FR2443973A1 - Independently operable, automatically locking aircraft load hooks - have separate linkages for locking engagement and common release gear - Google Patents
Independently operable, automatically locking aircraft load hooks - have separate linkages for locking engagement and common release gearInfo
- Publication number
- FR2443973A1 FR2443973A1 FR7835346A FR7835346A FR2443973A1 FR 2443973 A1 FR2443973 A1 FR 2443973A1 FR 7835346 A FR7835346 A FR 7835346A FR 7835346 A FR7835346 A FR 7835346A FR 2443973 A1 FR2443973 A1 FR 2443973A1
- Authority
- FR
- France
- Prior art keywords
- locking
- independently operable
- linkages
- hooks
- common
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 239000000725 suspension Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D7/00—Arrangement of military equipment, e.g. armaments, armament accessories or military shielding, in aircraft; Adaptations of armament mountings for aircraft
- B64D7/08—Arrangement of rocket launchers
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Load-Engaging Elements For Cranes (AREA)
Abstract
The device is intended for load suspension under the aircraft and has independently operable, automatically locking hooks (5, 6). They have separate power-ratio linkages (9, 11, 13, 15;10, 12, 14, 16) for engaging each of the hooks actuated by pressure from the load supporting ring (3, 4) on a counter tip (25, 26) on the hook. The hook engagement alters the respective positions of common-axis locking levers (15, 16) with bistable springs (21, 22) permitting other bistable springs (23, 24) to push common-axis (20) catch arms (17, 18) into a locking position. Disengagement is simultaneous, by way of a lever pivoting about the catch arm axis acting on both linkages. Due to double-armed design, it both withdraws the catches and pushes the locking levers over centre.
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7835346A FR2443973A1 (en) | 1978-12-15 | 1978-12-15 | Independently operable, automatically locking aircraft load hooks - have separate linkages for locking engagement and common release gear |
DE2954483A DE2954483C2 (en) | 1978-12-15 | 1979-08-25 | |
DE2934482A DE2934482C2 (en) | 1978-12-15 | 1979-08-25 | Suspension device for carrying and dropping aircraft loads provided with suspension fittings |
US06/074,629 US4313582A (en) | 1978-12-15 | 1979-09-12 | Device with independent hooks and automatic locking mechanism for hooking up loads under aircraft |
GB7942602A GB2039986B (en) | 1978-12-15 | 1979-12-11 | Device with independent hooks and automatic locking mechanism for hooking up loads under aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7835346A FR2443973A1 (en) | 1978-12-15 | 1978-12-15 | Independently operable, automatically locking aircraft load hooks - have separate linkages for locking engagement and common release gear |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2443973A1 true FR2443973A1 (en) | 1980-07-11 |
FR2443973B1 FR2443973B1 (en) | 1982-06-11 |
Family
ID=9216176
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7835346A Granted FR2443973A1 (en) | 1978-12-15 | 1978-12-15 | Independently operable, automatically locking aircraft load hooks - have separate linkages for locking engagement and common release gear |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2443973A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2555543A1 (en) * | 1983-11-29 | 1985-05-31 | Alkan R & Cie | DEVICE FOR CARRYING OUT AND LOADING LOADS UNDER AIRPLANE WITH TRIPLE EXHAUST BY ROLLERS |
FR3106812A1 (en) * | 2020-02-04 | 2021-08-06 | Alkan | AERONAUTICAL CONVEYING AND RELEASING DEVICE |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2865582A (en) * | 1954-10-26 | 1958-12-23 | Pastushin Aviat Corp | Means for releasably mounting stores on aircraft |
US3722944A (en) * | 1971-04-02 | 1973-03-27 | Mc Donnell Douglas Corp | Store release mechanisms |
FR2316178A1 (en) * | 1975-07-03 | 1977-01-28 | Alkan R & Cie | DEVICE FOR LIFTING LOADS ON AIRCRAFT, INCORPORATED IN THE CARRYING AND AUTOMATIC RELEASE SYSTEM |
US4043525A (en) * | 1976-03-31 | 1977-08-23 | Mcdonnell Douglas Corporation | Variable orificing device |
-
1978
- 1978-12-15 FR FR7835346A patent/FR2443973A1/en active Granted
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2865582A (en) * | 1954-10-26 | 1958-12-23 | Pastushin Aviat Corp | Means for releasably mounting stores on aircraft |
US3722944A (en) * | 1971-04-02 | 1973-03-27 | Mc Donnell Douglas Corp | Store release mechanisms |
FR2316178A1 (en) * | 1975-07-03 | 1977-01-28 | Alkan R & Cie | DEVICE FOR LIFTING LOADS ON AIRCRAFT, INCORPORATED IN THE CARRYING AND AUTOMATIC RELEASE SYSTEM |
US4043525A (en) * | 1976-03-31 | 1977-08-23 | Mcdonnell Douglas Corporation | Variable orificing device |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2555543A1 (en) * | 1983-11-29 | 1985-05-31 | Alkan R & Cie | DEVICE FOR CARRYING OUT AND LOADING LOADS UNDER AIRPLANE WITH TRIPLE EXHAUST BY ROLLERS |
EP0144265A1 (en) * | 1983-11-29 | 1985-06-12 | R. ALKAN & Cie. | Aircraft external load suspension and release unit with triple escapement rockers |
US11465744B2 (en) | 2020-02-03 | 2022-10-11 | Alkan | Aeronautical conveying and release device |
FR3106812A1 (en) * | 2020-02-04 | 2021-08-06 | Alkan | AERONAUTICAL CONVEYING AND RELEASING DEVICE |
Also Published As
Publication number | Publication date |
---|---|
FR2443973B1 (en) | 1982-06-11 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |