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US3954233A Expired / Lapsed US ⏱️ 0.0 years remaining

Automatic hanging and wedging device for aircraft loads

Assignee: R Alkan et Cie
•
Filing: 1975-03-13
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Granted: 1976-05-04
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Expires: 1995-03-13
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Abstract

Abstract This device for automatically releasably hanging and holding against lateral oscillation load carried under aircrafts has load suspension hooks and holding members preventing the lateral oscillation of the load which project very moderately from the underface of a closed casing containing the actuating mechanism. This mechanism includes in combination linkage detents and springloaded devices disposed on either side of each load suspension hook. A certain delay is introduced into the action whereby when the load is lifted for engagement with the hooks, these are actuated to their load-supporting position and release with a predetermined time-lag the linkage holding the load against lateral oscillation to their operative position. To this end, each pivotally mounted hook is connected via a spring-loaded piston-and-cylinder actuator to a rocker controlling the movement of wedge members controlling in turn a lever supporting the holding members.

Inventors

  • 👤 Jean H. Hasquenoph
  • 👤 Pierre F. Coutin

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-23 22:19
CPC Classifications
B; B64; B64D; B64D7/00; B64D7/08

Claims Analysis

Total Claims: 13
Claim 1
Independent Claim 73 words
Device for automatically and releasably hanging and holding loads carried under aircraft against lateral oscillation, comprising automatic detent means of the wedge member type for retaining the load, means for mechanically connecting said detent means to a pivoting suspension hook when said suspension hook is engaged by the load, and automatic load holding means adapted to hold the load against lateral oscillation, said automatic load holding means being actuated directly by said hook.
Claim 2
Dependent Claim 73 words
Device for automatically and releasably hanging and holding loads carried under aircraft against lateral oscillation, comprising automatic detent means of the wedge member type for retaining the load, means for mechanically connecting said detent means to a pivoting suspension hook when said suspension hook is engaged by the load, and automatic load holding means adapted to hold the load against lateral oscillation, said automatic load holding means being actuated directly by said hook.
Claim 3
Dependent Claim 80 words
Device as set forth in claim 1, wherein said load holding means comprise a spring-type actuator interposed between on the one hand a lever controlling the actuation of said wedge members and on the other hand a load suspension hook, said actuator acting on the one hand in the direction to urge said wedge members to the hook closing position and on the other hand in the direction to open said hook in the release position of said detent means.
Claim 4
Dependent Claim 41 words
Device as set forth in claim 2, wherein each wedge member is adapted to react against a fixed element of the aircraft structure and a movable holding member adapted to engage the load in order to hold same against lateral oscillation.
Claim 5
Dependent Claim 41 words
Device as set forth in claim 3, wherein each wedge member is adapted to engage a shoe-supporting load-holding member consisting of a pivoting lever carrying a shoe adapted to engage the top of the load for holding same against lateral oscillation.
Claim 6
Dependent Claim 51 words
Device as set forth in claim 4, wherein the contour of the operative faces of each wedge member and the faces between which said wedge member is operative, notably the face of the movable member which is associated with the holding shoe, is such that it provides a constant contact angle.
Claim 7
Dependent Claim 23 words
Device as set forth in claim 5, wherein two shoe-supporting load-holding levers are provided, one on each side of each load suspension hook.
Claim 8
Dependent Claim 24 words
Device as set forth in claim 4, wherein said pair of pivoting levers disposed on either side of a suspension hook are operatively interconnected.
Claim 9
Dependent Claim 45 words
Device as set forth in claim 5, wherein said pair of pivoting levers disposed on either side of a suspension hook are responsive to the action of a mechanism operatively connected to said hook so as to raise said levers during the hook opening movement.
Claim 10
Dependent Claim 154 words
Device for releasably hanging and holding loads carried under aircrafts against lateral oscillation, comprising load holding members adapted to engage directly the load to be held against lateral oscillation, wedge members adapted to engage directly the load holding members, pivotally mounted suspension hooks having beak portions for engaging the load, a closed casing having apertures, and a mechanism capable of controlling both said load suspension hooks and said wedge members, said mechanism and said wedge members being mounted in said closed casing with only the beak portions of said load suspension hooks and said load holding members responsive to said wedge members projecting from said casing apertures, each of said load holding members comprising a push member extending through one aperture of said casing and a ball and socket means capable when said push member is actuated by said wedge members to engage the top of the load to be held against lateral oscillation.
Claim 11
Dependent Claim 154 words
Device for releasably hanging and holding loads carried under aircrafts against lateral oscillation, comprising load holding members adapted to engage directly the load to be held against lateral oscillation, wedge members adapted to engage directly the load holding members, pivotally mounted suspension hooks having beak portions for engaging the load, a closed casing having apertures, and a mechanism capable of controlling both said load suspension hooks and said wedge members, said mechanism and said wedge members being mounted in said closed casing with only the beak portions of said load suspension hooks and said load holding members responsive to said wedge members projecting from said casing apertures, each of said load holding members comprising a push member extending through one aperture of said casing and a ball and socket means capable when said push member is actuated by said wedge members to engage the top of the load to be held against lateral oscillation.
Claim 12
Dependent Claim 44 words
Device as set forth in claim 9, wherein each wedge member is disposed in a recess formed in said closed casing and adapted, in its operative position, to engage the top surface of said recess and thus push a corresponding load holding member downwards.
Claim 13
Dependent Claim 47 words
Device as set forth in claim 10, wherein said aperture formed in said casing to permit the projection of said hook beak portions and load holding members are sealed, the former by means of shields having a part-cylindrical configuration, and the latter by means of resilient sleeves.

References Cited (Backward Citations)

US3610094A Cited
US3494248A Cited
US3784132A Cited
US3722944A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1979-05-04 1979-11-03 1980-05-04 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1983-05-04 1983-11-03 1984-05-04 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1987-05-04 1987-11-03 1988-05-04 $7700.00 Window Closed / Lapsed

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