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US3197552A - Flexible base assembly - Google Patents

Flexible base assembly
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Publication number
US3197552A
US3197552AUS343171AUS34317164AUS3197552AUS 3197552 AUS3197552 AUS 3197552AUS 343171 AUS343171 AUS 343171AUS 34317164 AUS34317164 AUS 34317164AUS 3197552 AUS3197552 AUS 3197552A
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guide bar
members
cap
socket
sleeves
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US343171A
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Henry J Flair
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Description

July 27, 1965 H. J. FLAIR FLEXIBLE BASE ASSEMBLY Filed Feb. 6, 1964 FIG.I.
INVENTOR.
HENRY J. FLAIR BY ATTYS.
United States Patent O 3,197,552 FLEXIBLE BASE ASSEMBLY Henry 13. Flair, Franhiin Park, 12L, assignor, by mesne assignments, to the United tates of America as represented by the Secretary of the Navy Filed Feb. 6, 1964, Ser. No. 343,171 3 Claims. (Cl. 174-86) This invention relates to a flexible base assembly and more particularly to a flexible base assembly for enabling a whip antenna to pivot in a drag stream.
As submarines and other modern vessels achieve higher and higher speeds, the stress on the whip antenna becomes quite high. The stress is particularly high where there is no provision to allow the antenna to pivot from the vertical position. An antenna fixed at a position other than vertical is less desirable for communicating. Larger antennas to withstand the stress are impractical.
The general purpose of this invention is to provide a flexible base assembly which maintains the stress on the whip antenna within tolerable limits. To attain this the whip antenna is pivoted into the drag stream by a flexible base assembly.
An object of the present invention is to provide an assembly to substantially reduce the failure of whip antennas.
Another object of this invention is to provide for the use of slender ship antennas of practical size without ensuing antenna failures.
Yet another object of this invention is to provide for the use of vertical antenna capable of having a silhouette that can be streamlined with the drag stream.
With these and other objects in view, as will hereinafter more fully appear and which will be more particularly pointed out in the appended claims, reference is now made to the following description taken in connection with the accompanying drawings in which:
FIG. 1 shows a flexible base assembly in a deflected position.
FIG. 2 shows a smaller base assembly in a normal vertical position.
Referring now to the drawings, wherein like reference numerals designate like or corresponding parts throughout the two figures, there is shown in FIG. 1 a deflected flexible base assembly designated generally as reference numeral M9. Alarge end cap 12 is used to fasten the base assembly to a submarine or other vessel or mounting surface. Preferably theend cap 12 fits over a stud or other rotruding elements and is held in contact therewith by a safety capscrew 14-.
Theend cap 12 is fastened to asocket cap 16. Asafety screw 18 keeps theend cap 12 andsocket cap 16 from becoming unfastened. The outer portion of thesocket joint 16 is curved to act as acam surface 17.
Confined within a socket formed by theend cap 12 and thesocket cap 16 is aball pivot 20. Secured to the ball pivot Ed is aguide bar 22. The securing means for the guide bar and ball pivot may be any conventional se curing means. For example, adowel pin 21 is shown in the drawing as the securing means.
Surrounding theguide bar 22 are twosliding sleeves 24, the end of which are shaped to ride on thecam surface 17 andcurved surface 78 to be referred to later. The two sleeves face each other at anabutment 26. Theabutment 26 acts as a stop for thesleeves 24 and therefore controls the maximum amount of deflection of each end of the base assembly. The spacing between thesleeves 24 and theguide bar 22 is sufficient at theabutment end 23 to allow the sleeves to rock. Thus in a deflected position of the base assembly, thesleeves 24 rock and thesleeve surfaces 25 are in contact with theguide bar 22. The spacing 27 between theguide bar 22 andsleeve 24. is quite small but still suflicient to allow thesleeves 24 to rock. Acompression spring 23 surrounds the guide bar and is confined betweenflanges 30 on the extreme end respectively of thesleeves 24.
The other end of theguide bar 22 is secured to aball pivot 32 which is similar to theother ball pivot 20.
Asocket cap 36 combines with awhip end connector 38 to confine theball pivot 32 with the cavity defined by the juncture of the two. A safety screw 40 is similar to and performs the same function assafety screw 18.
Shown in FIG. 1 in dotted lines is awhip antenna base 42 fastened to thewhip end connector 38.
A smaller flexible base assembly 50 is shown in FIG. 2 Amast end connector 52 is secured to the submarine. Asocket cap 54 combines with theconnector 52 to enclose aball pivot 56. Aguide bar 58 is fastened to theball pivot 56. Surrounding theguide bar 58 are slidingsleeves 60 and acompression spring 62 in the same manner as in FIG. 1. The interior surface 61 of thesleeves 60 is shaped to allow the sleeves to rock when the assembly is deflected.
Aball pivot 64, secured to theguide bar 58 is enclosed within asocket joint 66 and a whip end connector 63. Awhip antenna 70 shown in dotted lines, is secured to the connector es.
Operation The base assemblies shown in FIG. 1 and FIG. 2 function in the same manner. The flexible base assembly 50, FIG. 2, holds a whip antenna in a normally vertical position. Upon being subjected to a drag stream of suflicient force, which places a stress upon the antenna, the base assembly it), FIG. 1, bends thus streamlining the antenna with the drag stream and reducing the drag force and consequently the stress on the antenna. Thesocket cap 36 pivots onball pivot 32 thus compressing thespring 28 contained within theflanges 30 of thesliding sleeves 24.
Theball pivot 20 pivots within thesocket cap 16 with a further compression of thespring 28 contained within the flanges 3d of thesliding sleeves 24.
In a deflected position the force pushes thefulcrum point 72 of thesliding sleeve 24 with the result that the curvefree side 74 moves up and theinner edge 76 is forced against theguide bar 22.
When the drag stream force is removed then thecurved surface 78 of thesocket cap 36 engages the free side '74 while thespring 28 is still under compression. The force on thefree side 74 against thesurface 78 eases the socket joint back into normal position while dampening out any vibration. In this manner there is no rocking back and forth of the antenna since thespring 28 is under compression and creates a force against thefulcrum 72 andsurface 78 when the base assembly is in a normal position.
The base assembly is capable of deflecting in any of 360 degrees about the base plane and therefore will function to compensate for a drag stream coming from any direction.
The illustrated model shown in the drawing is designed to deflect a maximum of 35 degrees on each ball pivot for a total of 70 degrees. However, a base assembly could be designed to pivot less than 70 degrees or as much as degrees.
Under certain conditions there may only be a need for one section to pivot thus eliminating or locking the action of one ball pivot.
The base assembly may be fitted with an alemite fitting to supply lubrication to theball pivots 20 and 32.
The apparatus shown and described is merely illustra tive and the invention is not limited thereto. Alterations and modification will readily suggest themselves to persons skilled in the art Without departing from the true spirit of this invention or from the scope of the annexed claims.
What is claimed is:
1. An antenna mount for submarines comprising:
a guide bar having a ball member on each end thereof and an abutment mounted therebetween;
each of said ball members secured in a socket member comprising a first cap member provided With a socket portion for receiving said ball member and a second cap member for retaining said ball member in said first cap member;
first and second sliding sleeve means slidably surrounding said guide bar, each of said sliding sleeve means being mounted on either side of said abutment, each of said sleeves having a shoulder forming an abutment at one of its ends;
a spring member concentrically mounted around said first and second sleeve members between said shoulders on said sleeves for biasing said sleeves against said second cap members;
said second cap members and said shoulders having mating curved surfaces in engagement With each other so as to provide for tilting movement of said socket members with respect to said guide bar; and
said abutment on said guide bar having a radial extent which exceeds the inner diameter of the other ends of said sliding sleeve members thereby restraining the degree of tilt of the socket members relative to the guide bar.
2. An antenna mount for submarines are defined in claim 1 but further characterized by having an antenna mounting means connected to the other end of one of said socket members for attaching an antenna to said mount whereby an antenna is held in a vertical position for References Cited by the Examiner UNlTED STATES PATENTS Ianney. Scholey. Eckart. Olenick. Daggett 28786 Cain 64l5 X FOREIGN PATENTS France.
CARL W. TOMLIN, Primary Examiner.

Claims (1)

1. AN ANTENNA MOUNT FOR SUBMARINES COMPRISING: A GUIDE BAR HAVING A BALL MEMBER ON EACH END THEREOF AND AN ABUTMENT MOUNTED THEREBETWEEN; EACH OF SAID BALL MEMBERS SECURED IN A SOCKET MEMBER COMPRISING A FIRST CAP MEMBER PROVIDED WITH A SOCKET PORTION FOR RECEIVING SADI BALL MEMBER AND A SECONND CAP MEMBER FOR RETAINING SAID BALL MEMBER IN SAID FIRST CAP MEMBER; FIRST AND SECOND SLIDING SLEEVE MEANS SLIDABLY SURROUNDING SAID GUIDE BAR, EACH OF SAID SLIDING SLEEVE MEANS BEING MOUNTED ON EITHER SIDE OF SAID ABUTMENT, EACH OF SAID SLEEVES HAVING A SHOULDER FORMING AN ABUTMENT AT ONE OF ITS ENDS; A SPRING MEMBER CONCENTRICALLY MOUNTED AROUND SAID FIRST AND SECOND SLEEVE MEMBERS BETWEEN SAID SHOULDERS ON SAID SLEEVES FOR BIASING SAID SLEEVES AGAINST SAID SECOND CAP MEMBERS; SAID SECOND CAP MEMBERS AND SAID SHOULDERS HAVING MATING CURVED SURFACES IN ENGAGEMENNT WITH EACH OTHER SO AS TO PROVIDE FOR TILTING MOVEMENT OF SAID SOCKET MEMBERS WITH RESPECT TO SAID GUIDE BAR; AND SAID ABUTMENT ON SAID GUIDE BAR HAVING A RADIAL EXTENT WHICH EXCEEDS THE INNER DIAMETER OF THE OTHER ENDS OF SAID SLIDING SLEEVE MEMBERS THEREBY RESTRAINING THE DEGREE OF TILT OF THE SOCKET MEMBERS RELATIVE TO THE GUIDE BAR.
US343171A1964-02-061964-02-06Flexible base assemblyExpired - LifetimeUS3197552A (en)

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Cited By (18)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US3451699A (en)*1966-05-021969-06-24Chevron ResCoupling devices for use in offshore well work
US3473148A (en)*1968-02-231969-10-14Earl KoenigSafety twinkle lamp
US4118951A (en)*1977-07-281978-10-10Neasham Leo BDrive unit for selectively effecting driving or free-wheeling condition of propeller shafting
US4151728A (en)*1978-01-161979-05-01Kimball Brian EUniversal coupling
US4228756A (en)*1979-02-011980-10-21Sailing Systems, Inc.Catamaran tiller-crossbar connector
FR2533487A1 (en)*1982-09-281984-03-30Molaug Ole ARTICULATED JOINTS ROBOT ARM
US4495961A (en)*1982-02-161985-01-29Heilmeier & Weinlein, Fabrik Fur Oel-Hydraulik Gmbh & Co., KgFlow divider
DE3427414A1 (en)*1984-07-251986-02-06Hans Dr. Langenthal Fehrensen CONNECTING DEVICE FOR TWO COMPONENTS
US4790789A (en)*1987-05-221988-12-13Mathis Michael SToy figure having adjustably movable joints
US5642956A (en)*1996-01-251997-07-01Regents Of The University Of CaliforniaAdjustable link for kinematic mounting systems
US5803647A (en)*1996-01-311998-09-08Hughes; CeiriogHandrail connection device
US6331089B1 (en)*2000-02-292001-12-18Shimano, Inc.Mounting device for bicycle component
US6352227B1 (en)*2000-06-082002-03-05Clarence Eduard HathawaySegmented, ball jointed support
US20060140710A1 (en)*2002-12-092006-06-29Valeo Systems D'essuyageBall pin and ball joint comprising one such ball pin
US20120142255A1 (en)*2010-12-072012-06-07The Boeing CompanyRobotic surface preparation by a random orbital device
WO2014199857A1 (en)*2013-06-112014-12-18株式会社IhiUnderwater mobile body
US9279437B2 (en)*2011-11-242016-03-08Knorr-Bremse Systeme Fuer Nutzfahrzeuge GmbhAdjustable holding device for sensors
US9453376B1 (en)*2008-12-092016-09-27Sandia CorporationSelf-assembling segmented coiled tubing

Citations (7)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US571972A (en)*1896-11-24Spring
FR556825A (en)*1922-10-021923-07-27 Soft and flexible transmission device
US1595317A (en)*1924-07-241926-08-10Cook Spring CompanySpring and seat therefor
US1623582A (en)*1922-11-131927-04-05John M ZaneFlexible coupling
US1960709A (en)*1931-07-231934-05-29Boyle Valve CompanyEngine valve
US2945084A (en)*1958-01-241960-07-12Donal C WeaverFlexible connector for aerials or the like
US3018125A (en)*1959-09-301962-01-23Gen ElectricFlexible link assembly for transmitting linear motion

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US571972A (en)*1896-11-24Spring
FR556825A (en)*1922-10-021923-07-27 Soft and flexible transmission device
US1623582A (en)*1922-11-131927-04-05John M ZaneFlexible coupling
US1595317A (en)*1924-07-241926-08-10Cook Spring CompanySpring and seat therefor
US1960709A (en)*1931-07-231934-05-29Boyle Valve CompanyEngine valve
US2945084A (en)*1958-01-241960-07-12Donal C WeaverFlexible connector for aerials or the like
US3018125A (en)*1959-09-301962-01-23Gen ElectricFlexible link assembly for transmitting linear motion

Cited By (21)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US3451699A (en)*1966-05-021969-06-24Chevron ResCoupling devices for use in offshore well work
US3473148A (en)*1968-02-231969-10-14Earl KoenigSafety twinkle lamp
US4118951A (en)*1977-07-281978-10-10Neasham Leo BDrive unit for selectively effecting driving or free-wheeling condition of propeller shafting
US4151728A (en)*1978-01-161979-05-01Kimball Brian EUniversal coupling
US4228756A (en)*1979-02-011980-10-21Sailing Systems, Inc.Catamaran tiller-crossbar connector
US4495961A (en)*1982-02-161985-01-29Heilmeier & Weinlein, Fabrik Fur Oel-Hydraulik Gmbh & Co., KgFlow divider
FR2533487A1 (en)*1982-09-281984-03-30Molaug Ole ARTICULATED JOINTS ROBOT ARM
DE3427414A1 (en)*1984-07-251986-02-06Hans Dr. Langenthal Fehrensen CONNECTING DEVICE FOR TWO COMPONENTS
EP0169463B1 (en)*1984-07-251988-03-30Hans Dr. FehrensenConnection device for two members
US4790789A (en)*1987-05-221988-12-13Mathis Michael SToy figure having adjustably movable joints
US5642956A (en)*1996-01-251997-07-01Regents Of The University Of CaliforniaAdjustable link for kinematic mounting systems
US5803647A (en)*1996-01-311998-09-08Hughes; CeiriogHandrail connection device
US6331089B1 (en)*2000-02-292001-12-18Shimano, Inc.Mounting device for bicycle component
US6352227B1 (en)*2000-06-082002-03-05Clarence Eduard HathawaySegmented, ball jointed support
US20060140710A1 (en)*2002-12-092006-06-29Valeo Systems D'essuyageBall pin and ball joint comprising one such ball pin
US9453376B1 (en)*2008-12-092016-09-27Sandia CorporationSelf-assembling segmented coiled tubing
US20120142255A1 (en)*2010-12-072012-06-07The Boeing CompanyRobotic surface preparation by a random orbital device
US8517799B2 (en)*2010-12-072013-08-27The Boeing CompanyRobotic surface preparation by a random orbital device
US9279437B2 (en)*2011-11-242016-03-08Knorr-Bremse Systeme Fuer Nutzfahrzeuge GmbhAdjustable holding device for sensors
WO2014199857A1 (en)*2013-06-112014-12-18株式会社IhiUnderwater mobile body
US20160090160A1 (en)*2013-06-112016-03-31Ihi CorporationUnderwater mobile body

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