发明名称 Composite piston
摘要 A composite piston structure is disclosed which provides a simple and reliable means for joining a carbon-carbon or ceramic piston cap 11 with a metallic piston body 13. Attachment is achieved by means of a special geometry which compensates for differences in thermal expansion without complicated mechanical fastening devices. The shape employs a flange created by opposed frustoconical shapes 12 and 19 with coincident vertices 15 intersecting on the radial centerline of the piston in order to retain the piston cap. The use of carbon-carbon for the piston cap material allows a close fit between the piston and a cylinder wall, eliminating the need for piston rings. The elimination of extra mechanical parts of previous composite pistons provides a lightweight composite piston capable of extended high temperature operation.
申请公布号 US4736676(A) 申请公布日期 1988.04.12
申请号 US19860890683 申请日期 1986.07.30
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION 发明人 TAYLOR, ALLAN H.
分类号 F16J1/01;B22D19/08;B22D19/14;F02B3/06;F02F3/00;F02F3/26;F02F7/00;(IPC1-7):F16J1/04 主分类号 F16J1/01
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