Spacecraft and thermal resistance type end cap mounting structure thereof

The invention relates to a spacecraft and a thermal resistance type end cap mounting structure thereof. The structure comprises an end cap which is internally provided with a first thermal insulation piece, a rear cabin section, a second heat insulation piece which is arranged between the end cap an...

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Bibliographic Details
Main Authors LIU QING, XIAO RENQIN, HU SHANGANG, ZOU TIANPING, WANG QIAOYUN
Format Patent
LanguageChinese
English
Published 28.01.2022
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:The invention relates to a spacecraft and a thermal resistance type end cap mounting structure thereof. The structure comprises an end cap which is internally provided with a first thermal insulation piece, a rear cabin section, a second heat insulation piece which is arranged between the end cap and the rear cabin section so as to form a heat radiation blocking layer, a third thermal insulation piece which is arranged between the end cap and the rear cabin section to form a heat conduction blocking layer, wherein the heat conduction blocking layer covers the heat radiation blocking layer, and a connecting piece which penetrates through the first thermal insulation piece and the third thermal insulation piece and connects the end cap with the rear cabin section. The formed heat radiation blocking layer avoids heat radiation, and the heat conduction blocking layer covers the heat radiation blocking layer, so that the end cap and the rear cabin section are in indirect contact during connection, and thermal radi
Bibliography:Application Number: CN202111315339