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Ultra-large type stretch-draw integral keel structure integration tool and method thereof

A technique of tensioning the whole and integration method, applied in the direction of aircraft assembly, etc., can solve the problem that the final assembly integration method is difficult to follow the final assembly idea, and achieve the effect of simple final assembly and integration, long cycle and high cost

Active Publication Date: 2021-07-27
SHANGHAI JIAO TONG UNIV +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

For the airship lightweight keel system with a length greater than 100 meters and a height greater than 40 meters, due to its special structural form and characteristics, its final assembly integration method is difficult to follow the traditional rigid airship structure, aircraft cabin and other general assembly ideas

Method used

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  • Ultra-large type stretch-draw integral keel structure integration tool and method thereof
  • Ultra-large type stretch-draw integral keel structure integration tool and method thereof
  • Ultra-large type stretch-draw integral keel structure integration tool and method thereof

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Embodiment Construction

[0059] The following describes several preferred embodiments of the present invention with reference to the accompanying drawings, so as to make the technical content clearer and easier to understand. The present invention can be embodied in many different forms of embodiments, and the protection scope of the present invention is not limited to the embodiments mentioned herein.

[0060] In the drawings, components with the same structure are denoted by the same numerals, and components with similar structures or functions are denoted by similar numerals. The size and thickness of each component shown in the drawings are shown arbitrarily, and the present invention does not limit the size and thickness of each component. In order to make the illustration clearer, the thickness of parts is appropriately exaggerated in some places in the drawings.

[0061] Such as figure 2 , image 3 , Figure 4 with Figure 5 As shown, a preferred embodiment of the present invention provid...

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Abstract

The invention discloses an ultra-large type stretch-draw integral keel structure integration tool and a method thereof, which relate to the technical field of aircraft structure general assembly. The ultra-large type stretch-draw integral keel structure integration tool is characterized by comprising a plurality of bearing frames, a plurality of center core supports, a tail cone support, a head cone support, a plurality of center core trusses, a plurality of stiffening rings and a plurality of longitudinal pull rods, wherein the bearing frames are anchored on the ground, and the center core support, the tail cone support and the head cone support are installed on the tops of the different bearing frames respectively. Scattered multi-point support is realized by adopting a modular, segmental frame and functional support integration tool, the support has three-dimensional pose adjustment capability, and efficient, economical, rapid and simple final assembly and integration of a large-scale tensegrity keel structure are realized by utilizing self-bearing support of the central core truss and the stiffening rings; the problems of high-altitude assembly of the all-round scaffold and high cost, long period and the like caused by manufacturing, erecting, disassembling and process interference of a large number of scaffolds are solved.

Description

technical field [0001] The invention relates to the technical field of aircraft structural assembly, in particular to a super-large tension integral keel structure integration tooling and a method thereof. Background technique [0002] Stratospheric airships rely on buoyancy, propulsion and control to achieve long-term flight, fixed-point cruise, and altitude maintenance, thereby completing applications such as scientific detection and communication, and have broad application prospects. However, due to the environment such as the low density of the stratosphere and the current structural materials, energy and other technologies, the length of the airships involved in the domestic and foreign demonstrations are all more than 100m, and the commercial-grade load scenarios can be completed. The temperature alternation between day and night brings great changes in the buoyancy and pressure of the soft capsule structure, and there are challenges in maintaining the altitude of the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/10
CPCB64F5/10
Inventor 陈务军张祎贝李世平章李强胡建辉徐建东刘晶相海军汤令辰黄晓惠
Owner SHANGHAI JIAO TONG UNIV
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