GB144332A - An improved apparatus for increasing the range of speed of aeroplanes - Google Patents

An improved apparatus for increasing the range of speed of aeroplanes

Info

Publication number
GB144332A
GB144332A GB18037/18A GB1803718A GB144332A GB 144332 A GB144332 A GB 144332A GB 18037/18 A GB18037/18 A GB 18037/18A GB 1803718 A GB1803718 A GB 1803718A GB 144332 A GB144332 A GB 144332A
Authority
GB
United Kingdom
Prior art keywords
aeroplanes
increasing
speed
range
improved apparatus
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
GB18037/18A
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.)
Societe des Moteurs Salmson
Original Assignee
Societe des Moteurs Salmson
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 Societe des Moteurs Salmson filed Critical Societe des Moteurs Salmson
Publication of GB144332A publication Critical patent/GB144332A/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
    • B64C3/50—Varying camber by leading or trailing edge flaps

Landscapes

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

Abstract

144,332. Soc. des Moteurs Salmson, (SystÞme Canton-UnnÚ). Aug. 11, 1917, [Convention date]. Steering and balancing.-The main aerofoils b have pivoted to their rear edges both ailerons g, which are moved in opposite directions for lateral stability, and wings d which are moved together in the same direction to constitute a trailing edge for the aerofoil. The mechanism for operating the wings d is entirely independent of the mechanism for operating the ailerons g.
GB18037/18A 1917-08-11 1918-11-04 An improved apparatus for increasing the range of speed of aeroplanes Expired GB144332A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR144332X 1917-08-11

Publications (1)

Publication Number Publication Date
GB144332A true GB144332A (en) 1920-06-17

Family

ID=8874986

Family Applications (1)

Application Number Title Priority Date Filing Date
GB18037/18A Expired GB144332A (en) 1917-08-11 1918-11-04 An improved apparatus for increasing the range of speed of aeroplanes

Country Status (1)

Country Link
GB (1) GB144332A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3223356A (en) * 1963-03-06 1965-12-14 Alvarez-Calderon Alberto Deflected slipstream system for aircraft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3223356A (en) * 1963-03-06 1965-12-14 Alvarez-Calderon Alberto Deflected slipstream system for aircraft

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