Trailer for Helicopter

a technology for helicopters and trailers, applied in the field of helicopters, can solve the problems of helicopter damage, high manpower requirements, and complicated process, and achieve the effect of reliable and efficien

Inactive Publication Date: 2010-10-07
AEROSPACE INDUSTRIAL DEVELOPMENT CORPORATION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

The technical effect of this patented technology relates to providing better ways to make sure that certain parts on a vehicle's wheels are safe when they shouldn’t land safely during flight without causing damage or injury from collisions between them.

Problems solved by technology

This patented technology solves issues related to carrying out this type of flight by attaching rollers onto the aircraft's wheeled legs while also balancing them properly during storage. However, these technical problem addressed in the current design involves requiring multiple components that can make up too much weight when carried around outside airplanes.

Method used

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  • Trailer for Helicopter
  • Trailer for Helicopter
  • Trailer for Helicopter

Examples

Experimental program
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Embodiment Construction

[0017]Referring to FIGS. 1 through 3, a trailer includes a chassis 1, two lifters 2, two drivers 3, two locks 4 and a connector 5. The chassis 1 includes a frame 11, boards 12, two groups of wheels 13, two pairs of tracks 15 and two racks 14. The frame 11 includes two beams. Each group of wheels 13 and a related pair of tracks 15 are attached to a related one of the beams. Each pair of tracks 15 includes a front track 15 and a rear track 15. Each rack 14 is attached to a related one of the beams, next to a related rear track 15.

[0018]Each lifter 2 includes a rear lifting unit 21, a front lifting unit 22, two rods 2, a pusher 24 and a front contact element 25 and a rear contact element 25. The rear lifting unit 21 includes two primary links 211 and 212 and an auxiliary 213. The primary link 212 includes an end pivotally but not movably connected to a related one of the beams and another end pivotally connected to a first end of the primary link 211. A second end of the primary link 211

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PUM

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Abstract

A trailer is provided for a helicopter. The trailer includes a chassis, at least two lifters provided on the chassis, at least two drivers provided on the chassis and connected to the lifters, at least two locks for locking the lifters in an upper position and a connector for connecting the chassis to a vehicle.

Description

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Claims

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Application Information

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Owner AEROSPACE INDUSTRIAL DEVELOPMENT CORPORATION
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