GB191200483A - Improvements in or relating to Airships or Aeroplanes or the like. - Google Patents

Improvements in or relating to Airships or Aeroplanes or the like.

Info

Publication number
GB191200483A
GB191200483A GB191200483DA GB191200483A GB 191200483 A GB191200483 A GB 191200483A GB 191200483D A GB191200483D A GB 191200483DA GB 191200483 A GB191200483 A GB 191200483A
Authority
GB
United Kingdom
Prior art keywords
propellers
cam
adjusted
rotating
moved
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
William Jacob Wilson
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 GB191200483A publication Critical patent/GB191200483A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C17/00Aircraft stabilisation not otherwise provided for

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)
  • Toys (AREA)

Abstract

483. Wilson, W. J. July 5. Propelling; balancing.-Air-ships, aeroplanes, &c. are balanced by the manual or automatic alteration of the pitch of single or twin propellers Fig. 1 shows one arrangement, in which the propeller blades are connected each to a rod d<4> connected to the rotatable collar d and to a rod e<4> mounted on a rotatable and slidable part e<2>. The sleeves e<2> are moved in the same direction, when an oppositely screwed sleeve g' is rotated, through bell-crank levers f and links e<3>. The collars d are connected through bevelgearing c, c<1> to the motor-driven shaft b, and the propeller blades are normally in the neutral position. When the sleeves e<2> are moved similarly, the two propellers tend to lift or depress the part of the machine to which they are secured. By the movement of the sleeve g<1> as a whole to either side, brought about manually through a lever i or automatically by a weight attached to the lever i as when the machine tilts, the propellers are differentially adjusted. As shown in Fig. 2, the propellers are adjusted through cams j pivoted at k, k<1> on which axes pinions are fixed meshing with a rack k<2>. By rotating a wheel l on the axis k, the pins f<3> on the bell-crank levers fare both moved outwards or inwards due to their movement in the cam-slots j<1>, and the propellers are similarly adjusted. The rack k<2> is connected through a pin m<2> which fits in a camslot m<1> with the manually or gravitationally operable cam m, so that the rack and cams j may be moved bodily in order to adjust the propellers differentially. In a further form, Fig. 3, the collar d is adjusted relatively to the seeve e<2> by means of cams p connected by a link r. Endlong movement of the link r through the cam q, brought about by hand or by a weight s<2>, alters the propeller blades similarly. A single propeller, operated as shown in Fig. 3, by a cam p and with a weight attached to the part p<2>, may be placed at the front or rear of the machine. A vertically rotating single propeller rotating about a transverse axis may be placed at each side of the machine above the centre of gravity and be operated by a weightcontrolled cam p. In all cases, the propellers are normally rotating in the neutral position.
GB191200483D 1912-07-05 1912-07-05 Improvements in or relating to Airships or Aeroplanes or the like. Expired GB191200483A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB191200483T 1912-07-05

Publications (1)

Publication Number Publication Date
GB191200483A true GB191200483A (en) 1913-04-10

Family

ID=32367250

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191200483D Expired GB191200483A (en) 1912-07-05 1912-07-05 Improvements in or relating to Airships or Aeroplanes or the like.

Country Status (1)

Country Link
GB (1) GB191200483A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2521806A (en) * 1946-10-02 1950-09-12 Alfred I Roman Differential propeller control

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2521806A (en) * 1946-10-02 1950-09-12 Alfred I Roman Differential propeller control

Similar Documents

Publication Publication Date Title
US2058678A (en) Flying machine
US1710670A (en) Tttbix of said leonard w
US1994488A (en) Direct lift aircraft
US1641567A (en) Aircraft-motor-control system
GB191200483A (en) Improvements in or relating to Airships or Aeroplanes or the like.
US1959270A (en) Aeroplane
US2023334A (en) Aeroplane
US1832254A (en) Airplane
US2271509A (en) Lateral control means for flying machines with pivoted wings
US1813485A (en) Controlling means for aeroplanes
US2015150A (en) Aircraft
US1940108A (en) Flying machine
US1849766A (en) Airplane
US1714170A (en) Flying machine
US1974040A (en) Aeroplane
GB299212A (en) Improvements in aeroplanes with stabilisation surfaces
US1906018A (en) Airplane
US1886932A (en) Airplane
US1906443A (en) Aviator training or amusement device
US1705904A (en) Aeroplane
US1070972A (en) Flying-machine.
US1987607A (en) Hovering airplane mechanism
US1024670A (en) Flying-machine.
US1891812A (en) Airplane
US1068652A (en) Flying-machine.