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
View PDF6 Cites 10 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

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

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Helicopter landing system and landing method
  • Helicopter landing system and landing method
  • Helicopter landing system and landing method

Examples

Experimental program
Comparison scheme
Effect test

Example Embodiment

[0048] Hereinafter, the present invention will be further described in detail through the accompanying drawings and embodiments. Through these descriptions, the characteristics and advantages of the present invention will become clearer.

[0049] The dedicated word "exemplary" here means "serving as an example, embodiment, or illustration." Any embodiment described herein as "exemplary" need not be construed as being superior or better than other embodiments. Although various aspects of the embodiments are shown in the drawings, unless otherwise noted, the drawings are not necessarily drawn to scale.

[0050] A helicopter landing system according to the present invention, such as figure 1 , figure 2 with image 3 As shown, the system includes an electromagnet installed on the bottom of the helicopter body and an apron 1 installed on the deck of the ship.

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

[0052] The apron 1 is circula...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

No PUM Login to view more

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

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
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
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap