AIR TURBINE START SYSTEM WITH MONOPOLE STARTER AIR VALVE POSITION

• US 20120266606A1
• Filed: 04/20/2011
• Published: 10/25/2012
• Est. Priority Date: 04/20/2011
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Zeiner, Peter Kenneth, Wiggins, Jimmy, Oman, Dave
• Granted Patent: US 9,845,734 B2
• Time in Patent Office: Days
• US Class Current: 60/788
• CPC Class Codes: F01D 17/06 responsive to speed
• CPC Class Codes: F01D 19/00 Starting of machines or engines; Regulating, controlling, or safety means in connection therewith warming-up before starting F01D25/10; turning or inching gear F01D25/34
• CPC Class Codes: F02C 7/277 the starter being a separate turbine
• CPC Class Codes: F05D 2260/40311 of the epicyclical, planetary or differential type
• CPC Class Codes: F05D 2260/80 Diagnostics
• CPC Class Codes: F05D 2260/85 Starting
• CPC Class Codes: F05D 2270/304 Spool rotational speed
• CPC Class Codes: F05D 2270/44 active, predictive, or anticipative
• CPC Class Codes: F05D 2270/54 by electronic means, e.g. electronic tubes, transistors or IC's within an electronic circuit
• CPC Class Codes: F05D 2270/65 Pneumatic actuators

Abstract

An air turbine start system is provided that includes an air turbine starter, a starter air valve, a turbine speed sensor, and a circuit. The starter air valve is movable between an open position, in which the pressurized air may flow into the air turbine starter, and a closed position, in which pressurized air does not flow into the air turbine starter. The turbine speed sensor is coupled to the air turbine starter, and is configured to sense the rotational speed of the turbine and supply a rotational speed signal representative thereof. The circuit is coupled to receive the rotational speed signal and is configured, upon receipt thereof, to determine whether the starter air valve is in the closed position or an open position.

Claims

1. An air turbine start system, comprising:

an air turbine starter comprising a rotationally mounted turbine, the air turbine starter adapted to receive pressurized air and configured, upon receipt of the pressurized air, to direct the pressurized air into the turbine to thereby cause the turbine to rotate at a rotational speed;

a starter air valve in fluid communication with the air turbine starter and movable between an open position, in which the pressurized air may flow into the air turbine starter, and a closed position, in which pressurized air does not flow into the air turbine starter;

a turbine speed sensor coupled to the air turbine starter, the turbine speed sensor configured to sense the rotational speed of the turbine and supply a rotational speed signal representative thereof; and

a circuit coupled to receive the rotational speed signal and configured, upon receipt thereof, to determine whether the starter air valve is in the closed position or an open position.

2. The system of claim 1, wherein the turbine speed sensor comprises a monopole sensor.

3. The system of claim 2, wherein:

the air turbine starter further comprises a plurality of gears coupled to the turbine; and

the monopole sensor is disposed adjacent at least one of the plurality of gears.

4. The system of claim 3, wherein:

the plurality of gears comprises a planet gear set; and

the monopole sensor is disposed adjacent the planet gear set.

5. The system of claim 3, wherein:

the plurality of gears comprises a ring gear; and

the monopole sensor is disposed adjacent the ring gear.

6. The system of claim 1, wherein:

the air turbine starter is further adapted to be coupled to a gas turbine engine; and

the circuit is further configured, upon receipt of the rotational speed signal, to determine if the air turbine starter is being back-driven by the gas turbine engine.

7. The system of claim 1, wherein the circuit is further configured, in response to the rotational speed signal, to control pressurized air flow to the air turbine starter, to thereby control turbine acceleration rate and speed.

8. The system of claim 1, further comprising a gas turbine engine coupled to the air turbine starter.

9. The system of claim 8, further comprising:

an engine control configured to control operations of the gas turbine engine,

wherein the circuit is disposed within the engine control.

10. A gas turbine engine system, comprising:

a gas turbine engine;

an air turbine starter coupled to the gas turbine engine and comprising a rotationally mounted turbine, the air turbine starter adapted to receive pressurized air and configured, upon receipt of the pressurized air, to direct the pressurized air into the turbine to thereby cause the turbine to rotate at a rotational speed;

a starter air valve in fluid communication with the air turbine starter and movable between an open position, in which the pressurized air may flow into the air turbine starter, and a closed position, in which pressurized air does not flow into the air turbine starter;

a monopole sensor coupled to the air turbine starter, the monopole sensor configured to sense the rotational speed of the turbine and supply a rotational speed signal representative thereof; and

a circuit coupled to receive the rotational speed signal and configured, upon receipt thereof, to determine whether the starter air valve is in the closed position or an open position.

11. The system of claim 10, wherein:

the air turbine starter further comprises a plurality of gears coupled to the turbine; and

the monopole sensor is disposed adjacent at least one of the plurality of gears.

12. The system of claim 11, wherein:

the plurality of gears comprises a planet gear set; and

the monopole sensor is disposed adjacent the planet gear set.

13. The system of claim 11, wherein:

the plurality of gears comprises a ring gear; and

the monopole sensor is disposed adjacent the ring gear.

14. The system of claim 10, wherein the circuit is further configured, upon receipt of the rotational speed signal, to determine if the air turbine starter is being back-driven by the gas turbine engine.

15. The system of claim 10, wherein the circuit is further configured, in response to the rotational speed signal, to control pressurized air flow to the air turbine starter, to thereby control turbine acceleration rate and speed.

16. The system of claim 10, further comprising:

an engine control configured to control operations of the gas turbine engine,

wherein the circuit is disposed within the engine control.

17. An air turbine start system, comprising:

an air turbine starter comprising a rotationally mounted turbine, the air turbine starter adapted to receive pressurized air and configured, upon receipt of the pressurized air, to direct the pressurized air into the turbine to thereby cause the turbine to rotate at a rotational speed;

a starter air valve in fluid communication with the air turbine starter and movable between an open position, in which the pressurized air may flow into the air turbine starter, and a closed position, in which pressurized air does not flow into the air turbine starter;

a monopole sensor coupled to the air turbine starter, the monopole sensor configured to sense the rotational speed of the turbine and supply a rotational speed signal representative thereof; and

a circuit coupled to receive the rotational speed signal and configured, upon receipt thereof, to;

(i) determine whether the starter air valve is in the closed position or an open position,

(ii) determine if the air turbine starter is being back-driven, and

(iii) control pressurized air flow to the air turbine starter, to thereby control turbine acceleration rate and speed.

18. The system of claim 17, wherein:

the air turbine starter further comprises a plurality of gears coupled to the turbine; and

the monopole sensor is disposed adjacent at least one of the plurality of gears.

19. The system of claim 18, wherein:

the plurality of gears comprises a planet gear set; and

the monopole sensor is disposed adjacent the planet gear set.

20. The system of claim 18, wherein:

the plurality of gears comprises a ring gear; and

the monopole sensor is disposed adjacent the ring gear.