GB191103120A - Improvements in Aeroplanes. - Google Patents

Improvements in Aeroplanes.

Info

Publication number
GB191103120A
GB191103120A GB191103120DA GB191103120A GB 191103120 A GB191103120 A GB 191103120A GB 191103120D A GB191103120D A GB 191103120DA GB 191103120 A GB191103120 A GB 191103120A
Authority
GB
United Kingdom
Prior art keywords
planes
fuselage
machine
pivoted
longitudinals
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
John Griffin Hanna
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 GB191103120A publication Critical patent/GB191103120A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for

Abstract

3120. Hanna, J. G. Feb. 7. Aerial machines without aerostats; framework.-The fuselage of the machine is triangular in cross section and is constructed of longitudinals 11 the lower one of which inclines rearwardly towards the upper ones so that the extremities are in the same horizontal line. The main planes are stayed by wires 38, 39 extending respectively from the axle 36 and from the framework 40. Planes, arrangement of.-The sides of the triangular fuselage are covered in and a central pin 14 is provided. These with the rear elevator 19 which is of substantial size and the main planes 15 disposed at the dihedral angle constitute an arrangement of surfaces giving automatic stability while minimizing the tendency to rock. Steering and balancing.-Lateral steering is effected by pulling down one or other of a pair of flexible planes 31 so as to brake the machine on one side. These planes are mounted on the underside of the main planes and are operated by cords 33 and a pivoted rod 32. The planes also cause the machine to assume the lateral cant necessary when turning. The rudder 26, pivoted at 27, is employed only for maintaining a straight course. The tail-plane elevator 19 is pivoted at 20 to the extremities of the longitudinals 11 of the fuselage. It is trussed by means of a pair of struts 22 which serve also for attachment of the operating-cords.
GB191103120D 1911-02-07 1911-02-07 Improvements in Aeroplanes. Expired GB191103120A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB191103120T 1911-02-07

Publications (1)

Publication Number Publication Date
GB191103120A true GB191103120A (en) 1912-02-07

Family

ID=32496353

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191103120D Expired GB191103120A (en) 1911-02-07 1911-02-07 Improvements in Aeroplanes.

Country Status (1)

Country Link
GB (1) GB191103120A (en)

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