FR2407858A2 - Self locking catch for airborne loads - operates with double profile cam to ease insertion of hook - Google Patents
Self locking catch for airborne loads - operates with double profile cam to ease insertion of hookInfo
- Publication number
- FR2407858A2 FR2407858A2 FR7733258A FR7733258A FR2407858A2 FR 2407858 A2 FR2407858 A2 FR 2407858A2 FR 7733258 A FR7733258 A FR 7733258A FR 7733258 A FR7733258 A FR 7733258A FR 2407858 A2 FR2407858 A2 FR 2407858A2
- Authority
- FR
- France
- Prior art keywords
- hook
- double profile
- catch
- profile cam
- operates
- 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
- 230000037431 insertion Effects 0.000 title abstract 2
- 238000003780 insertion Methods 0.000 title abstract 2
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—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft
- B64D7/08—Arrangements of rocket launchers or releasing means
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Clamps And Clips (AREA)
- Supports Or Holders For Household Use (AREA)
Abstract
The airborne load has a support hook (48) which locates under a pressure peg (50) whose inner ends rests against a double profile cam (80) to press the hook against the retaining catch (6). The double profile enables the insertion to have a greater freedom of movement to ease the fitting. In the catch position the double profile is slid aside and triggers the sprung catch when the hook presses the peg. The catch slides under the hook and the profile cam slides over the top of the peg and locks the mounting.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7733258A FR2407858A2 (en) | 1977-11-04 | 1977-11-04 | Self locking catch for airborne loads - operates with double profile cam to ease insertion of hook |
DE19782835607 DE2835607C3 (en) | 1977-11-04 | 1978-08-14 | Device for attaching and bracing loads under an aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7733258A FR2407858A2 (en) | 1977-11-04 | 1977-11-04 | Self locking catch for airborne loads - operates with double profile cam to ease insertion of hook |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2407858A2 true FR2407858A2 (en) | 1979-06-01 |
FR2407858B2 FR2407858B2 (en) | 1982-11-05 |
Family
ID=9197283
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7733258A Granted FR2407858A2 (en) | 1977-11-04 | 1977-11-04 | Self locking catch for airborne loads - operates with double profile cam to ease insertion of hook |
Country Status (2)
Country | Link |
---|---|
DE (1) | DE2835607C3 (en) |
FR (1) | FR2407858A2 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3019782C2 (en) * | 1980-05-23 | 1985-12-19 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Bomb or external load lock |
DE3941294A1 (en) * | 1989-12-14 | 1991-06-20 | Messerschmitt Boelkow Blohm | DEVICE FOR TENSIONING A LOAD |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1092828A (en) * | 1964-07-01 | 1967-11-29 | Douglas Aircraft Co Inc | Store carrier with sway braced lug |
DE2214559A1 (en) * | 1971-03-25 | 1972-11-23 | The Secretary of State for Defence in Her Britannic Majestys Government of the United Kingdom of Great Britain and Northern Ireland, London | Ejector release device |
FR2220423A1 (en) * | 1973-03-05 | 1974-10-04 | Ml Aviation Co Ltd | |
US3854681A (en) * | 1973-06-01 | 1974-12-17 | Alkan R & Cie | Device for steadying loads suspended from aircrafts |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2457795B2 (en) * | 1974-09-16 | 1980-04-03 | R. Alkan & Cie., Paris | Device for attaching and bracing loads that are carried under an aircraft |
-
1977
- 1977-11-04 FR FR7733258A patent/FR2407858A2/en active Granted
-
1978
- 1978-08-14 DE DE19782835607 patent/DE2835607C3/en not_active Expired
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1092828A (en) * | 1964-07-01 | 1967-11-29 | Douglas Aircraft Co Inc | Store carrier with sway braced lug |
DE2214559A1 (en) * | 1971-03-25 | 1972-11-23 | The Secretary of State for Defence in Her Britannic Majestys Government of the United Kingdom of Great Britain and Northern Ireland, London | Ejector release device |
FR2220423A1 (en) * | 1973-03-05 | 1974-10-04 | Ml Aviation Co Ltd | |
US3854681A (en) * | 1973-06-01 | 1974-12-17 | Alkan R & Cie | Device for steadying loads suspended from aircrafts |
Also Published As
Publication number | Publication date |
---|---|
DE2835607C3 (en) | 1981-04-02 |
FR2407858B2 (en) | 1982-11-05 |
DE2835607B2 (en) | 1980-07-31 |
DE2835607A1 (en) | 1979-05-10 |
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