The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Aug. 13, 1991

Filed:

Jul. 05, 1990
Applicant:
Inventors:

Craig E Thompson, Gilbert, AZ (US);

Walter L Blackmore, Tempe, AZ (US);

Walid M Boulos, Beverly, MA (US);

Marc Schmittenberg, Phoenix, AZ (US);

Yogendra Sheoran, Scottsdale, AZ (US);

Assignee:

Allied-Signal Inc., Morris Township, Morris County, NJ (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B01P / ;
U.S. Cl.
CPC ...
55-1 ; 55306 ; 55394 ; 60 39092 ;
Abstract

A radial inflow particle separator includes a pair of axially and radially spaced curvilinear walls cooperatively defining a circumferential flow path leading radially inwardly and axially to an engine. Preferably, the particle separator is employed with a turbine engine which is operated at times in an environment laden with dust and particulate matter. Such an environment is typically encountered by a turbine engine of a helicopter, or off-road vehicle. The particle separator provides dust and particulate control features including aero-inertial, particle trajectory, particle boundary-rebound, and scavenge flow tailoring to achieve a dust and particulate separation efficiency as good as or better than the best conventional axial-flow particle separators. This particle separation effectiveness is achieved in a radial inflow particle separator which is smaller and lighter in weight than axial flow devices, and which packages advantageously with the essential structures of a turbine engine.


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