Full-area bleed valves
09689315 ยท 2017-06-27
Assignee
Inventors
- Francis P. Marocchini (Somers, CT, US)
- Aaron F. Rickis (Feeding Hills, MA, US)
- Glenn Gradischer (Canton, CT, US)
- Robert Goodman (West Hartford, CT, US)
Cpc classification
F16K1/126
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10T137/3367
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F04D27/023
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16K3/0254
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16K31/122
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D17/26
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16K31/0668
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16K3/0218
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16K31/124
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D17/105
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D27/0215
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F02C9/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16K31/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16K3/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D17/26
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16K31/122
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D27/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D17/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A bleed valve includes inlet and outlet housings, a hollow shaft defining a valve axis, and a full-area piston. The shaft includes a first end mounted to an inner diameter portion of the inlet housing and a second end mounted to an end cap of the outlet housing. The piston is slidably mounted to the shaft. A first chamber is defined between an upstream side of the piston and the inner diameter portion of the inlet housing. A second chamber is defined between a downstream side of the piston and the end cap of the outlet housing. An area of an upstream surface of the piston at an angle with respect to the valve axis is in fluid communication with the first chamber, and is substantially equal to an area of a downstream surface of the piston at an angle with respect to the valve axis and in fluid communication with the second chamber.
Claims
1. A bleed valve for a turbomachine comprising: an inlet housing; an outlet housing downstream of the inlet housing; a hollow shaft defining a valve axis having a first end mounted to an inner diameter portion of the inlet housing and a second end mounted to an end cap of the outlet housing, wherein a radial gap is defined around the entire periphery of the end cap between an outer diameter surface of the end cap and a portion of the outlet housing; a full-area piston slidably mounted to the shaft between the inlet housing and the end cap for movement between an open and a closed position; a first pressure chamber defined between an upstream side of the piston and the inner diameter portion of the inlet housing in fluid communication with an intermediate-pressure port; and a second pressure chamber defined between a downstream side of the piston and the end cap in fluid communication with a solenoid pressure port, wherein the solenoid pressure port is configured to connect to a solenoid pressure valve that controls the pressure in the second pressure chamber, wherein an area of an upstream surface of the piston at an angle with respect to the valve axis and in fluid communication with the first pressure chamber is substantially equal to an area of a downstream surface of the piston at an angle with respect to the valve axis and in fluid communication with the second pressure chamber.
2. A bleed valve as recited in claim 1, wherein the intermediate-pressure port is configured to connect to an intermediate-pressure source.
3. A bleed valve as recited in claim 1, wherein an intermediate pressure of the first pressure chamber is for driving the piston into the closed position and a solenoid pressure of the second pressure chamber is for driving the piston into the open position.
4. A bleed valve as recited in claim 1, wherein the piston includes inner and outer sleeves, and a conical portion connecting therebetween, wherein the conical portion converges in a downstream direction.
5. A bleed valve as recited in claim 4, wherein the outer sleeve of the piston includes a high-pressure seal ring at an interface between an outer diameter surface of the outer sleeve of the piston and an inner diameter surface of the inlet housing.
6. A bleed valve as recited in claim 4, wherein the end cap includes a seal ring at an interface between an outer diameter surface of the end cap and an inner diameter surface of the outer sleeve of the piston.
7. A bleed valve as recited in claim 1, further comprising a spring positioned in an interior of the first pressure chamber.
8. A bleed valve as recited in claim 1, wherein, in an open position, a conical end portion of an outer sleeve of the piston forms a substantially conical surface in conjunction with the end cap.
9. A bleed valve as recited in claim 1, wherein a downstream side of an inner diameter portion of the inlet housing is proximate to an upstream side of the end cap.
10. A bleed valve system for a gas turbine engine comprising: a valve mounted within a high-pressure bleed duct of the gas turbine engine, wherein the valve includes an intermediate-pressure chamber and a solenoid pressure chamber, wherein the valve includes an inlet housing and an outlet housing, wherein a downstream side of an inner diameter portion of the inlet housing is proximate to an upstream side of an end cap of the outlet housing, wherein a radial gap is defined around the entire periphery of the end cap between an outer diameter surface of the end cap and a portion of the outlet housing; a solenoid pressure valve in fluid communication with the solenoid pressure chamber for controlling the pressure in the solenoid pressure chamber; and an intermediate-pressure source in fluid communication with the intermediate-pressure chamber, wherein an intermediate pressure of the intermediate-pressure chamber is for driving a piston of the valve into a closed position and a solenoid pressure of the solenoid pressure chamber is for driving the piston into an open position.
11. A bleed valve system as recited in claim 10, wherein the intermediate-pressure source is an intermediate stage of the compressor.
12. A bleed valve for a turbomachine comprising: an inlet housing; an outlet housing downstream of the inlet housing; a hollow shaft defining a valve axis having a first end mounted to an inner diameter portion of the inlet housing and a second end mounted to an end cap of the outlet housing; a full-area piston slidably mounted to the shaft between the inlet housing and the end cap for movement between an open and a closed position, wherein the piston includes inner and outer sleeves, and a conical portion connecting therebetween, wherein the conical portion converges in a downstream direction; a first pressure chamber defined between an upstream side of the piston and the inner diameter portion of the inlet housing in fluid communication with an intermediate-pressure port; and a second pressure chamber defined between a downstream side of the piston and the end cap in fluid communication with a solenoid pressure port, wherein the solenoid pressure port is configured to connect to a solenoid pressure valve that controls the pressure in the second pressure chamber, wherein an area of an upstream surface of the piston at an angle with respect to the valve axis and in fluid communication with the first pressure chamber is substantially equal to an area of a downstream surface of the piston at an angle with respect to the valve axis and in fluid communication with the second pressure chamber, wherein an intermediate pressure of the first pressure chamber is for driving the piston into the closed position and a solenoid pressure of the second pressure chamber is for driving the piston into the open position.
13. A bleed valve as recited in claim 12, wherein the outer sleeve of the piston includes a high-pressure seal ring at an interface between an outer diameter surface of the outer sleeve of the piston and an inner diameter surface of the inlet housing.
14. A bleed valve for a turbomachine comprising: an inlet housing; an outlet housing downstream of the inlet housing; a hollow shaft defining a valve axis having a first end mounted to an inner diameter portion of the inlet housing and a second end mounted to an end cap of the outlet housing; a full-area piston slidably mounted to the shaft between the inlet housing and the end cap for movement between an open and a closed position, wherein the piston includes inner and outer sleeves, and a conical portion connecting therebetween, wherein the conical portion converges in a downstream direction; a first pressure chamber defined between an upstream side of the piston and the inner diameter portion of the inlet housing in fluid communication with an intermediate-pressure port; a spring positioned in an interior of the first pressure chamber; and a second pressure chamber defined between a downstream side of the piston and the end cap in fluid communication with a solenoid pressure port, wherein the solenoid pressure port is configured to connect to a solenoid pressure valve that controls the pressure in the second pressure chamber, wherein an area of an upstream surface of the piston at an angle with respect to the valve axis and in fluid communication with the first pressure chamber is substantially equal to an area of a downstream surface of the piston at an angle with respect to the valve axis and in fluid communication with the second pressure chamber.
15. A bleed valve as recited in claim 14, wherein the outer sleeve of the piston includes a high-pressure seal ring at an interface between an outer diameter surface of the outer sleeve of the piston and an inner diameter surface of the inlet housing.
16. A bleed valve for a turbomachine comprising: an inlet housing; an outlet housing downstream of the inlet housing; a hollow shaft defining a valve axis having a first end mounted to an inner diameter portion of the inlet housing and a second end mounted to an end cap of the outlet housing; a full-area piston slidably mounted to the shaft between the inlet housing and the end cap for movement between an open and a closed position, wherein the piston includes inner and outer sleeves, and a conical portion connecting therebetween, wherein the conical portion converges in a downstream direction, and wherein, in an open position, the conical end portion of the outer sleeve of the piston forms a substantially conical surface in conjunction with the end cap; a first pressure chamber defined between an upstream side of the piston and the inner diameter portion of the inlet housing in fluid communication with an intermediate-pressure port; and a second pressure chamber defined between a downstream side of the piston and the end cap in fluid communication with a solenoid pressure port, wherein the solenoid pressure port is configured to connect to a solenoid pressure valve that controls the pressure in the second pressure chamber, wherein an area of an upstream surface of the piston at an angle with respect to the valve axis and in fluid communication with the first pressure chamber is substantially equal to an area of a downstream surface of the piston at an angle with respect to the valve axis and in fluid communication with the second pressure chamber.
17. A bleed valve as recited in claim 16, wherein the outer sleeve of the piston includes a high-pressure seal ring at an interface between an outer diameter surface of the outer sleeve of the piston and an inner diameter surface of the inlet housing.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) So that those skilled in the art to which the subject disclosure appertains will readily understand how to make and use the devices and methods of the subject disclosure without undue experimentation, preferred embodiments thereof will be described in detail herein below with reference to certain figures, wherein:
(2)
(3)
(4)
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
(5) Reference will now be made to the drawings wherein like reference numerals identify similar structural features or aspects of the subject disclosure. For purposes of explanation and illustration, and not limitation, a partial view of an exemplary embodiment of a bleed valve constructed in accordance with the disclosure is shown in
(6) As shown in
(7) With reference now to
(8) The area of an upstream surface 132 of piston 116 at an angle with respect to valve axis A, is in fluid communication with first pressure chamber 118, and is substantially equal to the area of a downstream surface 134 of piston 116. Downstream surface 134 of piston 116 is also at an angle with respect to valve axis A and is in fluid communication with a second pressure chamber 124, described below. The substantial equality between the areas of the upstream and downstream surfaces 132 and 134, respectively, allow for a uniform and substantially symmetrical full-area piston configuration.
(9) Those skilled in the art will readily appreciate that the full-area piston configuration described above provides a more light weight, compact and controllable bleed valve, as compared with a half-area piston configuration, that reliably operates at elevated temperature and pressure. Additionally, the symmetric configuration found in full-area piston 116 provides an optimum configuration for high vibration environment over traditional half-area bleed valves that tend to include asymmetries and have a cantilevered configuration.
(10) With continued reference to
(11) As shown in
(12) In an open position, a conical end portion 162 of outer sleeve 142 of piston 116 forms a substantially conical surface 164 in conjunction with end cap 114. A downstream side 166 of an inner diameter portion 112 of inlet housing 102 is proximate to an upstream side 170 of end cap 114. The proximity of downstream side 166 and upstream side 170 is possible due to the smaller and more compact structure of piston 116, resulting in a smaller overall valve envelope.
(13) A shown in
(14) A method for controlling pressure within a gas turbine compressor stage includes moving a piston, e.g. piston 116, into an open position such that high-pressure fluid is free to flow through a housing body, e.g. inlet and outlet housings 102 and 104, respectively, and supplying intermediate-pressure fluid to a first fluid chamber, e.g. first chamber 118. The first fluid chamber is in fluid communication with an upstream surface, e.g. upstream surface 132, of the piston, thereby moving the piston into a closed position.
(15) By utilizing higher-pressure fluid from intermediate compressor stages, there is less wear on the closing ring, e.g. high-pressure seal ring 146, because of the lower pressure differential between the fluid from the low-pressure compressor stages and the high-pressure fluid from the high-pressure compressor stages, as compared to the wear on the closing ring of the traditional half-area bleed valves where the pressure differential between ambient fluid and the high-pressure compressor fluid is much greater.
(16) The method also includes supplying fluid pressure from a solenoid pressure valve, e.g. solenoid pressure valve 206, when the solenoid pressure valve is energized, into a second fluid chamber, e.g. second fluid chamber 124, in fluid communication with a downstream surface, e.g. downstream surface 134, of piston, thereby moving said piston into an open position. The method includes passing high-pressure fluid through the housing body while piston 116 is in the open position for a desired time and removing fluid pressure from the second fluid chamber, e.g. when the solenoid valve is de-energized, thereby causing a force imbalance between the upstream and downstream surfaces allowing the piston to return to the closed position.
(17) The methods and systems of the present disclosure, as described above and shown in the drawings, provide light weight, compact and controllable bleed valves that can operate at high temperatures and pressures. While the apparatus and methods of the subject disclosure have been shown and described with reference to preferred embodiments, those skilled in the art will readily appreciate that changes and/or modifications may be made thereto without departing from the spirit and scope of the subject disclosure.