GB191213855A - Improvements in an Aeroplane with Automatic Longitudinal Balancing. - Google Patents

Improvements in an Aeroplane with Automatic Longitudinal Balancing.

Info

Publication number
GB191213855A
GB191213855A GB191213855DA GB191213855A GB 191213855 A GB191213855 A GB 191213855A GB 191213855D A GB191213855D A GB 191213855DA GB 191213855 A GB191213855 A GB 191213855A
Authority
GB
United Kingdom
Prior art keywords
planes
balancing
aeroplane
frame
cords
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
Inventor
Emile Ande Dandrieux
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
Application granted granted Critical
Publication of GB191213855A publication Critical patent/GB191213855A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C17/00—Aircraft stabilisation not otherwise provided for

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Forklifts And Lifting Vehicles (AREA)

Abstract

13,855. Dandrieux, E. A. June 14, 1911, [Convention date]. Aerial machines without aerostats; planes, arrangement and construction of; balancing.- The body 3 of an aeroplane is pivoted at its rear end to a rectangular frame A carrying the main planes, and the front end is movable vertically on guides 5, 6 and is supported by chains and ropes passing over pulleys M, M<1> and connected to a tension spring O having its end secured to the rear end of the frame A. The supporting-planes comprise a semicircular plane B, B<1> fixed to the frame, and laterallyextending planes G, G' which are pivoted about vertical axes H, H<1> so as to be movable forwards and rearwards to modify the relative positions of the centre of gravity and centre of pressure for balancing. The movements of the planes G, G<1> are controlled by the cords P, P<1> supporting the body 3, which are attached to levers N, N' secured to the inner end of the planes. The planes B, B<1>, G, G<1> are stayed by cords.
GB191213855D 1911-06-14 1912-06-13 Improvements in an Aeroplane with Automatic Longitudinal Balancing. Expired GB191213855A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
BE191213855X 1911-06-14

Publications (1)

Publication Number Publication Date
GB191213855A true GB191213855A (en) 1913-01-09

Family

ID=32601734

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191213855D Expired GB191213855A (en) 1911-06-14 1912-06-13 Improvements in an Aeroplane with Automatic Longitudinal Balancing.

Country Status (1)

Country Link
GB (1) GB191213855A (en)

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