FR2370948A1 - AZIMUT HARMONIZATION DEVICE FOR A LOAD TAKEN UNDER AIRCRAFT - Google Patents
AZIMUT HARMONIZATION DEVICE FOR A LOAD TAKEN UNDER AIRCRAFTInfo
- Publication number
- FR2370948A1 FR2370948A1 FR7634428A FR7634428A FR2370948A1 FR 2370948 A1 FR2370948 A1 FR 2370948A1 FR 7634428 A FR7634428 A FR 7634428A FR 7634428 A FR7634428 A FR 7634428A FR 2370948 A1 FR2370948 A1 FR 2370948A1
- Authority
- FR
- France
- Prior art keywords
- load
- trigger
- ejector
- azimut
- taken under
- 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
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
Abstract
Le dispositif d'harmonisation en azimut d'une charge emportée sous avion est destiné à être associé à une extremité d'un déclencheur ou éjecteur supportant la charge à larguer pour assurer le réglage désiré sans modification du déclencheur ou de l'éjecteur. Une extrémité 1 de l'ossature du déclencheur ou de l'éjecteur reçoit un bloc support 4 d'une extrémité du mécanisme du déclencheur ou de l'éjecteur et un moyen est prévu pour décaler transversalement ce bloc support par rapport à l'ossature, par exemple à l'aide d'une pièce 8 à excentrique d'axe vertical. La pièce 8 peut porter un pion de centrage agissant sur la charge ou être remplacée par une pièce avec crochet et bras de calage pour la suspension d'une charge à anneaux.The azimuth harmonization device of a load carried under an airplane is intended to be associated with one end of a trigger or ejector supporting the load to be released in order to ensure the desired adjustment without modifying the trigger or the ejector. One end 1 of the frame of the trigger or of the ejector receives a support block 4 from one end of the mechanism of the trigger or of the ejector and a means is provided for transversely shifting this support block with respect to the frame, for example using an eccentric part 8 with a vertical axis. The part 8 can carry a centering pin acting on the load or be replaced by a part with hook and wedging arm for the suspension of a load with rings.
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7634428A FR2370948A1 (en) | 1976-11-16 | 1976-11-16 | AZIMUT HARMONIZATION DEVICE FOR A LOAD TAKEN UNDER AIRCRAFT |
US05/850,883 US4182502A (en) | 1976-11-16 | 1977-11-14 | Device for the bearing harmonization of an airborne load |
DE19772759554 DE2759554C2 (en) | 1976-11-16 | 1977-11-15 | Centering pin for loads that can be disengaged on aircraft |
DE19772750962 DE2750962C2 (en) | 1976-11-16 | 1977-11-15 | Dropping device for a load carried under an aircraft |
GB4763577A GB1583796A (en) | 1976-11-16 | 1977-11-16 | Device for the adjustment of an airborne load |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7634428A FR2370948A1 (en) | 1976-11-16 | 1976-11-16 | AZIMUT HARMONIZATION DEVICE FOR A LOAD TAKEN UNDER AIRCRAFT |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2370948A1 true FR2370948A1 (en) | 1978-06-09 |
FR2370948B1 FR2370948B1 (en) | 1979-03-30 |
Family
ID=9179955
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7634428A Granted FR2370948A1 (en) | 1976-11-16 | 1976-11-16 | AZIMUT HARMONIZATION DEVICE FOR A LOAD TAKEN UNDER AIRCRAFT |
Country Status (3)
Country | Link |
---|---|
DE (2) | DE2759554C2 (en) |
FR (1) | FR2370948A1 (en) |
GB (1) | GB1583796A (en) |
Cited By (3)
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 |
FR2563181A1 (en) * | 1984-04-20 | 1985-10-25 | Alkan R & Cie | Adjustable mounting for aircraft carried load |
EP0745531A1 (en) * | 1995-05-31 | 1996-12-04 | AEROSPATIALE Société Nationale Industrielle | Device for anchoring a store suspended under the pylon of an aircraft |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2261173C3 (en) * | 1972-12-14 | 1979-06-13 | Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen | Device for detachable fixing |
FR2345346A1 (en) * | 1976-03-22 | 1977-10-21 | Alkan R & Cie | EJECTOR ALLOWING THE CARGO OF LOADS UNDER PLANE, WHETHER EQUIPPED WITH RINGS OR PARTS CALLED SADDLES |
-
1976
- 1976-11-16 FR FR7634428A patent/FR2370948A1/en active Granted
-
1977
- 1977-11-15 DE DE19772759554 patent/DE2759554C2/en not_active Expired
- 1977-11-15 DE DE19772750962 patent/DE2750962C2/en not_active Expired
- 1977-11-16 GB GB4763577A patent/GB1583796A/en not_active Expired
Non-Patent Citations (1)
Title |
---|
NEANT * |
Cited By (5)
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 |
FR2563181A1 (en) * | 1984-04-20 | 1985-10-25 | Alkan R & Cie | Adjustable mounting for aircraft carried load |
EP0745531A1 (en) * | 1995-05-31 | 1996-12-04 | AEROSPATIALE Société Nationale Industrielle | Device for anchoring a store suspended under the pylon of an aircraft |
FR2734785A1 (en) * | 1995-05-31 | 1996-12-06 | Aerospatiale | DEVICE FOR HANGING CARRIAGES UNDER A CARRIAGE MAT EQUIPPED WITH AN AIRCRAFT |
Also Published As
Publication number | Publication date |
---|---|
DE2750962A1 (en) | 1978-05-18 |
FR2370948B1 (en) | 1979-03-30 |
GB1583796A (en) | 1981-02-04 |
DE2750962C2 (en) | 1983-01-20 |
DE2759554C2 (en) | 1982-10-28 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |