Special vehicle for airplane outer wing and horizontal tail composite material detection

A special vehicle and outer wing technology, applied in the direction of the lifting device, etc., can solve the problems of difficult detection and operation of the lower wall plate, no space for ladders, and inability to move freely, etc., to achieve the effects of convenient operation, reasonable structural design, and improved efficiency

Active Publication Date: 2016-10-12
国营芜湖机械厂
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Problems solved by technology

In-situ detection, the detection operation of the lower wall is very difficult
Because these large parts need to be inspected in all areas, ladders and other tooling are used, and they cannot be moved at will. Some areas are blocked by aircraft parts, and there is no space for ladders. Therefore, it is necessary to design a suitable tooling to help flaw detectors. in situ detection

Method used

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  • Special vehicle for airplane outer wing and horizontal tail composite material detection
  • Special vehicle for airplane outer wing and horizontal tail composite material detection
  • Special vehicle for airplane outer wing and horizontal tail composite material detection

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Embodiment Construction

[0021] In order to make the purpose, technical solutions and beneficial effects of the present invention more clear, the preferred embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings, and the present invention will be further described to facilitate the understanding of technical personnel.

[0022] like Figure 1 to Figure 4 Shown, a kind of aircraft outer wing, horizontal tail composite material detection special vehicle, comprise electric mobile lifting platform 1, high back chair 9, detection instrument hanging basket 14, working surface controller 15, guardrail 16, described guardrail 16 is installed on The upper end of the electric mobile lifting platform 1, the high back chair 9 is symmetrically installed on the upper rear part of the electric mobile lifting platform 1, the high back chair 9 is located in the guardrail 16, and the work surface controller 15 is installed on the electric The upper middle par...

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Abstract

The invention discloses a special vehicle for airplane outer wing and horizontal tail composite material detection. The special vehicle comprises an electric movable lifting platform, a high back-rest chair, a detection instrument hanging basket, a workbench top controller and a guardrail. The guardrail is installed at the upper end of the electric movable lifting platform. The high back-rest chair is symmetrically arranged at the rear portion of the upper end of the electric movable lifting platform and located in the guardrail. The workbench top controller is arranged at the middle portion of the upper end of the electric movable lifting platform. The detection instrument hanging basket is arranged at the left front portion of the guardrail. The high back-rest chair is provided with an arm support, and the workbench top controller is connected with the electric movable lifting platform through a wire. The special vehicle has the beneficial effects of being reasonable in structural design, convenient to use and the like. The problem that traditional equipment cannot arrive at a detected part is solved, great convenience is brought to operators for operation, safety and reliability are achieved, the flexible degree is high, and the overhauling efficiency is improved.

Description

technical field [0001] The invention relates to the technical field of aviation product detection, in particular to a special vehicle for composite material detection of aircraft outer wings and horizontal tail. Background technique [0002] After the non-destructive testing and flight test of the composite material structure on the aircraft, ultrasonic testing is required before the transfer. At this time, the outer wings, horizontal tail and other large components have been installed and debugged. For in-situ detection, the detection operation of the lower wall is very difficult. Because these large parts need to be inspected in all areas, ladders and other tooling are used, and they cannot be moved at will. Some areas are blocked by aircraft parts, and there is no space for ladders. Therefore, it is necessary to design a suitable tooling to help flaw detectors. In situ detection. Contents of the invention [0003] In order to solve the above-mentioned technical proble...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B66F11/04
CPCB66F11/042
Inventor 潘峥桂永进田明崎汪洪量
Owner 国营芜湖机械厂
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