发明名称 Composite flexible blanket insulation
摘要 Composite flexible multilayer insulation systems (MLI) were evaluated for thermal performance and compared with currently used fibrous silica (baseline) insulation system. The systems described are multilayer insulations consisting of alternating layers of metal foil and scrim ceramic cloth or vacuum metallized polymeric films quilted together using ceramic thread. A silicon carbide thread for use in the quilting and the method of making it are also described. These systems are useful to provide lightweight thermal insulation for a variety of uses, particularly on the surface of aerospace vehicles subject to very high temperatures during flight.
申请公布号 US5038693(A) 申请公布日期 1991.08.13
申请号 US19890410576 申请日期 1989.09.21
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION 发明人 KOURTIDES, DEMETRIUS A.;PITTS, WILLIAM C.;GOLDSTEIN, HOWARD E.;SAWKO, PAUL M.
分类号 B32B5/26;B32B15/04;B64G1/50;B64G1/58;D02G3/46;F16L59/02 主分类号 B32B5/26
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