Tool equipment for hard shell type machine body

A kind of tooling equipment, hard-shell technology, applied in the direction of workpiece clamping device, manufacturing tools, weight reduction, etc., can solve the problems of low assembly efficiency and high requirements for assembly personnel, and achieve the goal of improving assembly efficiency, improving assembly quality, and reducing requirements Effect

Active Publication Date: 2022-03-08
天津飞悦航空科技股份有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In view of the related technologies mentioned above, the inventor believes that there are the following defects: this positioning method has too high requirements on the assemblers, and the assembly efficiency is low

Method used

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  • Tool equipment for hard shell type machine body
  • Tool equipment for hard shell type machine body
  • Tool equipment for hard shell type machine body

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Embodiment Construction

[0034] The following combination Figure 1 to Figure 6 The present invention is described in further detail.

[0035] The embodiment of the invention discloses a tooling device of a hard-shell fuselage. refer to figure 1 , a tooling device for a monocoque fuselage includes a receiving frame 1 , a supporting partition 3 , a beam 4 and a frame positioner 5 . The top of the receiving frame 1 is open, and can accommodate the lower fuselage 2 of the monocoque fuselage. The number of support partitions 3 is multiple, and the plurality of support partitions 3 are arranged in the storage frame 1 at intervals along the longitudinal direction of the storage frame 1 (that is, the front and rear directions), and each support partition 3 has an accommodation gap, This enables each support partition 3 to accommodate and position the lower fuselage 2 through its respective accommodation opening. The crossbeam 4 is arranged above the receiving frame 1, so that the bulkhead positioner 5 ca...

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PUM

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Abstract

The invention relates to the field of tooling equipment, in particular to hard shell type fuselage tooling equipment which comprises a containing frame used for containing a lower fuselage of a hard shell type fuselage; the multiple supporting partition plates are arranged in the containing frame at intervals in the longitudinal direction of the containing frame, and each supporting partition plate is provided with a containing notch, so that each supporting partition plate can contain and position the lower machine body through the corresponding containing notch; the cross beam is arranged on the top of the accommodating frame; and the bulkhead positioner is arranged on the cross beam in a hoisting manner and can be used for positioning the bulkhead of the hard-shell machine body when the bulkhead of the hard-shell machine body is arranged in the lower machine body. The method has the effects of reducing the requirement for assembling personnel and improving the assembling efficiency.

Description

technical field [0001] The invention relates to the technical field of tooling equipment, in particular to a tooling equipment with a hard shell body. Background technique [0002] The monocoque fuselage is often used as an important component of unmanned aircraft or unmanned submarines, at least it can install internal devices such as engines. The monocoque fuselage is mainly composed of an upper fuselage, a lower fuselage, and a bulkhead riveted or welded in the lower fuselage. This structure has a good aerodynamic shape. [0003] Existing tooling equipment mainly includes a base frame for carrying and positioning the lower fuselage. During the assembly process of the fuselage, the assembler needs to first install the bulkhead into the lower fuselage, and then fasten the upper fuselage to the lower fuselage, so as to ensure that the bulkhead can effectively support the upper and lower fuselages. When assembling the bulkhead, the assembler needs to use measuring tools to ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B25B11/02
CPCB25B11/02Y02T50/40
Inventor 陶庆明梁伟超李大巍曹恒祜赵文杰
Owner 天津飞悦航空科技股份有限公司
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