Manned/unmanned multipurpose aircraft with dual-mode taking off and landing

A dual-mode, multi-purpose technology, applied in the aviation field, can solve the problems of complex conversion mechanism, poor balance ability, and small resistance of fixed wings, etc., and achieve the effect of high safety factor of aircraft occupants, good stability, and high flight speed

Inactive Publication Date: 2017-07-04
赵润生
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, through its use process and the analysis of relevant data pictures, there are still many shortcomings and defects in this type of aircraft, such as poor balance ability when transitioning from vertical take-off to level flight or from level flight to vertical landing. Poor, complex conversion mechanism, large deflection rotor steering axis moment, small fixed wing, increased drag caused by excessive rotor diameter in level flight, high fuel consumption, and low safety factor, etc.

Method used

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  • Manned/unmanned multipurpose aircraft with dual-mode taking off and landing
  • Manned/unmanned multipurpose aircraft with dual-mode taking off and landing
  • Manned/unmanned multipurpose aircraft with dual-mode taking off and landing

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Embodiment Construction

[0023] specific implementation plan

[0024] Below in conjunction with view, the present invention will be further described:

[0025] When the aircraft takes off vertically, first open the louvered blade cover plate 9, then start the engine 19, and close the clutch 22 to communicate with the longitudinal transmission shaft 23, and drive the transmission bevel gear 17 through the main transmission bevel gear 24 installed on the longitudinal transmission shaft 23 And rotating the vertical shaft 14 drives the double-lift fan 18 to rotate. At this moment, the aircraft has just realized the vertical take-off and landing and hovering of the aircraft under the lift effect provided by the double-layer lift fan 18. When the aircraft needs to fly forward, the booster of the engine 19 is turned on, and the clutch 26 is connected with the propeller rotating shaft 27 at the same time, and the propeller 28 is rotated, so that the aircraft obtains thrust, and the aircraft is carried out in...

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Abstract

By using dual-mode taking off and landing and a flight mode combined by two-layer lift fans and propeller propulsion, a manned/unmanned multipurpose aircraft with the dual-mode taking off and landing disclosed by the invention has many of the advantages owned by fixed-wing aircrafts and helicopters; in addition, the manned/unmanned multipurpose aircraft with the dual-mode taking off and landing has the advantages of good stability, higher flight speed, farther flying range, higher safety factor for occupants in the manned/unmanned multipurpose aircraft, vertical taking off and landing, short-distance or ultrashort-distance taxiing taking off and landing with multiple loading and carrying capacity, good maneuverability and other technical advantages. The design of the manned/unmanned multipurpose aircraft with the dual-mode taking off and landing is completely free of the traditional design mode of tilting rotorcrafts from the exterior to the overall layout and overcomes the shortcomings of rotors of the helicopters in high-speed flight and the dependence on airport runways of the fixed-wing aircrafts. The manned/unmanned multipurpose aircraft with the dual-mode taking off and landing can be applied to a wide variety of fields such as islands, reefs, ships, boats, border posts and the like, and also becomes an all-purpose novel military and civilian multipurpose aircraft.

Description

technical field [0001] Dual-mode lifting manned / unmanned multi-purpose aircraft, belonging to the field of aviation technology [0002] technical background [0003] At present, the only tilt-rotor aircraft produced and put into use in the world is the MY-22 "Osprey" tilt-rotor aircraft developed by the United States for many years. However, through its use process and the analysis of relevant data pictures, there are still many shortcomings and defects in this type of aircraft, such as poor balance ability when transitioning from vertical take-off to level flight or from level flight to vertical landing. Poor, complex conversion mechanism, large deflection rotor steering axis moment, small fixed wing, increased drag due to excessive rotor diameter during horizontal flight, high fuel consumption, and low safety factor. The dual-mode lifting manned unmanned multi-purpose aircraft is a new model with a new concept layout that has been researched to solve the problems existing ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/20B64C27/26B64C29/00
CPCB64C27/20B64C27/26B64C29/0025B64U10/25B64U30/20
Inventor 赵润生
Owner 赵润生
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