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Expandable single-duct aircraft

An aircraft and ducted technology, applied in aircraft, unmanned aircraft, aircraft parts, etc., can solve the problems of inability to cruise for a long time, large flight resistance, short flight time, etc., to improve flight time and speed. The effect of reachability

Active Publication Date: 2021-03-12
江西洪都航空工业股份有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, due to the small space inside the single-duct aircraft and the balance of gravity maintained by the thrust of the engine, this type of aircraft is only suitable for mounting small reconnaissance equipment; and the fuel consumption is high, the voyage time is short, and it cannot cruise for a long time; the flight resistance is large, low speed

Method used

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Embodiment Construction

[0028] It should be noted that in this embodiment, the orientation words "up", "down", "left", and "right" are all described according to the drawings, and do not constitute limitations to the present invention.

[0029] Attached below Figure 1-9 The present invention is described in further detail:

[0030] An expandable single duct aircraft, comprising a main duct wall 1, an expandable duct wall A2, an expandable duct wall B3, a rotary actuator and hinge A4, a rotary actuator and hinge B5, a fixed tail 6, Combined empennage 7, coaxial reverse rotor propeller 8, cross-shaped empennage 9, multifunctional rudder surface 10, equipment compartment 11, consumable drone 12; main duct wall 1, expandable duct wall A2 and expandable The duct wall B3 is closed to form an annular duct, and the three are connected by the rotary actuator and the hinge A4, the rotary actuator and the hinge B5; It is consistent with the length direction of the main duct wall 1; the combined empennage 7 i...

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Abstract

The invention relates to an expandable single-duct aircraft, and belongs to the field of aircraft design. The expandable single-duct aircraft comprises an annular duct, propellers and an equipment cabin, the annular duct comprises a main duct wall, an expandable duct wall A and an expandable duct wall B, and the main duct wall, the expandable duct wall A and the expandable duct wall B are connected through rotary actuators and hinges; the propellers and the equipment cabinare both installed on a center shaft of the duct, the propellers provides advancing tension, and cross-shaped empennages are fixed between the equipment cabin and the main duct wall and between the expandable duct wall A and the expandable duct wall B; and in the fixed wing mode, the expandable duct wall A and the expandable duct wall B are expanded and are respectively and mechanically limited and locked with the main duct wall, and in the duct mode, the cross-shaped empennages are mechanically locked with the expandable duct wall A and the expandable duct wall B. The expandable single-duct aircraft has the following advantages: 1, the expandable single-duct aircraft has two modes of ducted flight and fixed wingflight; 2, a plurality of separable consumable unmanned aerial vehicles can be carried on the outer wall of the duct; and 3, the problems of a single ducted aircraft are solved.

Description

technical field [0001] The invention relates to an expandable single-duct aircraft, which belongs to the field of aircraft design. Background technique [0002] Single-duct aircraft has the characteristics of vertical take-off and landing, hovering and fast flight, and has been widely developed and researched in various countries. However, due to the small space inside the single-duct aircraft and the thrust of the engine to maintain the balance of gravity, this type of aircraft is only suitable for mounting small reconnaissance equipment; and the fuel consumption is high, the voyage time is short, and it cannot cruise for a long time; the flight resistance is large. low speed. Contents of the invention [0003] The purpose of the present invention is to solve the problems existing in the prior art, and to provide a deployable single-duct aircraft that takes into account both the fixed-wing mode and the duct mode. [0004] In order to achieve the above object, the presen...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/26B64D5/00
CPCB64C27/26B64D5/00B64U50/14
Inventor 李自启王黎明刘敏李鹏飞付炜嘉万俊明卢森何梦临吴萍徐超
Owner 江西洪都航空工业股份有限公司
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