GB130790A - Improvements in Aerofoils for Aeroplanes. - Google Patents

Improvements in Aerofoils for Aeroplanes.

Info

Publication number
GB130790A
GB130790A GB1327518A GB1327518A GB130790A GB 130790 A GB130790 A GB 130790A GB 1327518 A GB1327518 A GB 1327518A GB 1327518 A GB1327518 A GB 1327518A GB 130790 A GB130790 A GB 130790A
Authority
GB
United Kingdom
Prior art keywords
plane
pressure
ribs
supported
extending
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
GB1327518A
Inventor
Alexander Albert Holle
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 GB1327518A priority Critical patent/GB130790A/en
Publication of GB130790A publication Critical patent/GB130790A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/44—Varying camber
    • B64C3/48—Varying camber by relatively-movable parts of wing structures

Abstract

130,790. Holle, A. A. Aug. 15, 1918. Planes, construction of; balancing.-The front part of the supporting-plane of an aeroplane is made flexible within limits in relation to its main part so that the camber of the plane varies to counteract the travel of the centre of pressure as the incidence varies. Fig. 4 shows a plane in which the leading edge a is supported by springs b extending from the main spar y or from the ribs z. Stops e, which mav be adjusted during flight, limit the movement of the spring. The fabric of the forward part is supported by flexible members c, d extending from the ribs, the member d being such that it becomes more concave with upward pressure, and less concave and ultimately convex under downward pressure.
GB1327518A 1918-08-15 1918-08-15 Improvements in Aerofoils for Aeroplanes. Expired GB130790A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1327518A GB130790A (en) 1918-08-15 1918-08-15 Improvements in Aerofoils for Aeroplanes.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1327518A GB130790A (en) 1918-08-15 1918-08-15 Improvements in Aerofoils for Aeroplanes.

Publications (1)

Publication Number Publication Date
GB130790A true GB130790A (en) 1919-08-14

Family

ID=32345925

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1327518A Expired GB130790A (en) 1918-08-15 1918-08-15 Improvements in Aerofoils for Aeroplanes.

Country Status (1)

Country Link
GB (1) GB130790A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2408034A (en) * 2003-11-13 2005-05-18 Raymond Proost Variable camber aerofoil
US9896188B1 (en) * 2013-12-04 2018-02-20 The United States Of America As Represented By The Secretary Of The Air Force Variable camber adaptive compliant wing system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2408034A (en) * 2003-11-13 2005-05-18 Raymond Proost Variable camber aerofoil
US9896188B1 (en) * 2013-12-04 2018-02-20 The United States Of America As Represented By The Secretary Of The Air Force Variable camber adaptive compliant wing system

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