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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.

Active Publication Date: 2016-10-26
BEIJING INSTITUTE OF TECHNOLOGYGY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

However, this patent is only applicable to decks made of iron-cobalt-nickel and their alloys. If the deck is not a magnetic medium but some new composite material, the electromagnet cannot complete the adsorption with the deck.

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  • Helicopter landing system and landing method
  • Helicopter landing system and landing method
  • Helicopter landing system and landing method

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Embodiment Construction

[0048] The present invention will be further described in detail through the drawings and examples below. Through these descriptions, the features and advantages of the present invention will become more apparent.

[0049] The word "exemplary" is used exclusively herein to mean "serving as an example, embodiment, or illustration." Any embodiment described herein as "exemplary" is not necessarily to be construed as superior or better than other embodiments. While various aspects of the embodiments are shown in drawings, the drawings are not necessarily drawn to scale unless specifically indicated.

[0050] According to a kind of helicopter landing system provided by the present invention, such as figure 1 , figure 2 and image 3 As shown, the system includes an electromagnet installed at the bottom of the helicopter body and an apron 1 arranged on the ship deck,

[0051] Wherein, the electromagnet is preferably adsorbed on the landing gear of the helicopter,

[0052] The...

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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.

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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Application Information

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IPC IPC(8): B64F1/02B64D45/04
CPCB64D45/04B64F1/02
Inventor 王辉林德福王伟林时尧宋韬纪毅韩丁丁
Owner BEIJING INSTITUTE OF TECHNOLOGYGY
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