Vector tension device and vector tension control method for vertical take-off and landing unmanned aerial vehicle
A tension device and vertical take-off and landing technology, which is applied in the direction of vertical take-off and landing aircraft, power device on the aircraft, power device arrangement/installation, etc.
Pending Publication Date: 2017-07-07
HEBEI UNIV OF TECH +1
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Abstract
The invention relates to a vector tension device which comprises a swing type engine seat 51, a fixed type engine seat 53, a supporting seat connection optical shaft 56, flange bearings 57, a control steering gear 54, a ball head connecting smooth shaft 55, a ball head pulling rod 52, a first ball head 59 and a second ball head 58. The control steering gear 54 is fixed on the fixed type engine seat 53; the supporting seat connection smooth shaft 56 is connected on the fixed type engine seat 53 through the flange bearings 57; the swing type engine seat 51 is arranged on the supporting seat connection smooth shaft 56; the first ball head 59 is fixed on the side edge of the swing type engine seat 51 through the ball head connecting smooth shaft 55; the second ball head 58 is fixed on a steering gear rocker arm of the control steering gear 54; and the two ball heads are in rigid connection through the ball head pulling rod 52. The invention provides a vector tension control method for the vertical take-off and landing unmanned aerial vehicle through the vector tension device.
Application Domain
Power plant constructionVertical landing/take-off aircrafts +1
Technology Topic
Rocker armTension control +3
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