GB165223A - Improvements in means for stopping way on aircraft - Google Patents
Improvements in means for stopping way on aircraftInfo
- Publication number
- GB165223A GB165223A GB8729/20A GB872920A GB165223A GB 165223 A GB165223 A GB 165223A GB 8729/20 A GB8729/20 A GB 8729/20A GB 872920 A GB872920 A GB 872920A GB 165223 A GB165223 A GB 165223A
- Authority
- GB
- United Kingdom
- Prior art keywords
- chamber
- board
- sides
- blocks
- collapsable
- 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
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
- B64D17/00—Parachutes
- B64D17/78—Parachutes in association with other load-retarding apparatus
Abstract
165,223. Denson, J. D. March 24, 1920. Stopping way; planes, construction of; steering, balancing, and regulating altitude.-An aeroplane is fitted at its tail with a collapsable chamber, the mouth of which can be opened to admit air to retard a forward or diving movement; and the fincarrying board forming the top of the chamber can be elevated about its forward end without opening the chamber, to prevent nose diving. The board 42 carries a fin 48, and is connected to the sides and rear of the tail 11 of the machine bv fabric 43 which forms the sides of the collapsable chamber. The mouth of the chamber can be opened by raising the front portion of the board 42 by a hand-lever 44 which is connected to the board by links and levers 46, 45, 40, 40<1>. The rear end of the board can be raised to varying extents by sliding the fulcrum blocks 32<11> along its under surface. These blocks are carried by a sliding rod 32, pivoted to a rod 31 which is connected to the upper crank 29 on a shaft 28. By pressing upon one or other of the pedals 38, which are connected respectively to the upper and lower cranks 29, the fulcrum blocks 32<11> can be moved backwards or forwards. A hand-lever 27 is linked to a transverse shaft 23 carrying cranks at its ends for raising or lowering the rear ends of narrow longitudinallyextending planes pivoted near their front ends to the sides of the fuselage.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8729/20A GB165223A (en) | 1920-03-24 | 1920-03-24 | Improvements in means for stopping way on aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8729/20A GB165223A (en) | 1920-03-24 | 1920-03-24 | Improvements in means for stopping way on aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB165223A true GB165223A (en) | 1921-06-24 |
Family
ID=9858121
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8729/20A Expired GB165223A (en) | 1920-03-24 | 1920-03-24 | Improvements in means for stopping way on aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB165223A (en) |
-
1920
- 1920-03-24 GB GB8729/20A patent/GB165223A/en not_active Expired
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