# US 9,752,508 B2 · Air turbine starters having oil feed shutoff valves and gas turbine engines including the same

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- Number: US 9,752,508 B2
- Document ID: US9752508B2
- Status: Granted
- Kind: B2
- Application number: 14/755,668
- Filed: 2015-06-30
- Published: 2015-10-15
- Granted: 2017-09-05
- Earliest claimed: 2015-04-23
- Assignees: Honeywell International Inc.
- Applicants: Honeywell International Inc.
- Inventors: Kellan Geck; Gerhard Schroeder; Doug Smith
- Web page: https://patentgrep.com/patent/US9752508B2

## CPC

- F02C 7/27: Fluid drives (turbine starters F02C7/277)
- A61F 2/1613: {having special lens configurations, e.g. multipart lenses; having particular optical properties, e.g. pseudo-accommodative lenses, lenses having aberration corrections, diffractive lenses, lenses for variably absorbing electromagnetic radiation, lenses having variable focus}
- A61F 2/1629: {for changing longitudinal position, i.e. along the visual axis when implanted}
- A61F 2/1648: {Multipart lenses}
- A61F 2/1694: {Capsular bag spreaders therefor}
- F02C 7/275: Mechanical drives
- F02C 7/277: the starter being a {separate} turbine
- A61F 2220/0033: made by longitudinally pushing a protrusion into a complementary-shaped recess, e.g. held by friction fit
- F05D 2260/98: Lubrication
- F02C: GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS (construction of turbines F01D; jet-propulsion plants F02K; construction of compressors or fans F04; generating combustion products of high pressure or high velocity F23R; using gas turbines in compression refrigeration plants F25B11/00)
- A61F: FILTERS IMPLANTABLE INTO BLOOD VESSELS; PROSTHESES; DEVICES PROVIDING PATENCY TO, OR PREVENTING COLLAPSING OF, TUBULAR STRUCTURES OF THE BODY, e.g. STENTS; ORTHOPAEDIC, NURSING OR CONTRACEPTIVE DEVICES; FOMENTATION; TREATMENT OR PROTECTION OF EYES OR EARS; BANDAGES, DRESSINGS OR ABSORBENT PADS; FIRST-AID KITS (dental prosthetics A61C)
- F05D: INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS

## Abstract

Air Turbine Starters (ATSs) having oil feed shutoff valves are provided, as are gas turbine engines including ATSs. In one embodiment, the ATS includes an ATS housing assembly containing a sump chamber, an oil inlet, and a valve cavity. A rejected oil return passage is further formed in the ATS housing assembly and fluidly coupled to the valve cavity. An oil feed shutoff valve is positioned in the valve cavity and contains a valve element movable between open and closed positions. In the open position, the valve element permits oil flow from the oil inlet, through the valve cavity, and into the sump chamber. In the closed position, valve element blocks oil flow from the oil inlet into the sump chamber, while redirecting the oil flow into rejected oil return passage to reduce the loss of engine oil through the ATS in the event of an ATS housing breach.

## Claims

### Claim 1

An Air Turbine Starter (ATS), comprising:
an ATS housing assembly having a sump chamber, an oil inlet, and a valve cavity fluidly coupled between the sump chamber and the oil inlet;
a rejected oil return passage formed in the ATS housing assembly and fluidly coupled to the valve cavity;
an oil feed shutoff valve positioned in the valve cavity and containing a valve element movable between: (i) an open position in which the valve element permits oil flow from the oil inlet, through the valve cavity, and into the sump chamber, and (ii) a closed position in which valve element blocks oil flow from the oil inlet into the sump chamber, while redirecting the oil flow into the rejected oil return passage; and
a circumferential groove formed at least partially around the valve cavity, the circumferential groove fluidly coupled between the valve cavity and the oil inlet, the circumferential groove further fluidly coupled between the oil inlet and the rejected oil return passage.

### Claim 2 (depends on 1)

The ATS of claim 1 wherein the rejected oil return passage comprises an inlet and an outlet, the outlet of the rejected oil return passage formed in the ATS housing assembly at a vertical elevation higher than the inlet of the rejected oil return passage.

### Claim 3 (depends on 2)

The ATS of claim 2 wherein the ATS has a centerline, and wherein the rejected oil return passage comprises an elongated channel formed in the ATS housing assembly and angled with respect to a line parallel to the centerline of the ATS.

### Claim 4 (depends on 1)

The ATS of claim 1 wherein the valve element comprises a cylindrical sidewall, which covers the circumferential groove when the valve element is in the closed position.

### Claim 5 (depends on 1)

The ATS of claim 1 wherein the rejected oil return passage intersects a lower portion of the circumferential groove.

### Claim 6 (depends on 1)

The ATS of claim 1 wherein the oil feed shutoff valve further comprises:
a piston fixedly coupled to the valve element;
a control pressure chamber at least partially defined by the piston and the valve cavity, the control pressure chamber containing a first pressure urging movement of the valve element toward the open position; and
a reference pressure chamber at least partially defined by the piston and the valve cavity, the reference pressure chamber containing a second pressure urging movement of the valve element toward the closed position.

### Claim 7

An Air Turbine Starter (ATS) configured to be installed within a gas turbine engine containing an Accessory Gearbox (AGB), the ATS comprising:
an ATS housing assembly having a sump chamber, an oil inlet, and a valve cavity fluidly coupled between the sump chamber and the oil inlet;
a rejected oil return passage formed in the ATS housing assembly and fluidly coupled to the valve cavity;
an oil feed shutoff valve positioned in the valve cavity, the oil feed shutoff valve comprising:
a valve element movable between: (i) an open position in which the valve element permits oil flow from the oil inlet, through the valve cavity, and into the sump chamber, and (ii) a closed position in which valve element blocks oil flow from the oil inlet into the sump chamber, while redirecting the oil flow into the rejected oil return passage;
a piston fixedly coupled to the valve element;
a control pressure chamber at least partially defined by the piston and the valve cavity, the control pressure chamber containing a first pressure urging movement of the valve element toward the open position; and
a reference pressure chamber at least partially defined by the piston and the valve cavity, the reference pressure chamber containing a second pressure urging movement of the valve element toward the closed position; and
a reference pressure duct formed in the ATS housing and fluidly coupling the reference pressure chamber to the AGB when the ATS is installed within the gas turbine engine.

### Claim 8 (depends on 7)

The ATS of claim 7 wherein the reference pressure duct is fluidly isolated from the rejected oil return passage by the valve element.

### Claim 9 (depends on 7)

The ATS of claim 7 wherein the reference pressure duct intersects a bottom portion of the reference pressure chamber to permit drainage of engine oil leakage from the reference pressure chamber.

### Claim 10 (depends on 7)

The ATS of claim 7 wherein sump chamber comprises an air cavity containing an ATS air pressure, and wherein the oil feed shutoff valve control pressure chamber is fluidly coupled to the air cavity such that the first pressure is equivalent to the ATS air pressure.

### Claim 11

An Air Turbine Starter (ATS) configured to be installed within an engine cavity, the ATS comprising:
an ATS housing assembly containing a sump chamber and an oil inlet;
a valve cavity fluidly coupled between the sump chamber and the oil inlet;
a circumferential groove extending at least partially around the valve cavity;
an oil feed shutoff valve positioned in the valve cavity and containing a valve element having an annular sidewall, the oil feed shutoff valve movable between open and closed positions in which the annular sidewall uncovers and covers the circumferential groove, respectively, to selectively obstruct oil flow from the oil inlet, through the circumferential groove, and into the sump chamber; and
a rejected oil return passage fluidly coupled to the circumferential groove, the rejected oil return passage redirecting oil received at the oil inlet back to the engine cavity when the valve element is in the closed position.

### Claim 12 (depends on 11)

The ATS of claim 11 wherein the ATS is configured to be installed within an engine cavity containing an Accessory Gearbox (AGB) pressure, wherein the sump chamber contains an air cavity pressure, wherein the oil feed shutoff valve moves from the open position to the closed position when the air cavity pressure decreases below the AGB pressure by a predetermined amount.

### Claim 13 (depends on 12)

The ATS of claim 12 wherein the oil feed shutoff valve further comprises a piston fixedly coupled to the valve element and moving in conjunction therewith between open and closed positions, the piston comprising:
a first face exposed to the air cavity pressure; and
a second face opposite the first face and exposed to the AGB pressure.

### Claim 14 (depends on 11)

The ATS of claim 11 wherein the rejected oil return passage is fluidly coupled to the oil inlet of the ATS housing assembly through the circumferential groove such that oil flow is permitted from the oil inlet, around a portion of the annular sidewall, and to the rejected oil return passage when the valve element is in the closed position.

### Claim 15 (depends on 11)

The ATS of claim 11 wherein the rejected oil return passage comprises:
an inlet formed in the ATS housing assembly; and
an outlet fluidly coupled to the inlet of the rejected oil return passage, the outlet of the rejected oil return passage formed in the ATS housing assembly at a vertical elevation higher than the inlet of the rejected oil return passage such that a set head of oil urging the inflow of oil into the sump chamber is provided when the valve element is in the open position and the ATS operates under non-breach conditions.

### Claim 16 (depends on 11)

The ATS of claim 11 wherein the engine cavity contains an Accessory Gearbox (AGB) pressure, and wherein the ATS further comprises:
a reference pressure chamber; and
a reference pressure duct formed in the ATS housing assembly and placing the reference pressure chamber in fluid communication with the AGB pressure when the ATS is installed within the gas turbine engine.

### Claim 17 (depends on 16)

The ATS of claim 16 wherein the reference pressure duct is fluidly isolated from the rejected oil return passage by the valve element.

### Claim 18 (depends on 16)

The ATS of claim 16 wherein the reference pressure duct intersects a bottom portion of the reference pressure chamber to permit drainage of engine oil leakage therefrom.

### Claim 19 (depends on 16)

The ATS of claim 16 wherein the sump chamber comprises an air cavity containing an ATS air pressure, and wherein the ATS further comprises a control pressure chamber fluidly coupled to the ATS air pressure.

### Claim 20 (depends on 11)

The ATS of claim 11 wherein the ATS has a centerline, and wherein the rejected oil return passage comprises an elongated channel formed in the ATS housing assembly and angled with respect to a line parallel to the centerline of the ATS.