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US1758880A - Retarding device for aircraft - Google Patents

Retarding device for aircraft
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Publication number
US1758880A
US1758880AUS279320AUS27932028AUS1758880AUS 1758880 AUS1758880 AUS 1758880AUS 279320 AUS279320 AUS 279320AUS 27932028 AUS27932028 AUS 27932028AUS 1758880 AUS1758880 AUS 1758880A
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United States
Prior art keywords
cable
aeroplane
grappling
grappling device
pick
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Expired - Lifetime
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US279320A
Inventor
Lytle S Adams
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AIRWAYS PATENT Corp
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AIRWAYS PATENT CORP
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Publication date
Application filed by AIRWAYS PATENT CORPfiledCriticalAIRWAYS PATENT CORP
Priority to US279320ApriorityCriticalpatent/US1758880A/en
Application grantedgrantedCritical
Publication of US1758880ApublicationCriticalpatent/US1758880A/en
Anticipated expirationlegal-statusCritical
Expired - Lifetimelegal-statusCriticalCurrent

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RETARDING DEVICE FOR AIRCRAFT Filed May 21I 1928 INVENTOR 24 2/ I i -Adoms -i r A? 6. d? E m 22 /z 2/ ATTORNEY Patented May 13,- 1930 UNITED STATES PATENT OFFICE LYTLE S. ADAMS, OF SEATTLE, WASHINGTON, ASSIGNOR TO AIRWAYS PATENT COR- PORATION, A CORPORATION OF DELAWARE RETAEDIliTG DEVICE FOR AIRCRAFT Application filed May 21, 1928. Serial No. 279,320.
My invention relates to improvements in landing devices and the object of my invention is to provide simple and eflicient means by which a moving aeroplane or otheraircraft while in the air is enabled to pick up a ground tackle to connect itself with a retarding device by which the landing speed of the aeroplane may be retarded and the aeroplane quickly brought to a stop as it lands.
More specific objects are to provide means by which a weighted cable suspended from an aeroplane or other aircraft while moving in the air may be guided to, and caused to engage with, a device for taking hold of said cable, hereinafter termed a grappling device, that is supported ina fixed and stationary position to thereby effect a connection through the grappling device with any object or with any retarding means which it is desired to connect to the aeroplane.
Other objects are toprovide a grappling member of simple and efficient construction that may be readily engaged by a cable;'to provide efficient means for releasably supporting the grappling member; to provide guide means for aligning the cable with the grappling member; and to provide magnetic means for insuring the engagement of the cable within the grappling member.
Other and more specific objects will be apparent fromthe following description taken in connection with the accompanying drawings, wherein Figure 1 is a perspective View of apparatus constructed in accordance with my invention.
Fig. 2 is a longitudinal sectional View of the same, parts being shown in elevation.
Fig. 3 is an elevation showing the grappling member and a package connected with a cable.
Fig. 4 is a longitudinal section showing a retarding device connected with the grape pling member for retarding the speed of an aeroplane in landing, the cable being shown in the act of engaging with the grappling member.
Fig. 5 is a view similar to Fig. 4 except that the cable has picked up the grappling member and the retarding device or brake is in operation.
Fig. 6 is a cross section on a larger scale through the grappling member and the holder or receptacle for the same.
In a general way my invention consists in providing on the ground a pick up station affording two converging side walls, a magnetized bottom wall, and in providing a grappling device supported at the narrowest place between the side walls and in providing, on the aeroplane, a cable capable of being lowered and raised and having a weight of magnetic material on its lower end, the converging side walls and the magnetic bottom wall serving to guide the cable into the grappling device so that said grappling device will be picked up bodily by the cable.
Like reference numerals indicate like parts throughout the drawings wherein I show a pick up station embodying twoabutments 7 and 8 affording twoside walls 9 and 10 that are closer together at'the bottom and farther apart at the top and that afford a wide opening at the cable intake end and converge to form a narrow opening at the cable exit end.
A receptacle 11 is formed between the convergent ends of thewalls 8 and 9 for the reception of a cable grappling device designated by thenumeral 12. The shape of this receptacle is more clearly shown in Fig- 6, the same having overhangingtop edges 13 and having its side walls recessed as at 14 affording room for abail member 15 that is connected with the grappling member. Thebail 15 is large enough so that it will swing entirely over the grappling member.
Abottom wall 16 is disposed between theside walls 9 and 10 and extends at an incline up to the receptacle 11 and aplate 17 of elecstop 25, permits the cable to readily enter theslot 20 but prevents the release of said cable except when the pawl '22 is manually depressed. Aweight 26 of magnetic material is secured to the bottom end of thecable 21.
Flags 27 may be placed at the outer. ends of the end of the pick up station and being shielded by said station from direct contact with thecable 21 andweight 26. As the aeroplane approaches the pick up station the pilot lowers hiscable 21 until theweight 26 touches or almost touches the ground and at the same time maneuvers his aeroplane so that the cable will be drawn between thewalls 9 and 10 and will be guided to thegrappling device 12 which has previously been placed in the receptacle 11. As theweight 26 is drawn onto themagnetized plate 17 it, will be attracted and retarded thereby and prevented from bouncing and thecable 21 will be drawn taut and as the Weight approaches thegrappling device 12 the cable will be drawn into theslot 20 and locked there by thepawl 22. l/Vhen theweight 26 is drawn against thegrappling device 12 said grappling device will be drawn out of its receptacle and together with. theload 28 that is connected-therewith will be picked up and may be drawn up to the aeroplane. As thegrappling device 12 is drawn out of its receptacle 11 thebail 15 drops down and straightens.
out as shown in Figs. 3 and 5.
For retarding the speed of the aeroplane and bringing the same to a stop in less dis tance in landing I provide afriction drum 30 mounted for rotationbelowthe grappling device 12 and having acable 31 wound thereon that is connected with thebail 15 of the grappling device. When the apparatus is used as a retarding'means, in landing, the aeroplane flies low over the pick up station and lands just after it has passed over said station and thecable 21 picks up the grappling device and unwinds thecable 31 on thedrum 30 as shown in Fig. 5. Any desired amount of resistance may be exerted by thedrum 30 as may be required to bring the aeroplane to a quick stop without damage to the same.
The retarding means may be used in a similar manner for stopping lighter-than-air craft and holding them against a heavy wind, thereby dispensing with the services of a part of the ground crew required for handling such craft.
The foregoing description and accompanying drawings clearly disclose a preferred embodiment of my invention, but it will be understood that thisdisclosure is merely ilvice as applied to raising a load from the ground to be transferred to the aircraft, that being reserved for a divisional application.
What I claim is 1. In aeroplane pick up apparatus,a cable having a weight on its lower end and adapted to hang from an aeroplane, a grappling device arranged to receive said cable and be picked up thereby, and asupport for the grappling device having an upwardly inclined surface and forwardly converging guides for guiding the weight to the grappling device.
" 2. In aeroplane pick up apparatus, a cable arranged to hang from a moving aeroplane and having a weight on its lower end, a grappling device arranged to receive said cable and be picked u by the cable and a trough shape-d support or the grappling device having overhanging top edges.
3. In apparatus for making connection with a cable that is suspended from a moving aeroplane, a pick up station located on the ground, a grappling device supported by the pick up station and means in the pick up station for guiding the cable upwardly and laterally to the grappling device.
4. In apparatus for making connection with a cable that is suspended from a moving aeroplane in the air and that has a Weight on its bottom end, a pick up station havmg two convergent guide walls and an upwardly walls and at the upper forward end of thebottom for receiving and attaching itself to the cable.
5. In aeroplane pick up apparatus, a cable arranged to hang from a movlng aeroplane, a weight of magnetic material on the lower end of said cable, a grappling device arranged to receive said cable and be picked up thereby. a support for the grappling device, means for connecting a device on which a pull is to be exerted to the grappling device, means for guiding the cable to the grappling device and a magnetized plate in thebottom of. the guiding means for attracting said weight and drawing said cable into said grappling device.
6. In aeroplane pick up apparatus, a cable arranged to hang from a moving aeroplane, a weight of magnetic material on the lower end of said cable, a pick up station embodying two/abutments having two side guide walls divergent from bottom to top and convergent ing a receptacle between the convergent ends of said walls, a grappling device arranged to toward one end of the station, means formbe removably disposed within said receptacle and having a V shaped trough in its top side that terminates in a cable receiving slot, a pawl for holding a cable within said slot, means connecting the grappling device with apparatus for exerting a pull on said grappling device and an electromagnetic floor between said two guide walls for attracting the Weight on said cable.
7; The apparatus as described in claim 6 in which a bail member large enough to permit the grappling device to, turn therein is secured to the grappling device and the sides of the grappling device receptacle are recessed to afford clearance for said bail.
8'. In aeroplane pick up apparatus, a cable arranged to hang from a moving aeroplane, a grappling device arranged to be picked up by said 4 cable having an automatically set lock, and means connected with the grappling device for exerting a retarding force on the aeroplane in landing.
9. In aeroplane plck up apparatus, a cable arranged to hang from a moving aeroplane,
a grappling device arranged to be picked up by said cable, a friction brake drum adapted to offer resistance to rotation and a cable wound on the drum and connected with the grappling device 'for exerting a. retarding force on the aeroplane in landing.
10. In an airplane pick-up apparatus, a
cable arranged to hang from a moving a1rplane, a weighton the lower end of the cable, a pick-up station embodying two abutments having side guide walls convergent toward one end of the station, and forming a receptacle between the convergent ends of said walls, a grappling device disposed within said receptacle and having a trough terminating in a cable receiving slot, means connecting the grappling device with the apparatus for exerting apull on the grappling device and an upwardly inclined ground floor between said two guide walls for directing the weight on said cable to said grappling device.
11. In aeroplane pick up apparatus, a cable arrangedto hang from a moving aeroplane, a weight on the lower end of said cable, a grappling device arranged to receive said cable.
and to be picked up thereby, a sup ort for the grappling device, and upwar ly and laterally converging guide means associated with said support for guiding the cable to. the grappling device.
In witness'whereof, I hereunto subscribe day of May, A. D. 1928.
my name this 15th LYTLE S. ADAMS.
US279320A1928-05-211928-05-21Retarding device for aircraftExpired - LifetimeUS1758880A (en)

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Application NumberPriority DateFiling DateTitle
US279320AUS1758880A (en)1928-05-211928-05-21Retarding device for aircraft

Applications Claiming Priority (1)

Application NumberPriority DateFiling DateTitle
US279320AUS1758880A (en)1928-05-211928-05-21Retarding device for aircraft

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US1758880Atrue US1758880A (en)1930-05-13

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US2505707A (en)*1944-12-211950-04-25Wilmington Trust CompanyShock absorbing method and apparatus for air pickup systems and the like
US2692120A (en)*1952-11-191954-10-19All American Eng CoAir pickup system
US20070158498A1 (en)*2006-01-062007-07-12Lockheed Martin CorporationUAV recovery system II

Cited By (4)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US2505707A (en)*1944-12-211950-04-25Wilmington Trust CompanyShock absorbing method and apparatus for air pickup systems and the like
US2692120A (en)*1952-11-191954-10-19All American Eng CoAir pickup system
US20070158498A1 (en)*2006-01-062007-07-12Lockheed Martin CorporationUAV recovery system II
US7510145B2 (en)2006-01-062009-03-31Lockheed Martin CorporationUAV recovery system II

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