GB206562A - Improvements in planes for aircraft - Google Patents

Improvements in planes for aircraft

Info

Publication number
GB206562A
GB206562A GB2112222A GB2112222A GB206562A GB 206562 A GB206562 A GB 206562A GB 2112222 A GB2112222 A GB 2112222A GB 2112222 A GB2112222 A GB 2112222A GB 206562 A GB206562 A GB 206562A
Authority
GB
United Kingdom
Prior art keywords
planes
hinges
hinged
plane
forward portion
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
GB2112222A
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.)
English Electric Co Ltd
Original Assignee
English Electric Co Ltd
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 English Electric Co Ltd filed Critical English Electric Co Ltd
Priority to GB2112222A priority Critical patent/GB206562A/en
Publication of GB206562A publication Critical patent/GB206562A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/02—Mounting or supporting thereof

Abstract

206,562. English Electric Co., Ltd., and Manning, W. O. Aug. 2, 1922. Planes and the like, construction of; steering, balancing, and regulating altitude.-In planes in which a rear portion, such as an aileron 2, is hinged to a forward portion 1, the hinges 11 are located at or near the upper surface of the plane, and a metal flap 13, hinged to the lower surface of the forward portion 1. is held by the air-pressure alone, cr in combination with a spring across the V-shaped gap 12 formed between the two portions. The fabric covering the upper surface of the plane may be placed over the hinges 11.
GB2112222A 1922-08-02 1922-08-02 Improvements in planes for aircraft Expired GB206562A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2112222A GB206562A (en) 1922-08-02 1922-08-02 Improvements in planes for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2112222A GB206562A (en) 1922-08-02 1922-08-02 Improvements in planes for aircraft

Publications (1)

Publication Number Publication Date
GB206562A true GB206562A (en) 1923-11-02

Family

ID=10157555

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2112222A Expired GB206562A (en) 1922-08-02 1922-08-02 Improvements in planes for aircraft

Country Status (1)

Country Link
GB (1) GB206562A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2576279A1 (en) * 1985-01-21 1986-07-25 Metz Jean Francois Light aircraft comprising two half-wings made of composite materials

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2576279A1 (en) * 1985-01-21 1986-07-25 Metz Jean Francois Light aircraft comprising two half-wings made of composite materials

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