发明名称 Thermal compensating mount
摘要 A thermal compensating mount 10 is provided for an alignment sensitive component 12. Thermal compensating 10 mount comprises a cylindrical extension 14 which is formed integral to and has the same coefficient of thermal expansion as alignment sensitive component 12. A cylindrical receptacle 20 is formed into mounting surface 18. Cylindrical extension 14 secured within cylindrical receptacle 20 that surrounds the cylindrical extension. The difference between the diameter of cylindrical extension 14 and cylindrical receptacle 20 is such that the differential thermal expansion across cylindrical extension 14 and the edges of cylindrical receptacle 20 is exactly compensated for by the thermal expansion of the surrounding adhesive 16.
申请公布号 US4895430(A) 申请公布日期 1990.01.23
申请号 US19890366205 申请日期 1989.06.12
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION 发明人 JALINK, JR., ANTONY;CAMPBELL, SCOTT R.
分类号 G02B7/00 主分类号 G02B7/00
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