Universal transport packing case for remote sensing satellite

A technology for remote sensing satellites and packaging boxes, which is applied in the field of general transport packaging boxes for remote sensing satellites, can solve the problem of unsolved whole-satellite transportation, the short time of land transportation of communication satellites and navigation satellites, and the inability to meet the requirements of land transportation for remote sensing platforms. Exhaust requirements and other issues, to achieve the effect of shortening the assembly cycle and ensuring high-reliability transportation

Inactive Publication Date: 2012-11-14
BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Different from the structure of communication satellites and navigation satellites, remote sensing satellites have a unique non-load bearing tube through-structure configuration, and the problem of its whole-satellite transportation has not been solved. The demand for the transportation environment puts forward higher and newer requirements for the versatility, temperature, vibration reduction, leak rate, process monitoring, and online analysis of the packaging box.
[0005] The transportation status of communication satellites and navigation satellites is simple, both of which are in the whole-star state, while the transportation of remote sensing satellites has two working conditions: whole-star transportation and sub-compartment transportation; the transportation time of communication satellites and navigation satellites is short on land, and manual charging is required during the process. Exhaust, which cannot meet the long-term land transportation requirements of remote sensing platforms; two impact recorders are installed in the packaging boxes of communication satellites and navigation satellites to record the mechanical environment of transportation, which cannot meet the needs of remote sensing satellites for multi-channel real-time monitoring and analysis requirements, because the existing packaging boxes cannot meet the above requirements, the demand for multifunctional and universal packaging boxes is very urgent

Method used

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  • Universal transport packing case for remote sensing satellite
  • Universal transport packing case for remote sensing satellite
  • Universal transport packing case for remote sensing satellite

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Embodiment Construction

[0031] The remote sensing satellite general transport packing case of the present invention will be further described below in conjunction with the accompanying drawings. Wherein, the specific implementation is for the purpose of illustration only, and is not intended to limit the protection scope of the present invention.

[0032] figure 1 It is a structural schematic diagram of the remote sensing satellite universal transport packing box of the present invention, wherein the remote sensing satellite universal transport packing box of the present invention is mainly composed of a structural subsystem, a monitoring subsystem, a vibration damping subsystem, a temperature control subsystem, and a filling and exhausting subsystem A total of 5 parts.

[0033] The packaging box structure sub-system includes box body (box cover 4, box bottom 8, guiding device 5, sealing ring 12), L-shaped bracket 13, and mobile traction device 17 to form. The size of the inner cavity of the packin...

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Abstract

The invention discloses a universal transport packing case for a remote sensing satellite, which comprises a case cover and a case bottom, wherein an air conditioner, a temperature-humidity sensor, an inflatable / deflatable device capable of being automatically and / or manually inflated or deflated, hoisting points, transport fixing points and a data acquisition and control system are arranged on the case cover; a damping device is arranged on the inner side of the case bottom; an L-shaped bracket used during integrated satellite transport or a transport bracket used during subdivided transport, sensors comprising the temperature-humidity sensor and the like, and fans are arranged above the damping device; the data acquisition and control system is respectively and electrically telecommunicated with the temperature-humidity sensor, a pressure sensor, a vibration sensor, an impact sensor and the like, and is electrically telecommunicated with a remote control terminal so as to conveniently control the transport of the remote sensing satellite over a long distance in real time. The universal transport packing case for the remote sensing satellite can fulfill functions of highway transport, railway transport, system leakage detection and the like when different remote sensing satellites in integrated states or subdivided states are in various working conditions, the remote sensing satellites in the integrated states or the subdivided states can be highly reliably transported and the satellite development cycle is simultaneously shortened.

Description

technical field [0001] The invention belongs to the field of packaging and transportation for general assembly of spacecraft, and in particular relates to a general transportation packaging box for remote sensing satellites. Background technique [0002] In the process of satellite packaging and transportation, the packaging box is an important ground mechanical support equipment. The satellite packaging box is mainly used for the transfer of satellites between different factories and different factories and the packaging and transportation to the launch site. [0003] At present, satellite transport packaging boxes are generally designed according to different satellite platforms. The temperature, humidity, pressure, vibration reduction, and leakage rate of the packaging boxes are designed according to the characteristics of the satellites of the respective platforms, which can meet the transportation requirements of the satellites of the respective platforms. [0004] Diff...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B65D85/68
Inventor 傅浩张伟刘广通张立建赵培荣郑鹏鲍晓萍李长勋王强徐奕柳
Owner BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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