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Rotor aircraft capable of vertically taking off and landing

A technology for vertical take-off and landing and aircraft, which is applied in the field of aviation aircraft and can solve the problems of high requirements for take-off and landing sites, inability to take off and land vertically, and slow flight speed.

Inactive Publication Date: 2020-10-13
洛阳罗德普蓝旋翼机科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Helicopters occupy a high position in the aviation industry because of their great advantages of vertical take-off and landing and ultra-low-altitude flight, but helicopters also have the disadvantage of slow flight speed; fixed-wing aircraft fly fast, but cannot take off and land vertically, and have high requirements for take-off and landing sites; The autogyro is known as the safest aircraft. It can land safely after the power plant stops in the air, but the flight speed is slow and it cannot take off and land vertically.
At present, there is no aircraft that combines the advantages of helicopters, fixed-wing aircraft and autogyro. Aiming at this phenomenon, the present invention designs a rotorcraft that can take off and land vertically, which can meet the needs of a wider range of applications. Exoplanet research opens up new directions

Method used

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  • Rotor aircraft capable of vertically taking off and landing
  • Rotor aircraft capable of vertically taking off and landing
  • Rotor aircraft capable of vertically taking off and landing

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Embodiment Construction

[0021] In order to make the technical means, creative features, objectives and effects of the present invention easy to understand, the present invention will be further explained below in conjunction with specific embodiments.

[0022] In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front end", "rear end", "both ends", "one end", "the other end" The orientation or positional relationship of other indications is based on the orientation or positional relationship shown in the drawings, which is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation and The azimuth structure and operation cannot be understood as a limitation of the present invention. In addition, the terms "first" and "second" are only used for descriptive purposes, and cannot be understood as indicating...

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PUM

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Abstract

The invention discloses a rotor aircraft capable of vertically taking off and landing. The rotor aircraft comprises a fuselage, wings, a propeller, rotors, an empennage and an undercarriage, wherein the front part of the fuselage is a closed cockpit; a power device, a luggage compartment, a transmission system, a control system and the like are arranged in the fuselage; the tail of the fuselage isprovided with a tail beam; the empennage is installed at the tail end of the tail beam; the wings are located on the left side and the right side of the middle of the fuselage and provide an installation point for the propeller and can also provide considerable lift force when the aircraft flies horizontally; one side of each wing is provided with an aileron and a flap, the ailerons provide rolling torque, and the flaps provide lift force. The rotor aircraft combines the advantages of a helicopter, a fixed-wing aircraft and a gyrocopter, has the vertical take-off and landing and ultralow-altitude flight capacity of the helicopter, also has the high-speed flight capacity of the fixed-wing aircraft, and further has the characteristics of high safety and low energy consumption of the gyrocopter, thereby meeting wider use requirements, and being beneficial to popularization and application.

Description

Technical field [0001] The invention relates to the field of aerospace vehicles, in particular to a rotorcraft capable of vertical take-off and landing. Background technique [0002] Since the Wright brothers invented the airplane, various aircraft have emerged in endlessly. Helicopters occupy a high position in the aviation industry due to their great advantages of vertical take-off and landing and ultra-low-altitude flight, but helicopters also have the disadvantage of slow flight speed; fixed-wing aircraft fly fast, but cannot take off and land vertically, and require high take-off and landing sites; Autogyro is known as the safest aircraft. It can land safely after the power unit is parked in the air, but the flight speed is slow and it cannot take off and land vertically. At present, there is no aircraft that combines the advantages of helicopters, fixed-wing aircraft and autogyro. In response to this phenomenon, the present invention designs a rotorcraft capable of vertica...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/26B64C29/00
CPCB64C27/26B64C29/00
Inventor 张旭杨世谊曹祖荣安涛黄延彪刘博文郭明辉
Owner 洛阳罗德普蓝旋翼机科技有限公司
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