Exhaust mixer for wave rotor assembly

Patent metadata

Field	Value
Publication number	US-10443493-B2
Application number	US-201615041191-A
Country	US
Kind code	B2
Filing date	Feb 11, 2016
Priority date	Feb 11, 2015
Publication date	Oct 15, 2019
Grant date	Oct 15, 2019

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.

First claim

What is claimed is:

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, the exit duct including a first duct wall and a second duct wall spaced apart circumferentially from the first duct wall to define a portion of the duct passage, and
an exhaust mixer located in the duct passage and arranged to circumferentially redirect relatively-high velocity exhaust gasses received by the exhaust mixer in the exit duct toward relatively-low velocity exhaust gasses received by a remainder of the exit duct so that the relatively-high velocity exhaust gasses are mixed with the relatively-low velocity exhaust gasses in the duct passage downstream of the exhaust mixer,
wherein the exhaust mixer includes a first radial sidewall that extends axially and circumferentially at an angle away from the first duct wall toward the second duct wall only partway into the duct passage relative to the central axis, the exhaust mixer being angled with respect to the remainder of the exit duct to redirect the relatively-high velocity exhaust gasses toward the relatively-low velocity exhaust gasses, the exhaust mixer having a converging area to accelerate the relatively-high velocity exhaust gasses.

2. The wave rotor assembly of claim 1 , 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.

3. The wave rotor assembly of claim 2 , 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.

4. The wave rotor assembly of claim 2 , 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.

5. The wave rotor assembly of claim 4 , 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.

6. 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.

7. The wave rotor assembly of claim 6 , 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.

8. The wave rotor assembly of claim 7 , wherein the relatively-high velocity exhaust gasses exit the exhaust mixer through the outlet aperture at a supersonic velocity.

9. The wave rotor assembly of claim 6 , 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.

10. 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 circumferentially redirect relatively-high velocity exhaust gasses received by the exhaust mixer in the exit duct toward relatively-low velocity exhaust gasses received by a remainder of the exit duct so that the relatively-high velocity exhaust gasses are mixed with the relatively-low velocity exhaust gasses in the duct passage downstream of the exhaust mixer,
wherein the exhaust mixer is formed to include a mixer passage extending through the exhaust mixer angled with respect to the remainder of the exit duct, 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 to accelerate the relatively-high velocity exhaust gasses.

11. The wave rotor assembly of claim 10 , 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.

12. The wave rotor assembly of claim 10 , 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.

13. The wave rotor assembly of claim 12 , 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.

14. The wave rotor assembly of claim 10 , 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.

15. The wave rotor assembly of claim 14 , 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.

16. The wave rotor assembly of claim 10 , wherein the relatively-high velocity exhaust gasses exit the exhaust mixer through the outlet aperture at a local sonic velocity.

17. 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

Assignees

• Rolls Royce Nam Tech Inc

Inventors

• Emmerson Calvin W
• Snyder Philip H

Classifications

• F01N13/1805

  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 title

• F23R3/56

  Combustion chambers having rotary flame tubes · CPC title

• F02C3/16

  the combustion chambers being formed at least partly in the turbine rotor {or in an other rotating part of the plant} · CPC title

• F02C3/14 Primary

  characterised by the arrangement of the combustion chamber in the plant (combustion chambers per se F23R; F02C3/205 takes precedence) · CPC title

• F02C5/04

  the combustion chambers being formed at least partly in the turbine rotor · CPC title