A towing device for light amphibious aircraft

A technology for amphibious aircraft and traction devices, which is applied to ground devices, aircraft parts, transportation and packaging, etc., and can solve problems such as aircraft sliding, lack of corresponding equipment, and unstable fixation of the aircraft

Active Publication Date: 2022-07-22
湖北航特航空飞行器有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] At present, with the development of science and technology and the improvement of living standards, the number of small amphibious aircraft is gradually increasing. When parking an amphibious aircraft, there will generally be a special traction device to tow it, and the general traction device is not enough to fix the amphibious aircraft. Firm, when towing the aircraft, often cause the aircraft to slide due to the insecure fixation of the aircraft, which poses a great safety hazard
[0003] After searching, the Chinese patent application number is CN201820550229.6, which discloses a small amphibious aircraft traction device, including a base, the lower end of the base is connected with a connecting block through a shock absorbing device, and the lower end of the connecting block is rotatably connected with a Roller, the base is provided with a first bar-shaped groove, and the base is also symmetrically provided with a second bar-shaped groove, and the base is symmetrically provided with a first groove with an upward opening, but the above-mentioned device is only through the support seat The fuselage and landing gear of the amphibious aircraft are clamped and fixed with arc-shaped splints. There is no corresponding mechanism that can effectively fix the floating plate on the amphibious aircraft, so there is still no way to simultaneously fix the amphibious aircraft. Effective fixing of fuselage and floating plate

Method used

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  • A towing device for light amphibious aircraft
  • A towing device for light amphibious aircraft
  • A towing device for light amphibious aircraft

Examples

Experimental program
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Effect test

Embodiment 1

[0036] A towing device for a light amphibious aircraft, such as Figure 1-9 As shown, it includes a support frame 1, the outer wall of one side of the support frame 1 is fixed with a connecting plate 9 by screws, the top outer wall of the connecting plate 9 is fixed with a support plate 11 by screws, and the connecting plate 9 and the top outer wall of the support frame 1 are provided with at least two A sliding guide groove 34, the inner wall of the sliding guide groove 34 is slidably connected with the front splint 12 of the fuselage, the outer wall of one side of the front splint 12 of the fuselage is fixed with a squeeze switch 14 by screws, and the outer wall of one side of the front splint 12 of the fuselage is fixed with more than three springs 32. The outer wall of one side of the spring 32 is fixed on the outer wall of one side of the support plate 11, the outer walls of the two sides of the support frame 1 are provided with more than three guiding through grooves 37, ...

Embodiment 2

[0046] A towing device for a light amphibious aircraft, such as figure 1 , figure 2 , Figure 4 , Figure 5 , Figure 7As shown in the figure, in order to allow the staff to easily push the aircraft onto the support frame 1; this embodiment makes the following improvements on the basis of Embodiment 1: the outer wall of the top of the support frame 1 is provided with more than three rectangular installation grooves 15 to support The top inner wall of the frame 1 is fixed with more than three L-shaped mounting plates 22 by screws, and the bottom inner wall of the support frame 1 and one side outer wall of the L-shaped mounting plate 22 are fixed by screws with more than three first elastic telescopic rods 24, three or more The outer wall of one side of the first elastic telescopic rod 24 is rotatably connected with more than three rotating columns 23, the outer wall of the rotating column 23 is fixed with a rolling wheel 2, and the outer wall of the three or more rotating c...

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Abstract

The invention discloses a traction device for a light amphibious aircraft, which relates to the technical field of amphibious aircraft traction devices; in order to solve the problem that the fuselage and the floating plate of the amphibious aircraft cannot be effectively fixed at the same time; the device specifically includes a support frame A connecting plate is fixed on the outer wall of one side of the support frame, and a supporting plate is fixed on the outer wall of the top of the connecting plate. At least two sliding guide grooves are opened on the connecting plate and the outer wall of the top of the supporting frame. A squeeze switch is fixed on the outer wall of one side of the front splint. In the present invention, by arranging the front splint of the fuselage, the squeeze switch, the side splint of the fuselage, the second floating plate clamping block and the first floating plate clamping block, the staff can control the electro-hydraulic push rod to push the U-shaped pusher through the control panel. The height of the raised plate allows the side splint of the fuselage, the second floating plate clamping block and the first floating plate clamping block to clamp and fix different types of amphibious aircraft.

Description

technical field [0001] The invention relates to the technical field of traction devices for amphibious aircraft, in particular to a traction device for light amphibious aircraft. Background technique [0002] At present, with the development of science and technology and the improvement of living standards, small amphibious aircraft are gradually increasing. When parking amphibious aircraft, there are generally special traction devices to tow them, and general traction devices are not enough to fix amphibious aircraft. Firm, when towing the aircraft, the aircraft is often slipped because the aircraft is not firmly fixed, and the safety hazard is great. [0003] After retrieval, the Chinese patent application number CN201820550229.6 discloses a small amphibious aircraft traction device, including a base, the lower end of the base is connected with a connecting block through a shock absorbing device, and the lower end of the connecting block is rotatably connected with a Roll...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64F1/22
CPCB64F1/222
Inventor 胡豆胡明程刘天福
Owner 湖北航特航空飞行器有限公司
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