GB143953A - Improvements in or connected with the planes of aeroplanes - Google Patents

Improvements in or connected with the planes of aeroplanes

Info

Publication number
GB143953A
GB143953A GB285919A GB285919A GB143953A GB 143953 A GB143953 A GB 143953A GB 285919 A GB285919 A GB 285919A GB 285919 A GB285919 A GB 285919A GB 143953 A GB143953 A GB 143953A
Authority
GB
United Kingdom
Prior art keywords
ailerons
plane
aileron
under
aeroplane
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
GB285919A
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.)
ETIENNE ROYER
Original Assignee
ETIENNE ROYER
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 ETIENNE ROYER filed Critical ETIENNE ROYER
Priority to GB285919A priority Critical patent/GB143953A/en
Publication of GB143953A publication Critical patent/GB143953A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Abstract

143,953. Royer, E. July 31, 1919. Steering and balancing.-The lifting effect of the planes of aeroplanes is varied by adjusting ailerons pivoted under the plane on axes parallel to, but a certain distance behind, the leading edge. These ailerons may be used in conjunction with ordinary ailerons at the rear edge for turning the aeroplane without the use of a rudder. Fig. 1 shows a hinged aileron 13 under the leading edge and operated by cords 14 attached to an arm 15 and passing over a pulley 16. In practice, these ailerons would be received in recesses under the plane when withdrawal, so as to present no projection. Turning may be effected by lowering the front aileron at one side of the aeroplane and lowering the ordinary rear aileron at the other side so as to brake the machine on the latter side. One or more front ailerons may be placed between the side ailerons 13. The rear ailerons may be arranged at an angle to the trailing edge of the plane.
GB285919A 1919-07-31 1919-07-31 Improvements in or connected with the planes of aeroplanes Expired GB143953A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB285919A GB143953A (en) 1919-07-31 1919-07-31 Improvements in or connected with the planes of aeroplanes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB285919A GB143953A (en) 1919-07-31 1919-07-31 Improvements in or connected with the planes of aeroplanes

Publications (1)

Publication Number Publication Date
GB143953A true GB143953A (en) 1920-06-10

Family

ID=9747301

Family Applications (1)

Application Number Title Priority Date Filing Date
GB285919A Expired GB143953A (en) 1919-07-31 1919-07-31 Improvements in or connected with the planes of aeroplanes

Country Status (1)

Country Link
GB (1) GB143953A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2450709A (en) * 1943-02-22 1948-10-05 Lockheed Aircraft Corp Aircraft control
US2990140A (en) * 1958-10-24 1961-06-27 Lockheed Aircraft Corp Combination gust alleviator and highlift device for aircraft

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2450709A (en) * 1943-02-22 1948-10-05 Lockheed Aircraft Corp Aircraft control
US2990140A (en) * 1958-10-24 1961-06-27 Lockheed Aircraft Corp Combination gust alleviator and highlift device for aircraft

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