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A special vehicle for composite material detection of aircraft outer wing and horizontal tail

A special vehicle and outer wing technology, applied in the direction of the lifting device, etc., can solve the problems of not being able to move at will, difficult to detect and operate the lower wall, and no space for the ladder to be placed.

Active Publication Date: 2018-08-31
国营芜湖机械厂
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  • Abstract
  • Description
  • Claims
  • Application Information

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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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  • A special vehicle for composite material detection of aircraft outer wing and horizontal tail
  • A special vehicle for composite material detection of aircraft outer wing and horizontal tail
  • A special vehicle for composite material detection of aircraft outer wing and horizontal tail

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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] Such as Figure 1 to Figure 4 As shown, a special vehicle for composite material testing of the outer wing and flat tail of an aircraft includes an electric mobile lifting platform 1, two high-back chairs 9, a testing instrument hanging basket 14, a worktable controller 15, and a guardrail 16. The guardrail 16 Installed on the upper end of the electric mobile lifting platform 1, the two high-back chairs 9 are symmetrically installed on the upper rear part of the electric mobile lifting platform 1, and the two high-back chairs 9 are located in the guardrail 16. The controller 15 is installed in the middle part of the u...

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Abstract

The invention discloses a special vehicle for composite material testing of aircraft outer wings and flat tail, which comprises an electric mobile lifting platform, two high-back chairs, a hanging basket for testing instruments, a worktable controller, and a guardrail, and the guardrail is installed on the electric mobile lifting platform. Two high-back chairs are installed symmetrically on the upper end of the electric mobile lifting platform, and the two high-back chairs are located in the guardrail. The worktable controller is installed in the middle of the upper end of the electric mobile lifting platform. Installed on the left front of the guardrail, arm supports are installed on the two high-back chairs, and the controller on the working surface is connected to the electric mobile lifting platform through wires. The invention has the advantages of reasonable structural design, convenient use, etc., solves the problem that the traditional equipment cannot reach the detected part, greatly facilitates the operation of operators, is safe and reliable, has high flexibility, and improves the efficiency of maintenance.

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 Patents(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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