GB191002611A - Improvements in or relating to the Construction of Aeroplanes. - Google Patents

Improvements in or relating to the Construction of Aeroplanes.

Info

Publication number
GB191002611A
GB191002611A GB191002611DA GB191002611A GB 191002611 A GB191002611 A GB 191002611A GB 191002611D A GB191002611D A GB 191002611DA GB 191002611 A GB191002611 A GB 191002611A
Authority
GB
United Kingdom
Prior art keywords
fabric
frame
edge
plane
short
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
Horace Leonard Short
Albert Eustace Short
Hugh Oswald Short
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 GB191002611A publication Critical patent/GB191002611A/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

2611. Short, H. L., Short, A. E., and Short, H. O. Feb. 2. Planes, construction of; steering and balancing. - Supporting, steering, and balancing planes used on flying-machines are constructed so that the plane is practically flat when passing through the air without any inclination, while when it is placed at an angle to the direction of motion its surface becomes curved. A lateral balancing-plane is shown in Fig. 1 and is constructed of a rigid frame to the leading edge 1 of which a sheet of fabric 4 is firmly fixed. The rear edge of the fabric is connected directly, or through the intermediary of a bar 5, by means of springs 6 to the rear member 2 of the frame. The springs tend to keep the fabric flat but allow it to become curved when the frame becomes inclined to the direction of motion. The fabric, in an alternative arrangement, may be connected to a spring roller at the leading or rear end of the frame, the other edge of the fabric being fixed to the frame, and part or all of the fabric may be elastic. Another modification is shown in Fig. 7, in which the plane 4 passes over a roller 10, the free edge being connected to the fabric through the springs 11. The fabric may be provided with tapered flexible ribs 7, Fig. 1, of the kind described in Specification 23,166/09.
GB191002611D 1910-02-02 1910-02-02 Improvements in or relating to the Construction of Aeroplanes. Expired GB191002611A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB191002611T 1910-02-02

Publications (1)

Publication Number Publication Date
GB191002611A true GB191002611A (en) 1910-05-19

Family

ID=32560304

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191002611D Expired GB191002611A (en) 1910-02-02 1910-02-02 Improvements in or relating to the Construction of Aeroplanes.

Country Status (1)

Country Link
GB (1) GB191002611A (en)

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