Helicopter landing system and landing method

A helicopter and ship landing technology, applied in the aviation field, can solve problems such as electromagnet adsorption, and achieve the effects of good reliability, wide applicability and versatility, and convenient use.
CN106043728AActive Publication Date: 2016-10-26BEIJING INSTITUTE OF TECHNOLOGYGY
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Patent Information

Authority / Receiving Office
CN · China
Current Assignee / Owner
BEIJING INSTITUTE OF TECHNOLOGYGY
Publication Date
2016-10-26

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Abstract

The invention discloses a helicopter landing system. The helicopter landing system comprises a landing auxiliary mechanism installed at the bottom of a helicopter body, and a parking apron arranged on a ship deck. The landing auxiliary mechanism comprises an electromagnet attracting to a helicopter undercarriage. The parking apron is round. A plurality of evenly distributed electromagnetic devices are arranged in the parking apron. The helicopter landing system further comprises a slideway arranged on the ship deck. The parking apron is installed on the slideway. When landing, a helicopter slides to a preset position along the slideway. After landing, the helicopter slides to a helicopter warehouse along the slideway. The helicopter landing system is simple in structure and convenient to use and has good reliability and wide applicability and universality. The helicopter can land safely and stably under the circumstance of strong light and poor sea conditions. Helicopter of different models and sizes can be suitable for the helicopter landing system after improved slightly.
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Description

technical field

[0001] The invention relates to the field of aviation technology, in particular to a helicopter stable landing system and a landing method. Background technique

[0002] According to the classification of operation, helicopters can be divided into manned and unmanned helicopters; according to the classification of energy, they can be divided into electric energy and chemical energy helicopters. Generally, manned helicopters are larger in size, mostly chemical energy, and have obvious mechanical stability; unmanned helicopters have two energy sources, electric energy and chemical energy, and are generally smaller in size, poor in mechanical stability, and poor in resistance to sea wind and mechanical interference. .

[0003] Compared with the stable land, the vertical take-off and landing of the helicopter on the ship is disturbed by the following uncertain factors: the aerodynamic parameters at sea change extremely fast and are difficult to predict; the move...

Claims

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