GB112775A - Improvements in Means for Stopping Way or Maintaining the Equilibrium of Aeroplanes. - Google Patents
Improvements in Means for Stopping Way or Maintaining the Equilibrium of Aeroplanes.Info
- Publication number
- GB112775A GB112775A GB122/18A GB12218A GB112775A GB 112775 A GB112775 A GB 112775A GB 122/18 A GB122/18 A GB 122/18A GB 12218 A GB12218 A GB 12218A GB 112775 A GB112775 A GB 112775A
- Authority
- GB
- United Kingdom
- Prior art keywords
- planes
- aeroplanes
- equilibrium
- maintaining
- stopping way
- 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; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/023—Aircraft characterised by the type or position of power plants of rocket type, e.g. for assisting taking-off or braking
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
112,775. Maiche, C. Jan. 26, 1916, [Convention date]. Planes, arrangement of; stopping way; parachutes.-A braking-device for aerial machines comprises a series of planes arranged behind the tail-plane and adapted for use also to counteract the sinking of the nose of the machine or, in the case of a nose-dive, to have a parachute action. Fig. 1 shows a series of planes b<1>, b<2> arranged behind the tail-plane and serving as auxiliary supporting-planes, but capable of being adjusted to the position shown in Fig. 3 to act as a brake. The planes are adjusted in pairs, in opposite directions by means of bars c', c<2> actuated by connexions c<o>, f, e.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR112775X | 1916-01-26 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB112775A true GB112775A (en) | 1919-01-02 |
Family
ID=32242011
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB122/18A Expired GB112775A (en) | 1916-01-26 | 1918-01-02 | Improvements in Means for Stopping Way or Maintaining the Equilibrium of Aeroplanes. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB112775A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2559823A (en) * | 1945-04-09 | 1951-07-10 | Northrop Aircraft Inc | Rudder for tailless airplanes |
-
1918
- 1918-01-02 GB GB122/18A patent/GB112775A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2559823A (en) * | 1945-04-09 | 1951-07-10 | Northrop Aircraft Inc | Rudder for tailless airplanes |
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