GB191211493A - Aeroplane having Automatic Stability. - Google Patents

Aeroplane having Automatic Stability.

Info

Publication number
GB191211493A
GB191211493A GB191211493DA GB191211493A GB 191211493 A GB191211493 A GB 191211493A GB 191211493D A GB191211493D A GB 191211493DA GB 191211493 A GB191211493 A GB 191211493A
Authority
GB
United Kingdom
Prior art keywords
planes
steering
shaft
aeroplane
hinged
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
Georges De Bothezat
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 GB191211493A publication Critical patent/GB191211493A/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

Abstract

11,493. Bothezat, G. de. May 15, 1911, [Convention date]. Aerial machines without aerostats; steering and balancing; planes, arrangement of.-The frame A carrying the supporting-planes of an aeroplane is hinged about a transverse shaft C to the body part of the machine in order to maintain longitudinal stability. Oscillations of the body B are prevented by the provision on it fore and aft of planes I, II which have equal movements about the shaft C. The thrust F of the motor, the head resistance R of the body and the vertical line passing through the centre of gravity G<b> of the body B all pass through the shaft C. The planes I, II may be turned in opposite directions for steering vertically, or a separate elevator may be provided. A rudder for lateral steering may be provided on either or both of the parts A, B. The part A may also be hinged about a longitudinal axis and the body B provided with laterally arranged planes similar to the planes I. II in order to maintain lateral stability. A fixed tail plane q, q<1> may be fitted to the supporting plane structure A.
GB191211493D 1911-05-15 1912-05-14 Aeroplane having Automatic Stability. Expired GB191211493A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
BE191211493X 1911-05-15

Publications (1)

Publication Number Publication Date
GB191211493A true GB191211493A (en) 1913-01-30

Family

ID=32513568

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191211493D Expired GB191211493A (en) 1911-05-15 1912-05-14 Aeroplane having Automatic Stability.

Country Status (1)

Country Link
GB (1) GB191211493A (en)

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