GB524032A - Improvements in or relating to aerodynamic means for braking aircraft - Google Patents
Improvements in or relating to aerodynamic means for braking aircraftInfo
- Publication number
- GB524032A GB524032A GB1938/39A GB193839A GB524032A GB 524032 A GB524032 A GB 524032A GB 1938/39 A GB1938/39 A GB 1938/39A GB 193839 A GB193839 A GB 193839A GB 524032 A GB524032 A GB 524032A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- members
- relating
- jan
- aerodynamic means
- 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
- 230000009977 dual effect Effects 0.000 abstract 1
- 238000007689 inspection Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWERÂ PLANTSÂ 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)
- Tires In General (AREA)
Abstract
524,032. Controlling aircraft. DORNIERWERKE GES., and DORNIER, C. Jan. 19, 1939, No. 1938. Convention date, Jan. 31, 1938. [Class 4] In an aircraft provided with dual rudder units 3, 5 and 2, 4, brake members 6, 7 adapted to be extended or retracted from the interior of the aircraft, are mounted on the upper and lower sides of the fuselage and between the rudder units. The members 6, 7 are provided with air slots as shown or with circular holes. According to the Specification as open to inspection under Sect. 91 the members may be operated independably or simultaneously. This subject-matter does not appear in the Specification as accepted.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE524032X | 1938-01-31 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB524032A true GB524032A (en) | 1940-07-29 |
Family
ID=6552150
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1938/39A Expired GB524032A (en) | 1938-01-31 | 1939-01-19 | Improvements in or relating to aerodynamic means for braking aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB524032A (en) |
-
1939
- 1939-01-19 GB GB1938/39A patent/GB524032A/en not_active Expired
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