GB477844A - Safety means for use in preventing or correcting spinning in aircraft - Google Patents

Safety means for use in preventing or correcting spinning in aircraft

Info

Publication number
GB477844A
GB477844A GB18618/36A GB1861836A GB477844A GB 477844 A GB477844 A GB 477844A GB 18618/36 A GB18618/36 A GB 18618/36A GB 1861836 A GB1861836 A GB 1861836A GB 477844 A GB477844 A GB 477844A
Authority
GB
United Kingdom
Prior art keywords
flaps
fuselage
spinning
aircraft
correcting
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
GB18618/36A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB18618/36A priority Critical patent/GB477844A/en
Publication of GB477844A publication Critical patent/GB477844A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • B64C9/34Adjustable control surfaces or members, e.g. rudders collapsing or retracting against or within other surfaces or other members
    • B64C9/36Adjustable control surfaces or members, e.g. rudders collapsing or retracting against or within other surfaces or other members the members being fuselages or nacelles
    • 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
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/30Wing lift efficiency

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Emergency Lowering Means (AREA)
  • Body Structure For Vehicles (AREA)

Abstract

477,844. Controlling aeroplanes. MARTIN, J. July 4, 1936, No. 18618. [Class 4] Means for diverting air on to the rudder of an aeroplane when the latter is at a high angle of incidence comprise flaps mounted in advance of the tail unit and normally folded flush with the fuselage but adjustable to laterally projecting positions. Flaps 2, 2, Fig. 2, are hinged longitudinally at 3 to the fuselage 1 and are normally nested against the surface or accommodated in recesses therein. The flaps are maintained in their inoperative position by cables 10 connected to a cockpit control, for instance a hand lever with pawl and ratchet locking means, and are moved outwardly by spring struts 6 when this control is released, Fig. 4.
GB18618/36A 1936-07-04 1936-07-04 Safety means for use in preventing or correcting spinning in aircraft Expired GB477844A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB18618/36A GB477844A (en) 1936-07-04 1936-07-04 Safety means for use in preventing or correcting spinning in aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB18618/36A GB477844A (en) 1936-07-04 1936-07-04 Safety means for use in preventing or correcting spinning in aircraft

Publications (1)

Publication Number Publication Date
GB477844A true GB477844A (en) 1938-01-04

Family

ID=10115538

Family Applications (1)

Application Number Title Priority Date Filing Date
GB18618/36A Expired GB477844A (en) 1936-07-04 1936-07-04 Safety means for use in preventing or correcting spinning in aircraft

Country Status (1)

Country Link
GB (1) GB477844A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3848831A (en) * 1971-10-12 1974-11-19 M Geary Fuselage flaps for an aircraft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3848831A (en) * 1971-10-12 1974-11-19 M Geary Fuselage flaps for an aircraft

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