Air turbine starter with turbine air exhaust outlet valve

Patent metadata

Field	Value
Publication number	US-10844740-B2
Application number	US-201816021229-A
Country	US
Kind code	B2
Filing date	Jun 28, 2018
Priority date	Jun 28, 2018
Publication date	Nov 24, 2020
Grant date	Nov 24, 2020

Abstract

A system includes an air turbine starter having an inlet, a turbine air exhaust outlet, an output shaft, and a turbine in fluid communication with the inlet and the turbine air exhaust outlet. The turbine is operably coupled to the output shaft. The system also includes an outlet valve assembly configured to adjust an exhaust area of the turbine air exhaust outlet.

First claim

What is claimed is:

1. A system comprising:
an air turbine starter comprising:
an inlet;
a turbine air exhaust outlet;
an output shaft; and
a turbine in fluid communication with the inlet and the turbine air exhaust outlet, the turbine operably coupled to the output shaft;
an outlet valve assembly configured to adjust an exhaust area of the turbine air exhaust outlet, wherein the outlet valve assembly comprises a valve housing and a valve body arranged between the valve housing and the turbine air exhaust outlet, the valve housing comprises at least one pressure port, and a pressurized cavity is formed between the at least one pressure port and the valve body responsive a pressurized flow from the actuator;
an actuator in fluid communication with the outlet valve assembly, the actuator operable to adjust the exhaust area of the turbine air exhaust outlet by sliding the valve body between an open position and a closed position in the turbine air exhaust outlet; and
at least one spring positioned between a housing of the air turbine starter and the valve body, the at least one spring configured to provide an opening force to slide the valve body towards the open position and increase the exhaust area of the turbine air exhaust outlet.

2. The system as in claim 1 , wherein the actuator is operable to increase the pressurized flow to the pressurized cavity and provide a closing force greater than the opening force to slide the valve body towards the closed position and decrease the exhaust area of the turbine air exhaust outlet.

3. The system as in claim 1 , further comprising a starter air valve in fluid communication with the inlet of the air turbine starter, wherein the starter air valve is operable to adjust an inlet air flow to the inlet of the air turbine starter.

4. A system of an aircraft, the system comprising:
an air turbine starter comprising a turbine operably coupled an output shaft, the output shaft coupled to a gearbox of a gas turbine engine;
an outlet valve assembly configured to adjust an exhaust area of a turbine air exhaust outlet of the turbine, wherein the outlet valve assembly comprises a valve housing and a valve body arranged between the valve housing and the turbine air exhaust outlet, the valve housing comprises at least one pressure port, and a pressurized cavity is formed between the at least one pressure port and the valve body responsive a pressurized flow from the actuator;
a controller operable to actuate the outlet valve assembly to slide the valve body between an open position and a closed position in the turbine air exhaust outlet to adjust the exhaust area of the turbine air exhaust outlet and drive rotation of the output shaft responsive to an inlet air flow received at an inlet of the air turbine starter and the exhaust area of the turbine air exhaust outlet, wherein the output shaft drives rotation of the gas turbine engine through the gearbox; and
at least one spring positioned between a housing of the air turbine starter and the valve body, the at least one spring configured to provide an opening force to slide the valve body towards the open position and increase the exhaust area of the turbine air exhaust outlet.

5. The system as in claim 4 , wherein the controller is operable to command the actuator to increase the pressurized flow to the pressurized cavity and provide a closing force greater than the opening force to slide the valve body towards the closed position and decrease the exhaust area of the turbine air exhaust outlet.

6. The system as in claim 4 , further comprising a starter air valve in fluid communication with the inlet of the air turbine starter, wherein the controller is operable to control the starter air valve to adjust the inlet air flow to the inlet of the air turbine starter.

7. A method comprising:
determining an operating mode of an air turbine starter;
actuating an outlet valve assembly to slide a valve body between an open position and a closed position in a turbine air exhaust outlet to adjust an exhaust area of the turbine air exhaust outlet of the air turbine starter based on the operating mode, by commanding an actuator in fluid communication with the outlet valve assembly to adjust the exhaust area of the turbine air exhaust outlet, wherein the actuator is commanded to control a pressurized flow through at least one pressure port of a valve housing of the outlet valve assembly into a pressurized cavity formed between the at least one pressure port and the valve body arranged between the valve housing and the turbine air exhaust outlet;
providing an opening force by at least one spring to slide the valve body towards the open position and increase the exhaust area of the turbine air exhaust outlet; and
driving rotation of an output shaft of the air turbine starter responsive to an inlet air flow received at an inlet of the air turbine starter and the exhaust area of the turbine air exhaust outlet.

8. The method as in claim 7 , further comprising:
commanding the actuator to increase the pressurized flow to the pressurized cavity and provide a closing force greater than the opening force to slide the valve body towards the closed position and decrease the exhaust area of the turbine air exhaust outlet.

9. The method as in claim 7 , further comprising:
commanding the actuator to slide the valve body to an intermediate position between the closed position and the open position based on determining that the operating mode comprises an extended motoring mode below a nominal starting speed of the air turbine starter.

10. The method as in claim 7 , further comprising:
controlling a starter air valve in fluid communication with the inlet of the air turbine starter to adjust the inlet air flow to the inlet of the air turbine starter.

Assignees

• Hamilton Sundstrand Corp
• Hamilton Sunstrand Corp

Inventors

• Zawilinski David J
• Simpson Scott W
• Fukuda Takao

Classifications

• F05D2260/4031

  as in toothed gearing · CPC title

• F05D2260/57

  using servos, independent actuators, etc. · CPC title

• F01D17/145 Primary

  by means of valves, e.g. for steam turbines (valves in general F16K) · CPC title

• F01D19/02

  dependent on temperature of component parts, e.g. of turbine-casing · CPC title

• F05D2220/323

  for aircraft propulsion, e.g. jet engines · CPC title