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A rescue transport aircraft

A technology for transporting airplanes and airplanes, which is applied in the field of aircraft, and can solve problems such as being easily affected by traffic and terrain, patients missing rescue time, and increasing treatment costs, so as to shorten transportation time, reduce the probability of sudden symptoms, and avoid secondary damage effect

Inactive Publication Date: 2019-01-25
FOSHAN SHENFENG AVIATION SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] At present, most medical rescues use ambulances to transport patients. Ambulances are easily affected by traffic and terrain when driving on the road, causing patients to miss the best rescue time; although helicopters are also used for rescue, their cost is high and maintenance The work is complicated, which will undoubtedly greatly increase the cost of treatment

Method used

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  • A rescue transport aircraft
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Embodiment Construction

[0018] Below in conjunction with accompanying drawing, the present invention is described in detail: a kind of rescue transport aircraft, comprises fuselage 1, wing 2, lift device 3, empennage 4.

[0019] The fuselage 1 is a flat structure in which the front end is thicker than the rear end; in this way, when the aircraft is flying, the fuselage 1 can also generate lift while reducing air resistance. The inside of fuselage 1 is a cavity structure, and the top of fuselage 1 is provided with hatch 5, and opening hatch 5 is convenient to put the wounded in the fuselage 1 or the wounded is taken out from the fuselage 1.

[0020] Wing 2 adopts delta wing, and wing 2 extends from fuselage 1 front end to fuselage 1 rear end, under identical wing 2 area, reduces the wingspan of wing 2, dwindles the width of aircraft.

[0021] The main controller 6 is arranged in the fuselage 1, and the aircraft carries out autonomous flight through the control of the main controller 6. The main contro...

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PUM

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Abstract

The invention relates to a rescue transport aircraft, belonging to the technical field of aircraft, comprising a fuselage, a wing, a lifting device and a tail fin. The fuselage has a flat structure with thicker front end than rear end. The wing adopts delta wing, and the wing extends from the front end to the rear end of the fuselage; a mast controller is arranged in that fuselage. The lifting device comprises two large motors with large blades and two small motors with small blades. The lifting device provides vertical lift and horizontal forward pull for the aircraft. The pitch and yaw of the aircraft are adjusted by the tail fins. During take-off, the inclination caused by the side wind is adjusted by controlling the speed difference between the two small motors through the vertical lift of the large motor and the tension of the small motor. The wings are lifted to the wounded position quickly, and the wounded are landed vertically by a large electric motor. Finally, the plane takesoff vertically with the wounded and transports them to the treatment point for treatment. The invention can carry out vertical take-off and landing, has long sailing time, stable flight process and high safety factor.

Description

technical field [0001] A rescue transport aircraft belongs to the technical field of aircraft, and in particular relates to an aircraft. Background technique [0002] At present, most medical rescues use ambulances to transport patients. Ambulances are easily affected by traffic and terrain when driving on the road, causing patients to miss the best rescue time; although helicopters are also used for rescue, their cost is high and maintenance The complexity of the work will undoubtedly greatly increase the cost of treatment. Contents of the invention [0003] In view of this, the present invention provides a rescue transport aircraft, which can perform vertical lift, and can quickly transport the wounded to the treatment point in places with inconvenient traffic. [0004] A rescue and transportation aircraft includes a fuselage, wings, lifting devices and an empennage. [0005] The fuselage is a flat structure with the front end thicker than the rear end; in this way, wh...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/26B64D27/02B64D27/24B64C3/10B64C29/00
CPCB64C3/10B64C27/26B64C29/0008B64D27/02B64D27/24B64U50/19B64U2101/00B64D27/026
Inventor 李玉龙王志成
Owner FOSHAN SHENFENG AVIATION SCI & TECH
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