GB190907349A - Mono-aeroplane. - Google Patents

Mono-aeroplane.

Info

Publication number
GB190907349A
GB190907349A GB190907349DA GB190907349A GB 190907349 A GB190907349 A GB 190907349A GB 190907349D A GB190907349D A GB 190907349DA GB 190907349 A GB190907349 A GB 190907349A
Authority
GB
United Kingdom
Prior art keywords
plane
frame
pivot
planes
pivoted
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
Emmanuel Roche
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 GB190907349A publication Critical patent/GB190907349A/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
    • B64C3/385—Variable incidence wings

Landscapes

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

Abstract

7349. Roche, E. March 27. Aerial machines without aerostats; planes, arrangement of; steering and balancing.-An aerial machine comprises a forward triangular plane a pivoted to the frame c for vertical steering, a fixed plane e, and a rear adjustable plane j, for ensuring stability, pivoted to a frame h<1>, which is hinged in turn to the plane e. The planes a, e are provided with keel planes d, f, and a vertical rudder g is hinged to the plane f. The rear plane j is adapted to be rotated in its own plane about the pivot i on the frame h<1>, and its horizontal inclination can be varied by turning the frame h<1> relatively to the plane e. The plane j is guided in its movement about the pivot i by guides k, which embrace the frame h<1>. In a modification, the plane j is arranged to turn about its horizontal axis by means of the pivot n, Fig. 7, passing through the frame h<1>.
GB190907349D 1909-03-27 1909-03-27 Mono-aeroplane. Expired GB190907349A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB190907349T 1909-03-27

Publications (1)

Publication Number Publication Date
GB190907349A true GB190907349A (en) 1909-09-30

Family

ID=32443094

Family Applications (1)

Application Number Title Priority Date Filing Date
GB190907349D Expired GB190907349A (en) 1909-03-27 1909-03-27 Mono-aeroplane.

Country Status (1)

Country Link
GB (1) GB190907349A (en)

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