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US Patent 7575412 Anti-stall casing treatment for turbo compressors

Patent 7575412 was granted and assigned to MTU Aero Engines on August, 2009 by the United States Patent and Trademark Office.

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Is a
Patent
Patent

Patent attributes

Current Assignee
MTU Aero Engines
MTU Aero Engines
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
7575412
Date of Patent
August 18, 2009
Patent Application Number
10505971
Date Filed
February 5, 2003
Patent Citations Received
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US Patent 12085021 Adjustable air flow plenum with movable closure for a fan of a gas turbine engine
3
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US Patent 12018621 Adjustable depth tip treatment with rotatable ring with pockets for a fan of a gas turbine engine
4
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US Patent 12066035 Adjustable depth tip treatment with axial member with pockets for a fan of a gas turbine engine
5
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US Patent 12078070 Adjustable air flow plenum with sliding doors for a fan of a gas turbine engine
6
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US Patent 11920617 Fluid systems and methods that address flow separation
7
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US Patent 11965528 Adjustable air flow plenum with circumferential movable closure for a fan of a gas turbine engine
8
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US Patent 11970985 Adjustable air flow plenum with pivoting vanes for a fan of a gas turbine engine
9
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US Patent 11987352 Fluid systems that include a co-flow jet
10
Patent Primary Examiner
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Richard Edgar
Patent abstract

A compressor includes a casing defining a generally cylindrical flow passage, a rotor carrying at least one set of rotor blades, at least one set of stator blades, and anti-stall casing treatment. The casing treatment includes an annular recess in the casing for removing low momentum flow adjacent the tips of the rotor blades, and returning the flow to the generally cylindrical flow passage upstream of the point of removal. A plurality of curved guide vanes are located within the annular recess so as to define an annular inlet downstream of the vanes and/or an annular outlet upstream of the vanes. Each guide vane projects radially inwardly from the casing towards a free end which is exposed at or near the mouth of the recess to define a series of curved channels within the recess adjacent the annular inlet and/or the annular outlet.

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