Foldable type composite lifting power aircraft with extended platform

A folding, aircraft technology, applied in the field of aircraft, can solve the problems of low safety factor, excessively long wings on both sides, and high requirements for take-off and landing, and achieve the effect of safeguarding personnel and materials, high wing structure strength, and reducing gravitational acceleration.

Inactive Publication Date: 2018-11-13
JIANGSU CHANGTAN ROBOT CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The traditional fixed wing has the advantages of fast flight speed, low energy consumption, etc., but it has the disadvantages that the main wing and the horizontal tail are not connected front and rear, the wing structure is not strong, easy to be damaged, the take-off and landing requirements are high, and the take-off and landing distance is long; the traditional vertical The take-off and landing aircraft has the advantages of convenient take-off and landing, but has the disadvantages of large energy consumption, low safety factor, poor load capacity, slow horizontal flight speed, and easy crash; although the current vertical take-off and landing fixed wing has the characteristics of convenient take-off and landing , but the controllability is not ideal when flying horizontally, and there are disadvantages such as large flight resistance, high energy consumption, and low safety factor.
At the same time, existing fixed-wing aircraft with a relatively high safety factor have shortcomings such as too long wings on both sides, unable to be folded from the root, and occupying a large hangar area, which affects the entry of future flying cars into homes and aircraft carriers. Carrying a large number limits the play of the aircraft carrier's combat effectiveness.

Method used

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  • Foldable type composite lifting power aircraft with extended platform

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Embodiment Construction

[0026] The present invention will be further described below in conjunction with the accompanying drawings.

[0027] Such as figure 1 As shown, a foldable compound lift aircraft with an expanded platform includes a fuselage 101, composite lift wings 102 installed on both sides of the fuselage 101 through folding hinges 109, and propellers 106; wherein, the fuselage 101 is set It is a deck platform, and there are fixing holes 1003 on both sides of the deck platform; the composite lift wing 102 can be divided into two parts, the lift main wing 1021 and the balance empennage 1023, which are respectively arranged at the front and back of the composite lift wing 102 There is a space reserved between the lift main wing 1021 and the balance tail 1023, and a horizontal elevating rudder wing 1022 is arranged in the space; wherein, at least one self-enclosed ducted fan 104 is installed inside the lift main wing 1021. Further, the composite lift wing 102 is folded and installed on both...

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Abstract

The invention discloses a foldable type composite lifting power aircraft with an extended platform. The foldable type composite lifting power aircraft with the extended platform comprises an aircraftbody, composite lifting power wings which are installed at the two sides of the aircraft body in a foldable mode and a propeller, wherein the aircraft body is arranged as a deck platform; self-sealingducted fans are arranged in the composite lifting power wings; horizontal lifting rudder wings are arranged in the composite lifting power wings, and the composite lifting power wings are externallyprovided with vertical tail wings and vertical rudder wings. Compared with the prior art, the foldable type composite lifting power aircraft with the extended platform has the characteristics that thetake-off and landing distance is short, the loading capacity is large, the flight speed is high, the flight distance is far, the aircraft is maneuverable and flexible, the supermobility of the flightpath can be realized, the obstacle avoidance ability is good, the energy consumption is low, the extended functions are multiple, the hang time is long and space occupation is small; in addition, thestorage and transportation space occupation is reduced and the foldable type composite lifting power aircraft with the extended platform is especially suitable for the environment with limited spacesuch as families and aircraft carriers. According to the scheme, the quantity of carrier based aircrafts can be greatly increased, and the advantages that the number of the aircraft carried by medium-sized carriers is no less than that of large-sized carriers and the like can be achieved.

Description

technical field [0001] The invention relates to an aircraft, in particular to a foldable composite lift aircraft with an extended platform, which belongs to the technical field of aircraft equipment. Background technique [0002] Existing aircraft are mainly divided into two categories: fixed-wing and vertical take-off and landing aircraft (such as helicopters and multi-rotors). Of course, there is also a vertical take-off and landing fixed-wing product. The traditional fixed wing has the advantages of fast flight speed, low energy consumption, etc., but it has the disadvantages that the main wing and the horizontal tail are not connected front and rear, the wing structure is not strong, easy to be damaged, the take-off and landing requirements are high, and the take-off and landing distance is long; the traditional vertical The take-off and landing aircraft has the advantages of convenient take-off and landing, but has the disadvantages of large energy consumption, low saf...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/30B64C27/20B64C27/26B64C37/02
Inventor 任曲波
Owner JIANGSU CHANGTAN ROBOT CO LTD
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