GB540724A - Aerodynamic devices for retarding aircraft, persons or objects in movement or for starting aircraft - Google Patents
Aerodynamic devices for retarding aircraft, persons or objects in movement or for starting aircraftInfo
- Publication number
- GB540724A GB540724A GB26604/39A GB2660439A GB540724A GB 540724 A GB540724 A GB 540724A GB 26604/39 A GB26604/39 A GB 26604/39A GB 2660439 A GB2660439 A GB 2660439A GB 540724 A GB540724 A GB 540724A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- flywheel
- parachute
- drum
- retarding
- 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.)
- Expired
Links
- 230000000979 retarding effect Effects 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
- B64D5/00—Aircraft transported by aircraft, e.g. for release or reberthing during flight
-
- 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
- B64D17/00—Parachutes
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Transmission Devices (AREA)
Abstract
540,724. Parachute apparatus. BONNEFOY, P. E. L. Sept. 25, 1939, No. 26604. Convention date, Sept. 26, 1938. [Class 4] A device for retarding aircraft, persons or objects, or for assisting the starting of an aircraft, comprises a parachute attached to a flexible member wound on a drum carried by the aeroplane &c. the unfolded parachute first unwinding the flexible member from the drum and storing up energy in a flywheel or other accumulator which is then utilised to wind in the flexible member rapidly to draw the parachute towards the aircraft &c. In one form, the parachute is attached to a flat band 6 wound upon a drum 5, and as the band unwinds a flywheel 26 is speeded up through gearing 11, 12 and a clutch 14, 16. When it is desired to retard the aircraft more strongly the flywheel 26 is clutched to the drum 5 through the gearing 21, 22, counter shaft 20, reversing gear 23, 24, 25, clutch 15, 17 and the gearing 11, 12 to wind in the band 6. The flywheel 26 may be assisted by another flywheel 44 adapted to be coupled to the flywheel 26 after being speeded up by a seaparate motor. The clutches 15, 17 and 14, 16 are actuated by a lever 32 which is coupled as shown to a locking
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR540724X | 1938-09-26 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB540724A true GB540724A (en) | 1941-10-28 |
Family
ID=8929666
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB26604/39A Expired GB540724A (en) | 1938-09-26 | 1939-09-25 | Aerodynamic devices for retarding aircraft, persons or objects in movement or for starting aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB540724A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2477907A (en) * | 1944-09-04 | 1949-08-02 | Prevost F Smith | Parachute zero speed landing motor |
US2634924A (en) * | 1946-11-01 | 1953-04-14 | Brown Owen | Means and method for conduction warfare |
US3002715A (en) * | 1958-11-04 | 1961-10-03 | Gordon R Sinclair | Deceleration parachute retraction system |
US3109615A (en) * | 1962-04-19 | 1963-11-05 | Rocket Power Inc | Ballistic actuated device for reeling in an elongated flexible element |
-
1939
- 1939-09-25 GB GB26604/39A patent/GB540724A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2477907A (en) * | 1944-09-04 | 1949-08-02 | Prevost F Smith | Parachute zero speed landing motor |
US2634924A (en) * | 1946-11-01 | 1953-04-14 | Brown Owen | Means and method for conduction warfare |
US3002715A (en) * | 1958-11-04 | 1961-10-03 | Gordon R Sinclair | Deceleration parachute retraction system |
US3109615A (en) * | 1962-04-19 | 1963-11-05 | Rocket Power Inc | Ballistic actuated device for reeling in an elongated flexible element |
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