TURBOENGINE BLADING MEMBER
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United States of America Patent
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N/A
Issued Date -
Mar 8, 2018
app pub date -
Sep 6, 2017
filing date -
Sep 7, 2016
priority date (Note) -
Published
status (Latency Note)
Importance
Abstract
Disclosed is a turboengine blading member, having at least one platform member and at least one airfoil member. A receiver through opening extends through the platform member. The connector post is received within the receiver through opening. Each of the connector post and the receiver through opening have a retainer flute provided on the circumferential wall and extending along at least a part of the circumferential extent. The retainer flutes are arranged juxtaposed each other with the open sides facing each other such as to jointly form a joint retainer cavity. First and second retainer members are bonded to each other to provide a common retainer member extending into both corresponding retainer flutes, thereby retaining the connector post within the receiver through opening and interlocking the airfoil member and the platform member.
First Claim
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- F01D Class
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- 7 Age