Run-in coating for axial-flow compressor of gas turbine...

Details Run-in coating for axial-flow compressor of gas turbine... Run-in coating for axial-flow compressor of gas turbine...

2005-06-28

2005-06-28

Verdier, Christopher (Department: 3745)

Rotary kinetic fluid motors or pumps

Bearing, seal, or liner between runner portion and static part

Between blade edge and static part

C415S173500, C277S355000, C277S922000, C277S923000, C029S888300

Reexamination Certificate

active

06910856

ABSTRACT:
Metal wire bundles are combined into brushes as a run-in coating for the axial-flow compressor stage of a gas turbine engine. The metal wire bundles are inserted into the basic material or are combined into brush segments that are inserted into corresponding recesses of the rotor housing.

REFERENCES:
patent: 4063848 (1977-12-01), Wiggins et al.
patent: 6439844 (2002-08-01), Turnquist et al.
patent: 6533284 (2003-03-01), Aksit et al.
patent: 6547522 (2003-04-01), Turnquist et al.
patent: 23 44 666 (1974-03-01), None
patent: 58-143014 (1983-08-01), None
patent: 59-505 (1984-01-01), None
patent: 09 144 699 (1997-06-01), None
patent: WO 02/36950 (2001-11-01), None

Affiliated with

Also associated with

Rating

Run-in coating for axial-flow compressor of gas turbine... does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Run-in coating for axial-flow compressor of gas turbine..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Run-in coating for axial-flow compressor of gas turbine... will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-3495949