-sectional view to show the position of the parts in FIG. 6A at the moment of release; and
FIG. 8 is a perspective view of a modified form of launching trigger.
DESCRIPTION OF THE FREE EMBODIMENTS:
Referring to FIGS. 1 and 2 there is shown akite 10 formed in the usual manner with the main orlongitudinal strut 12, thecross strut 14 held together by themetal cleat 16 or other suitable fastening at the midpoint of the cross strut to form the kite frame. Each of theends 18 of these struts is provided with a narrow slot to receive the edge-bracingstring 20 in tautened relationship thereabout, over one side of which thepaper portion 22 of the kite body is placed and held in place by the glued down flaps 24. On the front or windward side of the kite there is provided thestring harness 26 which attaches through thepaper 22 to the main strut at spaced points. Any form of harness can be used, that is, a two-point connection or a four-point connection as desired. The kite string is shown at 28 with which the kite is controlled in its flying position. Thekite 10 is merely illustrative of the type of airborne toy which the launching device of this invention may be used as will be apparent as the description proceeds.
As shown in FIGS. 1, 1A, 2 and 6, themain strut 12 has affixed thereto the elongated and curved section oftubing 30. One end of thetube 30 is press-fitted over the top end of the main strut in which position it engages over thestring 20 and further secures it within the slot of the strut. Thetube 30 has a passageway therethrough and is provided with a pair ofrounded apertures 32 and 34 spaced from the ends of this member. Themain strut 12 is provided with thefastener 36 comprising a short section of the same type of tubing used to fabricate theguide tube 30. A launchingrubber band 38 of elongated continuous loop configuration is provided with the glider engaging end indicated at 40, at which position the shorter andsmaller trigger band 42 is tied by merely looping it over and through itself. I
The launchingstrut 44 is mounted thereon with its bottom end thrust into thefastener tube 36 and its other or top end thrust into the other end of theguide tube 30 with that portion of therubber band 38 opposite the end engaged over the end of the launching strut. Theholes 32 and 34 are spaced sufficiently from the ends of thetube 30 so that when themain strut 12 and the launchingstrut 38 are in the position shown theholes 32 and 34 are open and free of any obstruction. Thetube 30 is normally a straight piece of tubing which is flexed to the mounted position shown.
Referring to FIGS. 1, 1A and 3, it is seen that the launching strut carries, as one embodiment of this invention, theblock member 46 having an aperture 48 (FIG. 5) therethrough that encompasses this strut. Theblock 46 as shown in FIG. 3 is constructed of a solid piece of plastic and has theback surface 50 which is planar and slopes forwardly and upwardly from the top surface of thestrut 44. Theaperture 48 is off center so that thesurface 50 is raised above the strut to facilitate its use as a catch as will be described.
FIG. 4 illustrates an alternate form of block member 46' formed of a short section ofplastic tubing 52 encompassing a short section of wood orother filler material 54, the end surfaces 56 and 58 of which are coplanar and beveled to form the same type of sloping catch surface as illustrated at 50. This type of catch or block is readily formed by the user in the event theplastic block 46 becomes lost or repairs are necessary during use of the kite.
Still referring to FIGS. 1 and 3, the launchingstrut 44 has themovable latch member 60 also formed of a section of plastic tubing, thebore 62 of which is larger than thestrut 44 so that it is not only freely slidable thereon but also cants and locks as will be described. The forward edge of thelatch member 60 has the protrudingtongue 64 formed by thearcuate cut 66 for this end. The back and top edge has an aperture or afastening ring 68 to which is tied one end of thetrip string 70. At the rear or bottom end of the launching strut there is provided thetail clamp 72 having the wire orplastic loop 74 on its forward edge and being provided with a pair of upright spacedfingers 76 and 78. As shown in FIGS. 1, 1A and 2, the trip string is attached to thelatch member 60 on the end opposite thetongue 64 and passes rearwardly through theloop 74 of thetail clamp 72, where it reverses and extends along the side of the launchingstrut 44 to the top end of the kite, through thehole 34, within and around the curve of thetubing 30 and out thehole 32 to the front side of the kite, where it is tied to the mainkite control string 28. Preferably, this end of the trip string is looped over thecontrol string 28 as indicated at 80.
This fastening can be accomplished by means of a non-slipping loop in the trip string or by a metal slip ring which is illustrated at 80. In any event, theend 80 engages the control string in a manner so that it will rotate thereabout and not tangle or wind up if the kite should go into a spin. This fastening also prevents tangling during periods of handling the kite as in transportation, packing or launching. As shown in FIGS. 1 and 2, thecontrol string 28 is affixed to theresilient rubber hand 82 which is affixed at its other end to theharness 26 as at theadjustable tie point 84. In order to prevent theloop 80 from tangling with therubber band 82, it has been found expedient to provide a barrier member. That section of thecontrol string 28 between theloop 80 and therubber band 82 accordingly carries thelightweight washer 86.
Theglider 88 to be launched by the kite of this invention, is illustrated in FIGS. 1A and 6 in the ready-tolaunch position. Any form of glider or flying toy can be used as long as it is provided with anotch 90 or similar off-set in itsfuselage member 92 and has a flattenedtail section 94 that can be retained within thespace 96 between thefingers 76 and 78 of thetail catch 72. This member is formed of molded plastic and the base portion encompasses and slidably engages the launching strut and catch means. These parts are arranged as shown in FIG. I when the glider is attached. Thenotch 90 is engaged in the end of therubber band 38 and the glider is moved rearwardly until thetail section 94 can be pressed between the fingers 76-78. The length of theband 38, the position of thetail catch 72 are adjusted so that with the glider attached as shown in FIG. 4, theband 38 is under sufficient tension to give a launching thrust to the glider on release, that is, just enough to send the glider free of the kite.
Thelatch member 60 is moved backwards on thestrut 44 clear of the sloping surface and the lighterweight trigger band 42 is stretched backwards and looped over and down upon this surface. While the trigger band is held in this position by the fingers it is only necessary to move the latch member forward so that thetongue 64 touches thesurface 50 above theband 42. Theband 42 is then released and because of its tension creeps or rolls upward on thisslope 50 until it engages the underside of thetongue 64 and cants thelatch 60 into the position shown in FIG. 3. The trip string is slack at this time. Thebore 62 of thelatch 60 is accordingly canted upon thestrut 44 and theedges 98 and 100 engage thereupon. This locking movement occurs before the tongue pivots beyond the upper reaches of the slope orcamming surface 50 so as to prevent thetrigger band 42 from releasing.
It is to be observed that, since thetrigger string 70 is slack, the kite can be flown in the usual manner by means of the mainkite control string 28, through the take-upband 82 and the harness orbridle 26. Once in the air and at the desired attitude it is only necessary to jerk thestring 28 which causes a sudden stretch in theband 82, thereby taking up the slack in thetrip string 70 which pulls through thetube 30, around theloop 74 and tautens, to move thelatch 60 rearwardly. Thetongue 64 is moved away from theslope 50 and its engagement with thetrigger band 42, which is immediately released. Themain rubber band 38 is also released, to flip the glider from the kite. The tension on theband 38 is strong enough to overcome the gripping force of thetail holder 72. I
FIG. 5 illustrates an alternative form of tail holder comprising a short section ofplastic tubing 102 which slidably engages and encompasses the launchingstrut 44 just ahead of thebase fastener 36, that is, in the same relative position as thetail holder member 72. In this instance the member to hold thetail section 94 comprises apaper clip 104 having or bent into a U- shapedupper end 106 opening to the front, supported by theshank 108, with one of its loops 110 extending along thestrut 44 and engaged by thetube 102 with theend portion 112 up-turned so as to insure a rigid mounting. This element is readily formed by the user. The tension or spread of thearm 114 of theU-shaped end 106 is readily adjusted to impart the necessary grip on thetail section 94 and the tip 116 can be bent to the side so that there are no sharp edges to catch on the soft light wood i.e., Balsa, of which glider bodies are constructed. The tail holder of FIG. 5 is used in the same manner as that described in relation to thetail holder 72.
FIGS. 6 and 6A show another form of trigger release for the glider launcher of this invention. In this embodiment a piece ofplastic tubing 120 is formed with a rear slopingplanar edge 122 and the tubular portion encompasses thestrut 44 in the same manner as the other tubular plastic pieces that have been described. A short piece of wire, shown in broken lines is retained between thetube 120 and the strut with a loop ortab end 124 extending from the rear and spaced above the top surface of the strut. Thetrigger member 126 has itsforward end 128 looped within the loop ortab 124 so as to be pivotable on a transverse axis.
The tubularslide catch member 130 encompasses thestrut 44 loosely with thespace 132 adapted to receive thetrigger 126 therein and with thetrigger band 42 caught under the pivot 124-128. The rear end of theslide catch 130 has theaperture 134 near the edge to form a tie place for thetrip string 70, as indicated at 136. FIG. 7 shows the relative action of these parts as the trip string is suddenly tautened, by a jerk on thecontrol string 28, in the direction of thearrow 140, pulling theslide 130 in the direction of thearrow 142, whereby it clears the end of thetrigger 126, which allows thetrigger 126 to pivot and free thetrigger band 42 as the glider is launched. Theband 42 rolls upwardly on theslope 122 and easily passes over the hinge 124-128.
In FIG. 8 a modified trigger base 120' is shown wherein the loop hings 128 is recessed back from theedge 122 by means of theslot 144 and the hole 146 forming a cross-wall section for the loop hinge. The function of the modified trigger base 120' is the same as that shown in FIGS. 6A and 7.
In FIG. 68 still another version of the trigger is shown wherein theflat base member 150 rests upon thestrut 44 and is held by means of the overlapping front and rear tubularplastic sections 152 which can be identical. The paid oftabs 154 extend from the base in spaced relationship and carry thepin 156 therebetween on which is mounted theplastic hub 158 having as a part thereof the plastic finger or spoke 160. Thetabs 154 present aslope 162 on the back and front sides so that the trigger can be mounted end-for-end. Theslopes 162 cooperate with theslide catch member 130 and function the same as theslopes 50 and 56-58 in holding and releasing thetrigger band 42 in the manner shown in FIGS. 6A and 7.
All of the parts are adjustable. The length of thetube 30 can be such that a relatively sharp bend is provided at the top end of the kite. This member also functions as a resilient bumper for the kite should it strike a tree or plungs to the ground. Thetube 30 is sized so as to be easily inserted over the struts l2 and 44 with little effort. All of the parts are of lightweight so as to not interfere with the flight characteristics of the kite. The tubular parts are made of any suitable plastic such as polypropylene, nylon or the proprietary product known as Mylar, etc., preferably having strength, pliability and some degree of lubricity. The tail holder and latches can be readily moved along the launchingstrut 44 to accommodate different sizes of gliders and provide varying degrees of tension for the launching and trigger mechanism. The length and other adjustments of thetrigger string 42 are readily made. The kite can be flown from a staked out position from themain string 28 and an auxiliary string (not shown) attached to the kite and extending to the tround so as to bring it down from time to time for repeated glider launchings. The launchingstrut 44 can be mounted along thecross strut 14 if desired for a transverse launch.
It is also apparent from this description that a number of modifications can be made within the scope and intent of the invention. Thus, thelatch 60 can be made to function in different ways or reversed. Thetongue 64 can ride higher on theslope 50 and a protuberance provided on the top of thetongue 64 on which to hook thetrigger band 42, instead of on theslope 50. Thus, the backward or downward movement of thelatch 60 would release the tongue from theblock 48 and allow the latch and the protuberance to pivot downward and release the trigger band. As illustrated the trigger ortrip string 70 reverses in theloop 74 so that it pulls downwardly or toward the tail of the kite in releasing the trigger. This loop can be omitted by reversing the positions of the trigger arrangement shown in FIG. 6A so that theslide 130 is pulled forward or upwardly to release.
In describing the parts of the kite and launching mechanism of this invention it is assumed that under flight conditions theguide loop 30 will be above the tail end or mount 36 and these parts are referred to as the top end and tail end of the kite, respectively. The launchingstrut 44 can be the same material i.e., wood or plastic, as the kite frame struts 12 and 14, and one such strut can be used as the launching strut. It is apparent that the launching strut is mounted at an angle with the strut l2 and acts as a guide or ramp to deflect theglider 92 away from the kite. The take-upband 82 can be double or single and like the launchingband 38 is preferably made of rubber. Thetrigger band 42 can be an ordinary rubber band of any desired length or size.
Under normal flying conditions of the kite thetakeup band 82 functions as a shock absorber and is strong enough to resist the pull of the kite and still have sufficient remaining stretch to yield further under a sudden jerk on the control string to take up the slack on thetrigger string 70. A convenient way of adjusting the degree of slack on the trigger string is provided by thewasher member 86 and theloop 80. With a glider or other article to be launched attached to the launching strut and the trigger set, etc., thecontrol string 28 can be pulled to impart tension on theshock absorber band 82. Thewasher 86 is allowed to slide away from theband 82 against theloop 80 and cause a reduction in the slack in thetrigger string 70. A string or stop member is then tied or otherwise affixed to thecontrol string 28 over which the washer cannot pass, so that it will be spaced from the end of theband 82 while thetrigger string 70 is still slack. Adjustment for the proper slack in thetrigger string 70 can also be made at thetie loop 68 or by slight adjustments in position of thetail support 72. For some kites it may be desirable to omit the launchingstrut 44 and use one of the struts of the kite frame for this purpose. In this event, the guide loop and mount 30 would be modified and shortened for at tachi'nent at the side wall on the end of the strut whereby both ends are open and it serves as a tubular guide for thetrigger string 70 to pass over the end of the strut, i.e., thestrut 12. Also, it is practical for some kites to use thetrigger string 70 directly from the conand control assembly.
What is claimed is:
l. A kite capable of carrying and launching an article aloft including:
a kite frame having a frame strut member with a resilient launching band affixed to one end thereof;
trigger means to hold said resilient launching band in a stretched position with said article releasably engaged by said band;
a bridle attached to said kite frame including a resilient take-up band attached to the main control string of said kite; and
a normally slack trip string attached to said control string at one end and to said trigger means at the other end, the resiliency of said take-up band allowing a sudden jerk on said control string to take up the slack in said trip string whereby to release said trigger means.
2. A kite in accordance with claim 1 in which:
said block member includes a pivotally mounted finger adapted to engage said resilient launching member and rotate to a locked position;
a catch member slidably carried by said launching strut and having a bore hole to receive said finger in the locked position; and
said one end of said trip string being attached to said catch member whereby the tautening of said trip string slides said catch member from the latched position.
3. A kite adapted to carry and launch an article from aloft comprising:
frame means including a frame strut member having a top end and a bottom end;
a main kite control string and a bridle string attached to said frame means with a resilient take-up band between said bridle string and said main control string;
mounting means at the top and bottom ends of said frame strut member, including a guide channel at the top end thereof;
a launching strut carried at its end by said mounting means;
a resilient launching band affixed at one end to said launching strut and have a resilient trigger band at the other end;
means on said launching strut to detachably hold a rear portion of the article to be launched;
releasable trigger means mounted on said launching strut and including a slidable member adapted to releasably engage said trigger band;
a trip string attached to said control string and extending through said guide channel to said slidable member whereby a sharp pull on said control string lengthens said take-up band and pulls said trip string to release said trigger means.
4. A kite in accordance withclaim 3 in which:
said trip string is normally slack in the flying position of said kite and the remaining stretch in said takeup band is sufficient to overcome said slack and tauten said trip string sufiiciently to release said trigger.
5. A kite in accordance withclaim 3 in which:
said trigger means comprises a block member affixed to said launching strut and having a sloping surface over which a portion of said resilient launching band engages in stretched relationship;
a catch member encompassing and slidably carried by said launching strut and having a tongue engageable over the engaged portion of said launching band;
said catch member being thereby canted upon said strut in a latched position; and
said one end of said trip string being attached to said catch member whereby the tautening of said trip string slides said catch member from the latched position.
6. A kite adapted to carry a glider aloft and launch same comprising:
a kite frame having an elongated frame strut member extending from the tail end to the top end of said kite;
a launching strut carried by said frame strut and having a plurality of sections of plastic tubing encompassing said launching strut;
one of said tubing sections encompassing said frame strut near the tail end to form a mounting;
another of said tubing sections having a guide loop and spaced fingers adapted to engage the tail portion of a glider;
one of said tubing sections being slidably mounted on said launching strut with a portion of its longitudinal bore hole open to form a trigger catch;
one of said tubing sections having a pivotal trigger member engageable in said trigger catch in a locked position;
still another of said tubing sections being elongated and arched approximately 180 whereby the extended end encompasses said extended top end of said frame strut and supports said launching strut at an angle to said frame strut;
spaced bore holes in the side of said last mentioned tubing section;
a main kite control string affixed to a shock-absorber band and a bridle attached between said band and said kite frame;
a resilient launching band held at one end between said arcuate tubing section and said launching strut and having a glider engaging loop and a trigger engaging loop; and
a trip string engaged at one end by said control string and extending in slack condition through the spaced bore holes of said arcuate tubing section through said guide loop and being affixed at its other end to said trigger means;
whereby a glider is positionable therein with its tail section between said fingers; its frame hooked in said glider engaging loop, with the launching band stretched sufficiently to throw said glider free of said kite and with the trigger engaging loop engaged under said trigger member in the locked position and the remaining stretch of said shockabsorber band is sufficient to overcome the slack condition of said trip string and release said trigger member from said trigger catch.
7. kite in accordance witla claim 6 in which: sal trip string engages sal control string by means of a loop therearound; and
said control string is provided with a washer member between said loop and the end of said shock-absorber band.
8. A kite in accordance with claim 6 in which:
said spaced fingers extending from said one tubing section comprise the open end hook of a wire member including a shank and a base loop encompassed by said tubing section upon said launching strut; and
said base loop is upturned from the surface of said launching strut to form said guide loop for said trip string.
9. A kite in accordance with claim 6 in which:
said pivotal trigger member is pivotally mounted in a wall section of said tubing spaced inwardly from the end of said tubing and said end is formed with a sloping surface.

Claims (9)

3. A kite adapted to carry and launch an article from aloft comprising: frame means including a frame strut member having a top end and a bottom end; a main kite control string and a bridle string attached to said frame means with a resilient take-up band between said bridle string and said main control string; mounting means at the top and bottom ends of said frame strut member, including a guide channel at the top end thereof; a launching strut carried at its end by said mounting means; a resilient launching band affixed at one end to said launching strut and have a resilient trigger band at the other end; means on said launching strut to detachably hold a rear portion of the article to be launched; releasable trigger means mounted on said launching strut and including a slidable member adapted to releasably engage said trigger band; a trip string attached to said control string and extending through said guide channel to said slidable member whereby a sharp pull on said control string lengthens said take-up band and pulls said trip string to release said trigger means.
6. A kite adapted to carry a glider aloft and launch same comprising: a kite frame having an elongated frame strut member extending from the tail end to the top end of said kite; a launching strut carried by said frame strut and having a plurality of sections of plastic tubing encompassing said launching strut; one of said tubing sections encompassing said frame strut near the tail end to form a mounting; another of said tubing sections having a guide loop and spaced fingers adapted to engage the tail portion of a glider; one of said tubing sections being slidably mounted on said launching strut with a portion of its longitudinal bore hole open to form a trigger catch; one of said tubing sections having a pivotal trigger member engageable in said trigger catch in a locked position; still another of said tubing sections being elongated and arched approximately 180* whereby the extended end encompasses said extended top end of said frame strut and supports said launching strut at an angle to said frame strut; spaced bore holes in the side of said last mentioned tubing section; a main kite control string affixed to a shock-absorber band and a bridle attached between said band and said kite frame; a resilient launching band held at one end between said arcuate tubing section and said launching strut and having a glider engaging loop and a trigger engaging loop; and a trip string engaged at one end by said control string and extending in slack condition through the spaced bore holes of said arcuate tubing section through said guide loop and being affixed at its other end to said trigger means; whereby a glider is positionable therein with its tail section between said fingers; its frame hooked in said glider engaging loop, with the launching band stretched sufficiently to throw said glider free of said kite and with the trigger engaging loop engaged under said trigger member in the locked position and the remaining stretch of said shock-absorber band is sufficient to overcome the slack condition of said trip string and release said trigger member from said trigger catch.
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US99615AExpired - LifetimeUS3684219A (en)1970-12-181970-12-18Glider launcher for kites

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Cited By (34)

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USD253602S (en)1977-05-181979-12-04Evans Dewayne LToy glider
US4211761A (en)*1974-08-221980-07-08Tung Shao EProcess for removal of sulfur dioxide from gaseous mixtures
US4324775A (en)*1977-10-031982-04-13Tung Shao EProcess for recovering sulfur by removal of sulfur dioxide from gaseous mixtures
USD302029S (en)1986-05-261989-07-04Yasuaki NinomiyaModel airplane
USD309164S (en)1988-02-291990-07-10Daniel M. AntonucciModel airplane
US5098039A (en)*1986-11-121992-03-24Linden Jr Kenneth MNight kite
US6257525B1 (en)1998-03-232001-07-10Gray Matter Holdings, LlcRemotely controlled aircraft
US6286786B1 (en)1998-03-232001-09-11Gray Matter Holdings, LlcRemotely controlled aircraft
US6435456B1 (en)2000-10-102002-08-20Bert G. ClawsonMechanism for releasing articles from kites
US20040232282A1 (en)*2003-01-172004-11-25Dennis Brian D.Methods and apparatuses for capturing and recovering unmanned aircraft, including a cleat for capturing aircraft on a line
US20050017129A1 (en)*1999-07-232005-01-27Mcdonnell William R.Launch and recovery system for unmanned aerial vehicles
US20050093507A1 (en)*2003-11-032005-05-05Sliwa Steven M.Methods and systems for starting propeller-driven devices
US20050133665A1 (en)*2003-01-172005-06-23Dennis Brian D.Methods and apparatuses for capturing unmanned aircraft and constraining motion of the captured aircraft
US20050151009A1 (en)*2003-01-172005-07-14Cory RoeselerMethods and apparatuses for launching unmanned aircraft, including methods and apparatuses for launching aircraft with a wedge action
US20050151014A1 (en)*2003-01-172005-07-14Mcgeer Brian T.Methods and apparatuses for launching, capturing, and storing unmanned aircraft, including a container having a guide structure for aircraft components
US20050178895A1 (en)*2003-01-172005-08-18Mcgeer Brian T.Methods and apparatuses for launching unmanned aircraft, including releasably gripping aircraft during launch and braking subsequent grip motion
US20050178894A1 (en)*2003-01-172005-08-18Mcgeer Brian T.Methods and apparatuses for launching unmanned aircraft, including methods and apparatuses for releasably gripping aircraft during launch
US20050230536A1 (en)*2003-01-172005-10-20Dennis Brian DMethods and apparatuses for capturing and storing unmanned aircraft, including methods and apparatuses for securing the aircraft after capture
US20060038067A1 (en)*2003-01-172006-02-23Dennis Brian DMethods and apparatuses for launching and capturing unmanned aircraft, including a combined launch and recovery system
US20060102783A1 (en)*2003-01-172006-05-18Dennis Brian DMethods and apparatuses for capturing and recovering unmanned aircraft, including extendable capture devices
US20060151667A1 (en)*2003-01-172006-07-13Dennis Brian DMethods and apparatuses for launching unmanned aircraft, including methods and apparatuses for transmitting forces to the aircraft during launch
US7143974B2 (en)2003-04-012006-12-05The Insitu Group, Inc.Methods and apparatuses for launching airborne devices along flexible elongated members
US20090189016A1 (en)*2008-01-252009-07-30Insitu, Inc.Systems and methods for recovering and controlling post-recovery motion of unmanned aircraft
US7806366B2 (en)2007-07-102010-10-05Insitu, Inc.Systems and methods for capturing and controlling post-recovery motion of unmanned aircraft
US8944373B2 (en)2010-09-272015-02-03Insitu, Inc.Line capture devices for unmanned aircraft, and associated systems and methods
US9266610B2 (en)2011-11-152016-02-23Insitu, Inc.Controlled range and payload for unmanned vehicles, and associated systems and methods
US9896222B2 (en)2014-11-202018-02-20Insitu, Inc.Capture devices for unmanned aerial vehicles, including track-borne capture lines, and associated systems and methods
US9944408B2 (en)2009-04-242018-04-17Insitu, Inc.Systems and methods for recovering and controlling post-recovery motion of unmanned aircraft
US10399674B2 (en)2014-07-282019-09-03Insitu, Inc.Systems and methods countering an unmanned air vehicle
US10407181B2 (en)2016-06-272019-09-10Insitu, Inc.Locking line capture devices for unmanned aircraft, and associated systems and methods
US10767682B2 (en)2017-06-292020-09-08Insitu, Inc.Frangible fasteners with flexible connectors for unmanned aircraft, and associated systems and methods
US10933997B2 (en)2015-10-022021-03-02Insitu, Inc.Aerial launch and/or recovery for unmanned aircraft, and associated systems and methods
US11066185B2 (en)2018-05-042021-07-20Insitu, Inc.Launch and/or recovery for unmanned aircraft and/or other payloads, including via parachute-assist, and associated systems and methods
US11142339B2 (en)2018-05-042021-10-12Insitu, Inc.Launch and/or recovery for unmanned aircraft and/or other payloads, including via parachute-assist, and associated systems and methods

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US2669403A (en)*1952-07-211954-02-16Doris A MckayGlider carrying and releasing device for kites
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US2822998A (en)*1954-01-221958-02-11Lambert J TothParachute-kite attachment

Cited By (73)

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US4211761A (en)*1974-08-221980-07-08Tung Shao EProcess for removal of sulfur dioxide from gaseous mixtures
USD253602S (en)1977-05-181979-12-04Evans Dewayne LToy glider
US4324775A (en)*1977-10-031982-04-13Tung Shao EProcess for recovering sulfur by removal of sulfur dioxide from gaseous mixtures
USD302029S (en)1986-05-261989-07-04Yasuaki NinomiyaModel airplane
US5098039A (en)*1986-11-121992-03-24Linden Jr Kenneth MNight kite
USD309164S (en)1988-02-291990-07-10Daniel M. AntonucciModel airplane
US6257525B1 (en)1998-03-232001-07-10Gray Matter Holdings, LlcRemotely controlled aircraft
US6286786B1 (en)1998-03-232001-09-11Gray Matter Holdings, LlcRemotely controlled aircraft
US20050017129A1 (en)*1999-07-232005-01-27Mcdonnell William R.Launch and recovery system for unmanned aerial vehicles
US9669946B2 (en)1999-07-232017-06-06Advanced Aerospace Technologies, Inc.Launch and recovery system for unmanned aerial vehicles
US7097137B2 (en)1999-07-232006-08-29Advanced Aerospace Technologies, Inc.Launch and recovery system for unmanned aerial vehicles
US6874729B1 (en)*1999-07-232005-04-05Advanced Aerospace Technologies, Inc.Launch and recovery system for unmanned aerial vehicles
US8864069B2 (en)1999-07-232014-10-21Advanced Aerospace Technologies, Inc.Launch and recovery system for unmanned aerial vehicles
US8567718B1 (en)1999-07-232013-10-29Advanced Aerospace Technologies, Inc.Launch and recovery system for unmanned aerial vehicles
US8517306B2 (en)1999-07-232013-08-27Advanced Aerospace Technologies, Inc.Launch and recovery system for unmanned aerial vehicles
US8167242B2 (en)1999-07-232012-05-01Advanced Aerospace Technologies, Inc.Launch and recovery system for unmanned aerial vehicles
US20110127378A1 (en)*1999-07-232011-06-02Advanced Aerospace Technologies, Inc.Launch and recovery system for unmanned aerial vehicles
US20110011974A1 (en)*1999-07-232011-01-20Advanced Aerospace Technologies, Inc.Launch and recovery system for unmanned aerial vehicles
US20070108345A1 (en)*1999-07-232007-05-17Mcdonnell William RLaunch and recovery system for unmanned aerial vehicles
US6435456B1 (en)2000-10-102002-08-20Bert G. ClawsonMechanism for releasing articles from kites
US7175135B2 (en)2003-01-172007-02-13The Insitu Group, Inc.Methods and apparatuses for capturing unmanned aircraft and constraining motion of the captured aircraft
US20050151009A1 (en)*2003-01-172005-07-14Cory RoeselerMethods and apparatuses for launching unmanned aircraft, including methods and apparatuses for launching aircraft with a wedge action
US7066430B2 (en)2003-01-172006-06-27The Insitu Group, Inc.Methods and apparatuses for capturing and recovering unmanned aircraft, including extendable capture devices
US20060151667A1 (en)*2003-01-172006-07-13Dennis Brian DMethods and apparatuses for launching unmanned aircraft, including methods and apparatuses for transmitting forces to the aircraft during launch
US20060175463A1 (en)*2003-01-172006-08-10The Insitu Group, Inc.Methods and apparatuses for launching, capturing, and storing unmanned aircraft, including a container having a guide structure for aircraft components
US7090166B2 (en)2003-01-172006-08-15The Insitu Group, Inc.Methods and apparatuses for launching unmanned aircraft, including methods and apparatuses for transmitting forces to the aircraft during launch
US20060102783A1 (en)*2003-01-172006-05-18Dennis Brian DMethods and apparatuses for capturing and recovering unmanned aircraft, including extendable capture devices
US7104495B2 (en)2003-01-172006-09-12The Insitu Group, Inc.Methods and apparatuses for launching, capturing, and storing unmanned aircraft, including a container having a guide structure for aircraft components
US7114680B2 (en)2003-01-172006-10-03The Insitu Group, Inc.Methods and apparatuses for launching and capturing unmanned aircraft, including a combined launch and recovery system
US7121507B2 (en)2003-01-172006-10-17The Insitu Group, Inc.Methods and apparatuses for capturing and storing unmanned aircraft, including methods and apparatuses for securing the aircraft after capture
US7128294B2 (en)2003-01-172006-10-31The Insitu Group, Inc.Methods and apparatuses for launching unmanned aircraft, including methods and apparatuses for launching aircraft with a wedge action
US7140575B2 (en)2003-01-172006-11-28The Insitu Group, Inc.Methods and apparatuses for launching unmanned aircraft, including methods and apparatuses for releasably gripping aircraft during launch
US20040232282A1 (en)*2003-01-172004-11-25Dennis Brian D.Methods and apparatuses for capturing and recovering unmanned aircraft, including a cleat for capturing aircraft on a line
US7152827B2 (en)2003-01-172006-12-26The Insitu Group, Inc.Methods and apparatuses for launching, capturing, and storing unmanned aircraft, including a container having a guide structure for aircraft components
US7165745B2 (en)2003-01-172007-01-23The Insitu Group, Inc.Methods and apparatuses for launching unmanned aircraft, including releasably gripping aircraft during launch and braking subsequent grip motion
US20060038067A1 (en)*2003-01-172006-02-23Dennis Brian DMethods and apparatuses for launching and capturing unmanned aircraft, including a combined launch and recovery system
US20050133665A1 (en)*2003-01-172005-06-23Dennis Brian D.Methods and apparatuses for capturing unmanned aircraft and constraining motion of the captured aircraft
US20050230536A1 (en)*2003-01-172005-10-20Dennis Brian DMethods and apparatuses for capturing and storing unmanned aircraft, including methods and apparatuses for securing the aircraft after capture
US20070252034A1 (en)*2003-01-172007-11-01The Insitu Group, Inc.Methods and apparatuses for launching unmanned aircraft, including releasably gripping aircraft during launch and braking subsequent grip motion
US7360741B2 (en)2003-01-172008-04-22Insitu, Inc.Methods and apparatuses for launching unmanned aircraft, including releasably gripping aircraft during launch and breaking subsequent grip motion
US7059564B2 (en)2003-01-172006-06-13The Insitu Group, Inc.Methods and apparatuses for capturing and recovering unmanned aircraft, including a cleat for capturing aircraft on a line
US7712702B2 (en)2003-01-172010-05-11Insitu, Inc.Methods and apparatuses for launching unmanned aircraft, including releasably gripping aircraft during launch and breaking subsequent grip motion
US20050151014A1 (en)*2003-01-172005-07-14Mcgeer Brian T.Methods and apparatuses for launching, capturing, and storing unmanned aircraft, including a container having a guide structure for aircraft components
US20050178895A1 (en)*2003-01-172005-08-18Mcgeer Brian T.Methods and apparatuses for launching unmanned aircraft, including releasably gripping aircraft during launch and braking subsequent grip motion
US20050178894A1 (en)*2003-01-172005-08-18Mcgeer Brian T.Methods and apparatuses for launching unmanned aircraft, including methods and apparatuses for releasably gripping aircraft during launch
US7143974B2 (en)2003-04-012006-12-05The Insitu Group, Inc.Methods and apparatuses for launching airborne devices along flexible elongated members
US7182290B2 (en)2003-11-032007-02-27The Insitu Group, Inc.Methods and systems for starting propeller-driven devices
US20050093507A1 (en)*2003-11-032005-05-05Sliwa Steven M.Methods and systems for starting propeller-driven devices
US7806366B2 (en)2007-07-102010-10-05Insitu, Inc.Systems and methods for capturing and controlling post-recovery motion of unmanned aircraft
US7798445B2 (en)2008-01-252010-09-21Insitu, Inc.Systems and methods for recovering and controlling post-recovery motion of unmanned aircraft
US20090189016A1 (en)*2008-01-252009-07-30Insitu, Inc.Systems and methods for recovering and controlling post-recovery motion of unmanned aircraft
US10843817B2 (en)2009-04-242020-11-24Insitu, Inc.Systems and methods for recovering and controlling post-recovery motion of unmanned aircraft
US9944408B2 (en)2009-04-242018-04-17Insitu, Inc.Systems and methods for recovering and controlling post-recovery motion of unmanned aircraft
US10981671B2 (en)2010-09-272021-04-20Insitu, Inc.Line capture devices for unmanned aircraft, and associated systems and methods
US8944373B2 (en)2010-09-272015-02-03Insitu, Inc.Line capture devices for unmanned aircraft, and associated systems and methods
US9340301B2 (en)2010-09-272016-05-17Insitu, Inc.Line capture devices for unmanned aircraft, and associated systems and methods
US9856036B2 (en)2010-09-272018-01-02Insitu, Inc.Line capture devices for unmanned aircraft, and associated systems and methods
US10501178B2 (en)2011-11-152019-12-10Insitu, Inc.Controlled range and payload for unmanned vehicles, and associated systems and methods
US9868527B2 (en)2011-11-152018-01-16Insitu, Inc.Controlled range and payload for unmanned vehicles, and associated systems and methods
US9266610B2 (en)2011-11-152016-02-23Insitu, Inc.Controlled range and payload for unmanned vehicles, and associated systems and methods
US10399674B2 (en)2014-07-282019-09-03Insitu, Inc.Systems and methods countering an unmanned air vehicle
US11161610B2 (en)2014-07-282021-11-02Insitu, Inc.Systems and methods for countering an unmanned air vehicle
US10513350B1 (en)2014-11-202019-12-24Insitu, Inc.Capture devices for unmanned aerial, vehicles, including track-borne capture lines, and associated systems and methods
US9896222B2 (en)2014-11-202018-02-20Insitu, Inc.Capture devices for unmanned aerial vehicles, including track-borne capture lines, and associated systems and methods
US11053024B2 (en)2014-11-202021-07-06Insitu, Inc.Capture devices for unmanned aerial vehicles, including track-borne capture lines, and associated systems and methods
US10933997B2 (en)2015-10-022021-03-02Insitu, Inc.Aerial launch and/or recovery for unmanned aircraft, and associated systems and methods
US10407181B2 (en)2016-06-272019-09-10Insitu, Inc.Locking line capture devices for unmanned aircraft, and associated systems and methods
US10967987B2 (en)2016-06-272021-04-06Insitu, Inc.Locking line capture devices for unmanned aircraft, and associated systems and methods
US10767682B2 (en)2017-06-292020-09-08Insitu, Inc.Frangible fasteners with flexible connectors for unmanned aircraft, and associated systems and methods
US11066185B2 (en)2018-05-042021-07-20Insitu, Inc.Launch and/or recovery for unmanned aircraft and/or other payloads, including via parachute-assist, and associated systems and methods
US11142339B2 (en)2018-05-042021-10-12Insitu, Inc.Launch and/or recovery for unmanned aircraft and/or other payloads, including via parachute-assist, and associated systems and methods
US11603216B2 (en)2018-05-042023-03-14Insitu, Inc.Launch and/or recovery for unmanned aircraft and/or other payloads, including via parachute-assist, and associated systems and methods
US12071260B2 (en)2018-05-042024-08-27Insitu, Inc.Launch and/or recovery for unmanned aircraft and/or other payloads, including via parachute-assist, and associated systems and methods

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