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Rim seal for a gas turbine engine




Title: Rim seal for a gas turbine engine.
Abstract: The rim seal is positioned in an annular space between blades and a non-rotating adjacent structure in a gas turbine engine. The rim seal is connectable to the non-rotating structure and is made of an abradable material. ...


- Montreal, QC, US
Inventors: Eric Durocher, Rene Paquet, Guy Lefebvre
USPTO Applicaton #: #20080061515

The Patent Description & Claims data below is from USPTO Patent Application 20080061515, Rim seal for a gas turbine engine.

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stats Patent Info
Application #
US 20080061515 A1
Publish Date
03/13/2008
Document #
File Date
12/31/1969
USPTO Class
Other USPTO Classes
International Class
/
Drawings
0




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20080313|20080061515|rim seal for a gas turbine engine|The rim seal is positioned in an annular space between blades and a non-rotating adjacent structure in a gas turbine engine. The rim seal is connectable to the non-rotating structure and is made of an abradable material. |
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