EXHAUST MIXER FOR WAVE ROTOR ASSEMBLY

• US 20160230656A1
• Filed: 02/11/2016
• Published: 08/11/2016
• Est. Priority Date: 02/11/2015
• Status: Active Grant

• Current Assignee: Rolls-Royce North American Technologies, Inc. (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce North American Technologies, Inc. (Rolls-Royce Holdings Plc)
• Inventors: Emmerson, Calvin W., Snyder, Philip H.
• Granted Patent: US 10,443,493 B2
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: F01D 9/023 Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
• CPC Class Codes: F01N 13/1805 Fixing exhaust manifolds, exhaust pipes or pipe sections to each other, to engine or to vehicle body pipe joints in general F16L; fixing auxiliaries in motor vehicles in general B60K
• CPC Class Codes: F02C 3/14 characterised by the arrangement of the combustion chamber in the plant combustion chambers per se F23R; F02C3/205 takes precedence
• CPC Class Codes: F02C 3/16 the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant
• CPC Class Codes: F02C 5/04 the combustion chambers being formed at least partly in the turbine rotor
• CPC Class Codes: F05D 2250/323 convergent
• CPC Class Codes: F05D 2260/2212 by creating turbulence vortex generators, turbulators or the like for mixing F05D2240/127
• CPC Class Codes: F23R 3/56 Combustion chambers having rotary flame tubes
• CPC Class Codes: F23R 7/00 Intermittent or explosive combustion chambers
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A wave rotor assembly includes a wave rotor combustor and an exit duct. The wave rotor combustor includes an aft plate formed to include an exit port and a rotor drum mounted for rotation relative to the aft plate. The rotor drum is formed to include a plurality of rotor passages arranged to align with the exit port during rotation of the rotor drum. The exit duct is coupled to the aft plate and defines a passage arranged to receive exhaust gasses flowing through the exit port.

Claims

1. A wave rotor assembly comprising

a wave rotor combustor including an aft plate formed to include an exit port that extends circumferentially along an arc about a central axis of the wave rotor combustor and a rotor drum mounted for rotation relative to the aft plate about the central axis, the rotor drum formed to include a plurality of rotor passages that extend along the central axis and are arranged so that the rotor passages align with the exit port at predetermined intervals when the rotor drum rotates about the central axis to allow exhaust gasses in the rotor passages to flow through the exit port,

an exit duct coupled to the aft plate that defines a duct passage arranged to receive the exhaust gasses flowing through the exit port, and

an exhaust mixer located in the duct passage and arranged to circumferentially redirect relatively-high velocity exhaust gasses received by the exit duct toward relatively-low velocity exhaust gasses received by the exit duct so that the relatively-high velocity exhaust gasses are mixed with the relatively-low velocity exhaust gasses in the duct passage.

2. The wave rotor assembly of claim 1, wherein the exhaust mixer includes a first sidewall that extends axially and circumferentially into the duct passage relative to the central axis to redirect the relatively-high velocity exhaust gasses toward the relatively-low velocity exhaust gasses.

3. The wave rotor assembly of claim 2, wherein the exhaust mixer further includes a second sidewall spaced apart circumferentially from the first sidewall and the second sidewall extends axially and circumferentially into the duct passage to redirect the relatively-high velocity exhaust gasses toward the relatively-low velocity exhaust gasses.

4. The wave rotor assembly of claim 3, wherein the second sidewall includes a forward leg that extends axially into the duct passage and an aft leg that extends from the forward leg axially and circumferentially into the duct passage.

5. The wave rotor assembly of claim 3, wherein the exhaust mixer further includes a radial outer wall and a radial inner wall spaced apart radially from the radial outer wall relative to the central axis and the radial outer wall and the radial inner wall extend between and interconnect the first and second sidewalls to form a mixer passage extending through the exhaust mixer.

6. The wave rotor assembly of claim 5, wherein the exhaust mixer includes a front end and a back end axially spaced apart from the front end relative to the central axis, a height of the first sidewall decreases from the front end to the back end, and a height of the second sidewall decreases from the front end to the back end.

7. The wave rotor assembly of claim 1, wherein the exhaust mixer forms a mixer passage extending through the exhaust mixer, an inlet aperture opening into the mixer passage, and an outlet aperture opening into the mixer passage.

8. The wave rotor assembly of claim 7, wherein the inlet aperture has an inlet area, the outlet aperture has an outlet area, and the inlet area is greater than the outlet area.

9. The wave rotor assembly of claim 8, wherein the relatively-high velocity exhaust gasses exit the exhaust mixer through the outlet aperture at a supersonic velocity.

10. The wave rotor assembly of claim 7, wherein the exhaust mixer has a front end adjacent to the inlet aperture and a back end axially spaced apart from the front end and the back end has a convoluted shape.

11. A wave rotor assembly comprising

a wave rotor combustor including an aft plate formed to include an exit port and a rotor drum mounted for rotation relative to the aft plate, the rotor drum formed to include a plurality of rotor passages arranged to align with the exit port during rotation of the rotor drum,

an exit duct coupled to the aft plate that defines a duct passage arranged to receive exhaust gasses flowing through the exit port, and

an exhaust mixer located in the duct passage and arranged to redirect the exhaust gasses received by the exit duct.

12. The wave rotor assembly of claim 11, wherein the exhaust mixer is arranged to redirect relatively-high velocity exhaust gasses received by the exit duct in a circumferential direction toward relatively-low velocity exhaust gasses received by the exit duct so that the relatively-high velocity exhaust gasses are mixed with the relatively-low velocity exhaust gasses in the duct passage.

13. The wave rotor assembly of claim 11, wherein the exhaust mixer includes a first sidewall that extends axially and circumferentially into the duct passage to redirect the relatively-high velocity exhaust gasses toward the relatively-low velocity exhaust gasses.

14. The wave rotor assembly of claim 13, wherein the exhaust mixer includes a second sidewall that is circumferentially spaced apart from the first sidewall and extends axially and circumferentially into the duct passage to redirect the relatively-high velocity exhaust gasses toward the relatively-low velocity exhaust gasses.

15. The wave rotor assembly of claim 11, wherein the exhaust mixer is formed to include a mixer passage extending through the exhaust mixer, an inlet aperture opening into the mixer passage, and an outlet aperture opening into the mixer passage, the inlet aperture has an inlet area, the outlet aperture has an outlet area, and the inlet area is greater than the outlet area.

16. The wave rotor assembly of claim 15, wherein the exhaust mixer includes a first sidewall, a second sidewall circumferentially spaced apart from the first sidewall, a radial outer wall, and a radial inner wall spaced apart radially from the radial outer wall relative to a central axis of the wave rotor combustor and the radial outer wall and the radial inner wall extend between and interconnect the first and second sidewalls between the front and back ends to define the mixer passage.

17. The wave rotor assembly of claim 16, wherein the exhaust mixer includes a front end and a back end axially spaced apart from the front end relative to the central axis, a height of the first sidewall decreases from the front end to the back end, and a height of the second sidewall decreases from the front end to the back end.

18. The wave rotor assembly of claim 15, wherein the relatively-high velocity exhaust gasses exit the exhaust mixer through the outlet aperture at a local sonic velocity.

19. A method of making a wave rotor assembly, the method comprising

providing a wave rotor, an exit duct, and an exhaust mixer, the wave rotor including an aft plate formed to include an exit port and a rotor drum mounted for rotation relative to the aft plate, the rotor drum formed to include a plurality of rotor passages arranged to align with the exit port at predetermined intervals during rotation of the rotor drum, and the exit duct defines a duct passage,

coupling the exit duct to the aft plate to cause the duct passage to be arranged to receive exhaust gasses flowing through the exit port, and

locating the exhaust mixer in the duct passage to redirect exhaust gasses received by the exit duct.

20. The method of claim 19, wherein the exit duct is arranged to receive relatively-low velocity exhaust gasses and relatively-high velocity exhaust gasses and the exhaust mixer is arranged to redirect the relatively-high velocity exhaust gasses received by the exit duct toward the relatively-low velocity exhaust gasses received by the exit duct so that the relatively-high velocity exhaust gasses are mixed with the relatively-low velocity exhaust gasses in the duct passage.