GB524032A - Improvements in or relating to aerodynamic means for braking aircraft - Google Patents

Improvements in or relating to aerodynamic means for braking aircraft

Info

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
Application number
GB1938/39A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Dornier Werke GmbH
Original Assignee
Dornier Werke GmbH
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Dornier Werke GmbH filed Critical Dornier Werke GmbH
Publication of GB524032A publication Critical patent/GB524032A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/023Aircraft 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.
GB1938/39A 1938-01-31 1939-01-19 Improvements in or relating to aerodynamic means for braking aircraft Expired GB524032A (en)

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)

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