GB151133A - Improvements in hinges for the control surfaces of aircraft - Google Patents

Improvements in hinges for the control surfaces of aircraft

Info

Publication number
GB151133A
GB151133A GB1832819A GB1832819A GB151133A GB 151133 A GB151133 A GB 151133A GB 1832819 A GB1832819 A GB 1832819A GB 1832819 A GB1832819 A GB 1832819A GB 151133 A GB151133 A GB 151133A
Authority
GB
United Kingdom
Prior art keywords
hinges
aircraft
control surfaces
gap
faces
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
GB1832819A
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.)
SIDDELEY DEASY MOTOR CAR COMPA
Original Assignee
SIDDELEY DEASY MOTOR CAR COMPA
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 SIDDELEY DEASY MOTOR CAR COMPA filed Critical SIDDELEY DEASY MOTOR CAR COMPA
Priority to GB1832819A priority Critical patent/GB151133A/en
Publication of GB151133A publication Critical patent/GB151133A/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

151,133. Armstrong Siddeley Motors, Ltd., and Farren, W. S. July 23, 1919. Double hinges for control surfaces of aircraft, comprising hinging-strips arranged in pairs so that the movable surface can pivot about either edge, are formed in three parts consisting of a link A, preferably of strip material, and two anchor plates A<2>, A<3> connected together by removable hinge pins A<4>. The parts may be formed of relatively thin metal to reduce the gap at the joint. The gap may be further reduced by recessing the meeting faces to receive the hinges, or an equivalent result may be obtained by attaching projecting lips B<5>, C<5> along the edges of the faces.
GB1832819A 1919-07-23 1919-07-23 Improvements in hinges for the control surfaces of aircraft Expired GB151133A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1832819A GB151133A (en) 1919-07-23 1919-07-23 Improvements in hinges for the control surfaces of aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1832819A GB151133A (en) 1919-07-23 1919-07-23 Improvements in hinges for the control surfaces of aircraft

Publications (1)

Publication Number Publication Date
GB151133A true GB151133A (en) 1920-09-23

Family

ID=10110574

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1832819A Expired GB151133A (en) 1919-07-23 1919-07-23 Improvements in hinges for the control surfaces of aircraft

Country Status (1)

Country Link
GB (1) GB151133A (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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