GB921267A - Improvements in dirigible craft - Google Patents

Improvements in dirigible craft

Info

Publication number
GB921267A
GB921267A GB3795360A GB3795360A GB921267A GB 921267 A GB921267 A GB 921267A GB 3795360 A GB3795360 A GB 3795360A GB 3795360 A GB3795360 A GB 3795360A GB 921267 A GB921267 A GB 921267A
Authority
GB
United Kingdom
Prior art keywords
vehicle
airscrew
action
centre line
airscrews
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
GB3795360A
Inventor
Arthur Philip Glenny
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.)
Sperry Gyroscope Co Ltd
Original Assignee
Sperry Gyroscope Co Ltd
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 Sperry Gyroscope Co Ltd filed Critical Sperry Gyroscope Co Ltd
Priority to GB3795360A priority Critical patent/GB921267A/en
Publication of GB921267A publication Critical patent/GB921267A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60VAIR-CUSHION VEHICLES
    • B60V1/00Air-cushion
    • B60V1/14Propulsion; Control thereof

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Steering Control In Accordance With Driving Conditions (AREA)
  • Steering-Linkage Mechanisms And Four-Wheel Steering (AREA)

Abstract

921,267. Vehicles supported by gaseous cushions. SPERRY GYROSCOPE CO. Ltd. Jan. 12, 1962 [Nov. 4, 1960], No. 37953/60. Class 4. A vehicle supported over land or water by a gaseous cushion, and propelled and manoeuvred by at least two devices each exerting a reversible horizontal thrust at a height above the cushion, the lines of action of the devices being rotatable in azimuth, is provided with means which, when the thrust reversing mechanism of a device is operated in a sense to brake the vehicle, rotates the line of action of that device so as to eliminate any athwartships component of force in a sense opposite to that of any athwartships component of force exerted immediately prior to the reversal of the thrust. Fig. 1 shows such a vehicle propelled and steered by two airscrews 2, 3, rotatable about vertical axes 7, 8. The vehicle is executing a right hand turn along a path 16, the thrust vectors of the airscrews being represented at 9 and 10 and giving rise to an appropriate nett lateral (centripetal) force and yawing torque. If now the thrusts of the airscrews are reversed by blade pitch reversal, the resultant lateral force and yawing torque will cause the vehicle to execute a left hand turn while decelerating, which is in general undesirable, especially if braking is desired in an emergency. To obviate this, blade pitch reversal of the airscrews is accompanied by rotation about axes 6 and 7, at least until the lines of action are parallel to the fore-and-aft centre line of the vehicle. Rotation of the lines of action may continue until they make the same angles with the centre line as before, or until they make lesser but proportional angles with the centre line. Fig. 3 shows apparatus for effecting this rotation for one airscrew, the apparatus for the other being similar. The line of action of the airscrew is rotatable by a motor 25 controlled by amplifier 26, which has two inputs, one from a potentiometer 21 driven by a manual steering control 24, and the other from a potentiometer 27 driven by motor 25, so that the motor shaft position is driven into correspondence with the setting of control 24. In one mode of operation, movement of the airscrew pitch control 34 to a reverse pitch setting operates switch 33 to ground one input of amplifier 26 so that motor 25 is driven to its neutral position, thus eliminating any lateral force on the vehicle. The pilot may disengage switch 33 from the pitch control 34 to resume steering control. In another mode of operation, switch 33 is omitted, and movement of control 34 to a reverse pitch setting moves switches 35 and 36 to make their upper contacts. This reverses the polarity of the voltage across potentiometer 27, so that the airscrew axis will be rotated from its instant position until it is parallel to the vehicle centre line, and then on again through the same angle. In a third mode of operation, switches 35 and 36 make their lower contacts which reverses the polarity of the voltage across potentiometer 27 and increases this voltage by cutting out series resistors 39, 40. The airscrew axis will therefore be rotated from its instant position until parallel to the centre line and then on again through a smaller angle. The airscrew engines are those driving the fans which generate the air cushion. According to the Provisional Specification, an airscrew and its engine may be in a rotatable unit.
GB3795360A 1960-11-04 1960-11-04 Improvements in dirigible craft Expired GB921267A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3795360A GB921267A (en) 1960-11-04 1960-11-04 Improvements in dirigible craft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3795360A GB921267A (en) 1960-11-04 1960-11-04 Improvements in dirigible craft

Publications (1)

Publication Number Publication Date
GB921267A true GB921267A (en) 1963-03-20

Family

ID=10400190

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3795360A Expired GB921267A (en) 1960-11-04 1960-11-04 Improvements in dirigible craft

Country Status (1)

Country Link
GB (1) GB921267A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3827527A (en) * 1968-11-29 1974-08-06 W Bertelsen Gimbal ground effect vehicles
US11066059B2 (en) * 2017-04-26 2021-07-20 Asko Hakala System for controlling an air cushion vehicle by propeller towers and a propeller tower

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3827527A (en) * 1968-11-29 1974-08-06 W Bertelsen Gimbal ground effect vehicles
US11066059B2 (en) * 2017-04-26 2021-07-20 Asko Hakala System for controlling an air cushion vehicle by propeller towers and a propeller tower

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