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Integrated modular system

A modular and integrated technology, applied in instrumentation, geometric CAD, calculation, etc., can solve the problems of lengthened space vehicle assembly cycle, cumbersome and complicated docking installation operations, high economic cost, etc., to simplify the external installation interface, The effect of reducing economic cost and time cost and improving the utilization rate of layout space

Pending Publication Date: 2019-04-16
SHANGHAI INST OF SPACE PROPULSION
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Problems solved by technology

[0004] Based on the above-mentioned propulsion system design method, in order to realize the complex installation and operation of the propulsion system, the main structure design of the spacecraft often has to specially design the cabin section suitable for the layout and installation requirements of the propulsion system, with low space utilization, heavy mass, and cumbersome docking and installation operations complex and high economic cost; in addition, in order to meet the assembly space requirements of the propulsion system, many spacecraft need to start in advance and complete the docking installation of the propulsion system on the main structure before the final assembly of the whole vehicle, and the strict assembly sequence The assembly cycle of the spacecraft is lengthened, the assembly efficiency is low, and the time cost is high

Method used

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  • Integrated modular system

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[0020] In order to make the above objects, features and advantages of the present invention more clearly understood, the present invention will be described in further detail below with reference to the accompanying drawings and specific embodiments.

[0021] like figure 1 As shown, the present invention provides an integrated modular system, comprising: a storage and supply module 1, an output module 2 and an inter-module conveying channel 3, and after the storage and supply module 1, the output module 2 and the inter-module conveying channel 3 are integrated, The module form is installed and docked with the main structure, and the conveying channel 3 connects the inner cavity channel of the storage and supply module 1 and the output module 2 to realize the conveying of the working medium from the storage and supply module 1 to the output module 2, wherein,

[0022] The storage and supply module 1 is integrated with: a storage and discharge container 4, a charge and exhaust p...

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Abstract

The invention provides an integrated modular system. According to the invention, integrated design is carried out according to use functions and installation requirements of each component with an independent function; Integration of components into a module, the connection relationship between the components is simplified; all functions of the system are realized. The performance index is ensured. The external mounting interface with the main structure is simplified. The compression system is in butt joint with the main structure to install a required assembly space. The design objective of completing the layout of a system with complex functions in a narrow space is achieved, the space utilization rate is increased, the assembly efficiency is improved, the development cost and the time cost are reduced, the system can better adapt to the compact and narrow layout space, and meanwhile the light-weight design of the system is achieved.

Description

technical field [0001] The present invention relates to an integrated modular system. Background technique [0002] With the development and application of space vehicle technology, the miniaturization and even miniaturization of space vehicles have become a development trend. The equipment layout space inside the micro-miniature spacecraft is small, the space available for the propulsion system layout is very compact, the space constraints on the layout envelope of the propulsion system are very strict, and the space available for the docking and installation operation of the propulsion system is extremely narrow. Conventional propulsion system layout design methods are often unable to meet the needs of micro and small space vehicles. [0003] At present, the conventional propulsion system layout mostly adopts the distributed layout design method: separate components are designed to realize each independent function, and then each separate component is distributed in vario...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/50
CPCG06F30/15
Inventor 黄含冰丁稷萍楼超超
Owner SHANGHAI INST OF SPACE PROPULSION
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