GB191121248A - Improvements in Balancing Devices for Aeroplanes and the like. - Google Patents

Improvements in Balancing Devices for Aeroplanes and the like.

Info

Publication number
GB191121248A
GB191121248A GB191121248DA GB191121248A GB 191121248 A GB191121248 A GB 191121248A GB 191121248D A GB191121248D A GB 191121248DA GB 191121248 A GB191121248 A GB 191121248A
Authority
GB
United Kingdom
Prior art keywords
planes
balancing
aeroplanes
extremities
balancing devices
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
Boleslas Bronislawski
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 GB191121248A publication Critical patent/GB191121248A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers

Abstract

21,248. Bronislawski, B. Oct. 1, 1910, [Convention date]. Steering and balancing. - Aeroplanes are balanced laterally and longitudinally bv inclined auxiliary planes a, b rotatable about vertical axes c and operated by a universally-mounted hand-lever F through links G, H. The balancing-planes are mounted at the extremities of the main and tail planes A, E of a monoplane. The Specification as open to inspection under Section 91(3) (a) comprises also an arrangement in which separately adjustable balancing-planes, such as the planes a, b, are carried at the extremities of front and rear transverse beams extending from the body of the aeroplane, and states that the invention is applicable also to dirigible balloons. This subject-matter does not appear in the Specification as accepted.
GB191121248D 1910-10-01 1911-09-26 Improvements in Balancing Devices for Aeroplanes and the like. Expired GB191121248A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR191121248X 1910-10-01

Publications (1)

Publication Number Publication Date
GB191121248A true GB191121248A (en) 1912-02-08

Family

ID=32525949

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191121248D Expired GB191121248A (en) 1910-10-01 1911-09-26 Improvements in Balancing Devices for Aeroplanes and the like.

Country Status (1)

Country Link
GB (1) GB191121248A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2744154A (en) * 1953-05-18 1956-05-01 Arthur W Ludwig Insulated fence post
US5004211A (en) * 1988-08-26 1991-04-02 Ernest Rayner Fence dropper

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2744154A (en) * 1953-05-18 1956-05-01 Arthur W Ludwig Insulated fence post
US5004211A (en) * 1988-08-26 1991-04-02 Ernest Rayner Fence dropper

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