Claims
- 1. In an air-oil separating arrangement for a gas turbine engine, an air-oil separator comprising:
- (a) a circular plate having a center and a pair of opposite faces; and
- (b) a plurality of separator fins attached to and extending from one of said opposite faces of said plate, said separator fins being spaced circumferentially from one another and extending radially from said center of said plate.
- 2. The separator as recited in claim 1, further comprising:
- (c) a hub connected to said center of said plate and extending outwardly from said one face of said plate.
- 3. The separator as recited in claim 2, wherein said fins have inner edges being spaced from one another and also from said hub of said plate.
- 4. The separator as recited in claim 1, wherein said separator fins have generally planar configurations and extend substantially perpendicular to said one face of said plate.
- 5. The separator as recited in claim 1, wherein said fins have inner edges being spaced from one another.
- 6. The separator as recited in claim 1, wherein each of said fins has a generally planar configuration and opposite outer and inner edges being radially spaced from one another relative to said center of said plate.
- 7. The separator as recited in claim 6, wherein said inner edge of said fin extends a greater height from said plate than does said outer edge of said fin.
Parent Case Info
This is a division of application Ser. No. 07/784,847 filed Oct. 30, 1991.
US Referenced Citations (10)
Foreign Referenced Citations (1)
Number |
Date |
Country |
29800 |
Feb 1984 |
JPX |
Divisions (1)
|
Number |
Date |
Country |
Parent |
784847 |
Oct 1991 |
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