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low-altitude composite aircraft

A composite aircraft, low-altitude technology, applied in the field of manned aircraft, can solve problems such as falling, aircraft imbalance, crash, etc., and achieve the effects of reducing production and manufacturing costs, simplifying design, and reducing control difficulty

Active Publication Date: 2021-04-06
深圳市朗赛微波通信有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Once any rotor fails, it will inevitably cause the aircraft to lose balance and fall, or even crash.

Method used

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Embodiment Construction

[0042] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0043] It should be noted that when an element is referred to as being “fixed” or “disposed on” another element, it may be directly on the other element or be indirectly on the other element. When an element is referred to as being "connected to" another element, it can be directly connected to the other element or indirectly connected to the other element.

[0044] In addition, the terms "first" and "second" are used for descriptive purposes only, and cannot be interpreted as indicating or implying relative importance or implicitly specifying the quantity of indicated technical features. Thus, a ...

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Abstract

The invention is applicable to the field of manned aircraft, and provides a low-altitude composite aircraft, including: an unpowered rotor mechanism, a four-rotor mechanism, a tilting mechanism and a frame for fixing the above mechanisms. The unpowered rotor mechanism provides lift for the low-altitude compound aircraft, and the four-rotor mechanism includes a left front rotor, a right front rotor, a left rear rotor and a right rear rotor whose rotation axes are arranged in parallel and have the same rotational speed. Arranged and turned oppositely, the left rear rotor and the right rear rotor turn oppositely, and the tilting mechanism is used to simultaneously drive the left front rotor, the right front rotor, the left rear rotor and the right rear rotor to Tilt forward or backward. The invention provides low-altitude composite aircraft to realize vertical lift and is conducive to improving the landing safety of the low-altitude composite aircraft and reducing energy consumption. Simultaneously, the simplified design reduces manufacturing costs and reduces the difficulty of control.

Description

technical field [0001] The invention belongs to the field of manned aircraft, in particular to a low-altitude composite aircraft. Background technique [0002] The existing tilting quadrotor aircraft includes a fuselage, a first wing, a second wing, a tilting unit and four sets of rotors; The two rods on the surface, and the four rotors are respectively fixed on the four ends of the two rods. The axis of rotation of the rotor is perpendicular to the rod. When the bar is in a horizontal state, the four rotors rotate to provide forward propulsion for the aircraft; when the bar is in a vertical state, the four rotors rotate to provide upward lift for the aircraft. The speed difference between the first rotor and the following two rotors is realized. The first wing and the second wing are respectively arranged on the left and right sides of the fuselage to provide lift when the aircraft is flying. That is, the take-off and landing flight of the aircraft requires the operatio...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C27/02B64C27/52
CPCB64C27/02B64C27/025B64C27/52
Inventor 涂名超
Owner 深圳市朗赛微波通信有限公司
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