GB190821092A - Improvements in Air-ships. - Google Patents

Improvements in Air-ships.

Info

Publication number
GB190821092A
GB190821092A GB190821092DA GB190821092A GB 190821092 A GB190821092 A GB 190821092A GB 190821092D A GB190821092D A GB 190821092DA GB 190821092 A GB190821092 A GB 190821092A
Authority
GB
United Kingdom
Prior art keywords
horizontal
frame
boom
framework
steering
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
Albert Tribelhorn
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 GB190821092A publication Critical patent/GB190821092A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft

Landscapes

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

Abstract

21,092. Tribelhorn, A. Oct. 6. Aerial machines with aerostats; aeroplanes; framework; steering. - The framework of The framework of an aerial machine i s made in sections hinged together,so that the machine may be collapsed for transit. Frames 2, connected by rods 3, 4, form the central section to which are hinged booms 10, 11. The whole frame is braced when extended by wires extending from the free end of the boom 11 through guides in the arms 2<b> of the frame, around the free end of the boom 10, and back to the boom 11. Horizontal planes are arranged at the sides of the central section and are supported by arms 19 hinged to the frame 2. When the aerostat is deflated, the tension wires are relaxed, and the planes, the aerostat, and the booms 10, 11 are folded over the central frame. A box rudder 29<a> rotatable about both horizontal and vertical axes is provided for steering the machine. The horizontal spindle 24 carrying the rudder is turned by cords passing over pulleys 25 and the spindle is mounted in a cross-head carried by a vertical spindle 23, which is turned for horizontal steering by cords passing over a pulley 27.
GB190821092D 1908-10-06 1908-10-06 Improvements in Air-ships. Expired GB190821092A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB190821092T 1908-10-06

Publications (1)

Publication Number Publication Date
GB190821092A true GB190821092A (en) 1909-03-11

Family

ID=32439008

Family Applications (2)

Application Number Title Priority Date Filing Date
GB190821092D Expired GB190821092A (en) 1908-10-06 1908-10-06 Improvements in Air-ships.
GB190902741D Expired GB190902741A (en) 1908-10-06 1909-02-04 Improvements in Air Ships.

Family Applications After (1)

Application Number Title Priority Date Filing Date
GB190902741D Expired GB190902741A (en) 1908-10-06 1909-02-04 Improvements in Air Ships.

Country Status (1)

Country Link
GB (2) GB190821092A (en)

Also Published As

Publication number Publication date
GB190902741A (en) 1909-06-10

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