IP Library Granted Patent US 8,424,279
Granted Patent B2
US 8,424,279 · App. 11/729,117 · Granted Apr 23, 2013

Particle separator and debris control system

Inventors: Ravi Rajamani (West Hartford, CT); Rajendra K. Agrawal (South Windsor, CT); Coy Bruce Wood (Ellington, CT)
Assignee: United Technologies Corporation
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Quick Facts
Patent No.
US 8,424,279
App. No.
11/729,117
Filed
Mar 28, 2007
Granted
Apr 23, 2013
Kind
B2
Art Unit
3741
USPC
60/39.092
Abstract

A gas turbine engine system includes an air inlet, an inlet particle separator located at the air inlet and having a blower selectively driven by a variable output motor, and a controller for dynamically controlling the variable output motor that selectively drives the blower of the inlet particle separator.

Claims (37)

1. A gas turbine engine system comprising:

an air inlet;

an inlet particle separator having a blower located upstream from a collection assembly and configured to propel debris to the collection assembly in a downstream direction, the blower being selectively driven by a variable output motor, wherein the inlet particle separator is located at the air inlet; and

a controller for dynamically controlling the variable output motor that selectively drives the blower of the inlet particle separator.

2. The system of claim 1 and further comprising:

an inlet debris monitoring system for sensing debris present at or near the inlet particle separator as a function of debris sensed.

3. The system of claim 2 , wherein the inlet debris monitoring system comprises a ring-shaped electrostatic sensor.

4. The system of claim 2 , wherein the controller adjusts an output of the blower as a function of the output signal from the inlet debris monitoring system.

5. The system of claim 1 and further comprising:

an exhaust debris monitoring system for sensing debris present at an engine exhaust outlet and transmitting an output signal to the controller as a function of debris sensed.

6. The system of claim 5 , wherein the controller adjusts an output of the blower as a function of the output signal from the exhaust debris monitoring system.

7. The system of claim 1 , wherein the controller comprises an electronic engine control module.

8. The system of claim 1 and further comprising:

a substantially frustoconical-shaped ramp located adjacent to the inlet particle separator blower for directing particles radially outward and away from a primary air flow path.

9. The system of claim 1 , wherein the variable output motor is configured to selectively drive the blower at a speed that falls within a predetermined operating speed range.

10. The system of claim 1 , wherein the variable output motor comprises an electric motor.

11. A debris control system for a gas turbine engine, the system comprising:

an air inlet for admitting ambient air into the gas turbine engine;

an inlet debris monitoring system for sensing debris present in the ambient air admitted through the air inlet, wherein the inlet debris monitoring system generates an output signal as a function of debris sensed;

an inlet particle separator located at the air inlet having a blower selectively operable by an electric motor, a ramp located adjacent to the blower for directing particles radially outward from a primary air flow, and a collection assembly, wherein the blower is positioned upstream of the collection assembly and is configured to propel debris from the ramp to the collection assembly in a downstream direction; and

an electronic controller that processes the output signal from the inlet debris monitoring system and drives the electric motor of the blower as a function of the output signal from the inlet debris monitoring system.

12. The system of claim 11 and further comprising:

an engine exhaust outlet; and

an exhaust debris monitoring system for sensing debris present at the engine exhaust outlet and for sending an output signal to the controller as a function of debris sensed, and wherein the controller drives the blower as a function of the output signals from both the exhaust debris monitoring system and the inlet debris monitoring system.

13. The system of claim 11 , wherein the inlet debris monitoring system comprises a ring-shaped electrostatic sensor.

14. The system of claim 11 , wherein the electric motor is configured to selectively drive the blower at speed that falls within a predetermined operating speed range.

15. A debris control system for a gas turbine engine, the system comprising:

an air inlet for admitting ambient air into the gas turbine engine;

an engine exhaust outlet;

an exhaust debris monitoring system for sensing debris present at the engine exhaust outlet, wherein the exhaust debris monitoring system generates an output signal as a function of debris sensed;

an inlet particle separator located at the air inlet having a blower selectively operable by an electric motor, a ramp located adjacent to the blower for directing particles radially outward from a primary air flow, and a collection assembly, wherein the blower is positioned upstream of the collection assembly and is configured to propel debris from the ramp to the collection assembly in a downstream direction; and

an electronic controller that processes the output signal from the exhaust debris monitoring system and drives the electric motor of the blower as a function of the output signal from the exhaust debris monitoring system.

16. The system of claim 15 and further comprising:

an inlet debris monitoring system for sensing debris present at or near the inlet particle separator and for sending an output signal to the controller as a function of debris sensed, and wherein the controller drives the blower as a function of the output signals from both the exhaust debris monitoring system and the inlet debris monitoring system.

17. The system of claim 16 , wherein the inlet debris monitoring system comprises a ring-shaped electrostatic sensor.

18. The system of claim 15 , wherein the electric motor is configured to selectively drive the blower at speed that falls within a predetermined operating speed range.

19. The system of claim 15 , wherein the ramp has a substantially frustoconical shape.

Assignments (4)
CHANGE OF NAME Recorded Jul 27, 2023
From: RAYTHEON TECHNOLOGIES CORPORATION
To: RTX CORPORATION
Reel/Frame 064714/0001 →
CORRECTIVE ASSIGNMENT TO CORRECT THE AND REMOVE PATENT APPLICATION NUMBER 11886281 AND ADD PATENT APPLICATION NUMBER 14846874. TO CORRECT THE RECEIVING PARTY ADDRESS PREVIOUSLY RECORDED AT REEL: 054062 FRAME: 0001. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF ADDRESS. Recorded Mar 4, 2021
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 055659/0001 →
CHANGE OF NAME Recorded Sep 4, 2020
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 054062/0001 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 28, 2007
From: RAJAMANI, RAVI; AGRAWAL, RAJENDRA K.; WOOD, COY BRUCE
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 019159/0529 →
Continuity (1)
Related Publication 20110179763A1 · Jul 28, 2011