GB249675A - Improvements in or relating to the tail control surfaces of aeroplanes and like aircraft - Google Patents

Improvements in or relating to the tail control surfaces of aeroplanes and like aircraft

Info

Publication number
GB249675A
GB249675A GB790425A GB790425A GB249675A GB 249675 A GB249675 A GB 249675A GB 790425 A GB790425 A GB 790425A GB 790425 A GB790425 A GB 790425A GB 249675 A GB249675 A GB 249675A
Authority
GB
United Kingdom
Prior art keywords
rudder
aircraft
plane
aeroplanes
relating
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
GB790425A
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 GB790425A priority Critical patent/GB249675A/en
Publication of GB249675A publication Critical patent/GB249675A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/02—Tailplanes

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)

Abstract

249,675. Chick, A. G., and Ordidge, F. H. March 24, 1925. Planes, construction of; steering and balancing. -An aeroplane or like aircraft having a vertical pin h extending forwardly from the rudder over a tail plane d which is pivoted about a transverse axis e towards its leading edge, has the rear edge k of the fin and the contiguous forward edge m of the rudder curved concentrically about the transverse axis e. The pin h is preferably carried by and rigidly braced to both spars of the plane d so as to move therewith. The plane d is moved by a screw shaft f which moves axially in a rotary nut g controlled by the pilot. The rudder has an extension j forward of its pivotal axis c. The invention may be used in conjunction with that described in Specification 217,031.
GB790425A 1925-03-24 1925-03-24 Improvements in or relating to the tail control surfaces of aeroplanes and like aircraft Expired GB249675A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB790425A GB249675A (en) 1925-03-24 1925-03-24 Improvements in or relating to the tail control surfaces of aeroplanes and like aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB790425A GB249675A (en) 1925-03-24 1925-03-24 Improvements in or relating to the tail control surfaces of aeroplanes and like aircraft

Publications (1)

Publication Number Publication Date
GB249675A true GB249675A (en) 1926-04-01

Family

ID=9842021

Family Applications (1)

Application Number Title Priority Date Filing Date
GB790425A Expired GB249675A (en) 1925-03-24 1925-03-24 Improvements in or relating to the tail control surfaces of aeroplanes and like aircraft

Country Status (1)

Country Link
GB (1) GB249675A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2744698A (en) * 1949-03-11 1956-05-08 Baynes Aircraft Interiors Ltd High speed aircraft wing and tail surfaces having variable sweepback
WO2015053838A1 (en) * 2013-07-22 2015-04-16 Learjet Inc. Tailplane with positive camber

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2744698A (en) * 1949-03-11 1956-05-08 Baynes Aircraft Interiors Ltd High speed aircraft wing and tail surfaces having variable sweepback
WO2015053838A1 (en) * 2013-07-22 2015-04-16 Learjet Inc. Tailplane with positive camber
CN105408205A (en) * 2013-07-22 2016-03-16 里尔喷射机公司 Tailplane with positive camber
US9873503B2 (en) 2013-07-22 2018-01-23 Learjet Inc. Tailplane with positive camber
CN105408205B (en) * 2013-07-22 2020-07-03 里尔喷射机公司 Horizontal rear wing with positive camber

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