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Hybrid power composite unmanned helicopter

An unmanned helicopter and hybrid power technology, applied in the field of unmanned aerial vehicles, can solve problems such as complex power structure, accident-prone, and helicopter out-of-control, and achieve the effect of simplifying the structure of the aircraft, avoiding complete loss of control, and reducing fuel consumption

Inactive Publication Date: 2018-11-06
诺一技术有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The main rotor is driven by the engine through the gearbox, and the rear tail rotor is driven by the transmission shaft. This kind of power structure is relatively complicated.
The tail rotor of the helicopter is likely to collide with objects such as treetops and high-voltage lines during low-altitude steering, resulting in irreparable consequences. Once the tail rotor breaks, the helicopter will completely lose control
In addition, the huge rotor of the helicopter is also a place prone to accidents. The huge main rotor rotates rapidly. If it hits an obstacle, it will cause destructive damage to the drone.

Method used

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Examples

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Embodiment Construction

[0036] The specific implementation manners of the present invention will be described in detail below in conjunction with the accompanying drawings.

[0037] Such as Figure 1~Figure 11 As shown, a hybrid unmanned helicopter includes a fuselage 1, and also includes a landing gear assembly 2 fixed on the lower part of the fuselage 1, a short wing assembly 3 arranged symmetrically on both sides of the fuselage 1, and a wing assembly 3 in the middle of the fuselage 1. The main propeller assembly 4 and the tail rotor assembly 5 at the rear of the fuselage 1;

[0038] The landing gear assembly 2 includes a frame body 201 and a detachable road wheel assembly 202 connected with the bottom bolts of the frame body 201; to ensure the safety of the fuselage 1, before take-off and after landing, the detachable road wheel assembly 202 is used to make the landing gear assembly 202 The landing gear assembly 2 drives the fuselage 1 to slide forward, which increases the convenience of the unm...

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Abstract

The invention relates to a hybrid power composite unmanned helicopter. The hybrid power composite unmanned helicopter comprises a helicopter body and further comprises an undercarriage component fixedat the lower part of the helicopter body, stub wing components symmetrically distributed on the two sides of the helicopter body, a main propeller component at the middle part of the helicopter body,and a tail rotor component at the rear part of the helicopter body, the undercarriage component comprises an undercarriage body and a dismountable ground wheel connected with the lower part of the undercarriage body through a bolt, the stub wing component comprises a stub wing body, a pushing propeller at the middle part of the stub wing body, and a pushing motor distributed in the stub wing body, the main propeller component comprises a main propeller main body rotatably connected with the upper part of the helicopter body, an engine distributed at the front part of the inner part of the helicopter body and an auxiliary generator arranged at the front part of the engine, the tail rotor component comprises a tail rotor main body arranged at the tail end of the helicopter body and a tail rotor motor arranged at the inner part of the tail end of the helicopter body, the invention provides the hybrid power composite unmanned helicopter, and a stub wing can be rapidly dismounted.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to a hybrid power composite unmanned helicopter. Background technique [0002] Rotary-wing UAVs and fixed-wing UAVs have their own advantages and disadvantages. Fixed-wing has a longer flight distance and a greater payload. The helicopter-style rotor has superior flexibility, allowing the drone to take off and land in a small space. The power transmission system of a helicopter is the most complicated set in the existing manned aircraft. The main rotor is driven by the engine through the gearbox, and the rear tail rotor is driven by the transmission shaft. This kind of power structure is relatively complicated. The tail rotor of the helicopter is easy to collide with objects such as treetops and high-voltage lines during low-altitude steering, resulting in irreparable consequences. Once the tail rotor breaks, the helicopter will completely lose contro...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/22B64D27/02B64C25/36B64D27/26B64D35/02B64D35/08
CPCB64C25/36B64C27/22B64D27/02B64D35/02B64D35/08B64U50/11B64U50/19B64D27/40B64D27/026
Inventor 屠增培张建明侯霖明李炜张枨枨汪志杰王文涛童康康高峰
Owner 诺一技术有限公司
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