Bifurcated ducts including plenums for stabilizing flow therethrough and exhaust systems including the same

Patent metadata

Field	Value
Publication number	US-9969500-B2
Application number	US-201414174422-A
Country	US
Kind code	B2
Filing date	Feb 6, 2014
Priority date	Feb 6, 2014
Publication date	May 15, 2018
Grant date	May 15, 2018

Abstract

Plenums for bifurcated ducts and bifurcated ducts are provided for stabilizing flow therethrough. The plenum comprises an outer cylindrical body intersected by a pair of exhaust duct stubs that are configured to be coupled to a corresponding pair of exhaust ducts and an inner body. The outer cylindrical body includes an axial rear end portion. The inner body is disposed in the axial rear end portion and increases in diameter in the aft direction. The inner body comprises one of a generally axi-symmetrical inner body or a non-axi-symmetrical inner body. The bifurcated duct comprises the plenum and the pair of exhaust ducts. Exhaust systems are also provided.

First claim

What is claimed is:

1. A bifurcated duct, configured to receive combustion products from gas turbine engine, comprising:
a mirror symmetric plenum comprising:
an outer cylindrical body that extends along a longitudinal axis that is intersected by a pair of exhaust duct stubs that are joined to a corresponding pair of exhaust ducts at a fixed orientation, wherein the outer cylindrical body includes an inlet at an axial front end portion and an axial rear end portion opposite the inlet, and wherein the pair of exhaust duct stubs extend radially outward from the longitudinal axis; and
an inner body disposed in the axial rear end portion, wherein the inner body is frustoconical and increases in diameter in an aft direction, the inner body having a first end defined at the axial rear end portion and a second end opposite the first end,
wherein the second end extends into the outer cylindrical body towards the inlet and is spaced a distance apart from the inlet to define a chamber in the outer body between the inlet and the second end of the inner body, the chamber of the outer body has a first internal volume that is greater than a second internal volume of the outer body defined between the second end of the inner body and the axial rear end portion; and
wherein the inlet receives the combustion products and each of the pair of exhaust ducts directs the combustion products in an axial direction.

2. The bifurcated duct of claim 1 , wherein the inner body and the outer cylindrical body cooperate to form the mirror symmetric plenum, wherein the mirror symmetric plenum is a seamless unitary plenum.

3. The bifurcated duct of claim 1 , wherein the inner body is coupled to the outer cylindrical body to form the mirror symmetric plenum.

4. The bifurcated duct of claim 1 , wherein the outer cylindrical body and the inner body are co-axially disposed.

5. The bifurcated duct of claim 1 , wherein the mirror symmetric plenum is configured to be disposed between a diffuser in an exhaust section of the gas turbine engine and the pair of exhaust ducts.

6. The bifurcated duct of claim 1 , wherein an inner surface of the outer cylindrical body is contoured to define a rounded fillet where intersected by the pair of exhaust duct stubs.

7. The bifurcated duct of claim 1 , wherein the inner body comprises one of a hollow body, a solid body, or a substantially solid body.

8. The bifurcated duct of claim 5 , wherein the gas turbine engine propels an aircraft.

9. An exhaust system for an aircraft comprising:
a gas turbine engine comprising an exhaust section including a diffuser for exhausting combustion products from the gas turbine engine; and
a bifurcated exhaust duct downstream of the diffuser, the bifurcated exhaust duct comprising:
a mirror symmetric plenum comprising:
an outer cylindrical body that extends along a longitudinal axis that is intersected by a pair of exhaust duct stubs that are joined to a corresponding pair of exhaust ducts at a fixed orientation, wherein the outer cylindrical body includes an inlet at an axial front end portion and an axial rear end portion opposite the inlet, and wherein the pair of exhaust duct stubs extend radially outward from the longitudinal axis; and
an inner body disposed in the axial rear end portion, wherein the inner body is frustoconical and increases in diameter in an aft direction, the inner body having a first end defined at the axial rear end portion and a second end opposite the first end,
wherein the second end extends into the outer cylindrical body towards the inlet and is spaced a distance apart from the inlet to define a chamber in the outer body between the inlet and the second end of the inner body, the chamber of the outer body has a first internal volume that is greater than a second internal volume of the outer body defined between the second end of the inner body and the axial rear end portion; and
wherein the inlet receives the combustion products and each of the pair of exhaust ducts directs the combustion products in an axial direction.

10. The exhaust system of claim 9 , wherein the bifurcated exhaust duct comprises a seamless unitary structure.

11. The exhaust system of claim 9 , wherein the mirror symmetric plenum comprises a seamless unitary plenum or a plenum assembly comprising the inner body coupled to the outer cylindrical body.

Assignees

• Honeywell Int Inc

Inventors

• Anderson Morris
• Sheoran Yogendra Yogi
• Hollingshead Doug

Classifications

• B64D33/04 Primary

  of exhaust outlets or jet pipes · CPC title

• F01D25/30

  Exhaust heads, chambers, or the like · CPC title

• F05D2220/324

  to drive unshrouded, low solidity propeller · CPC title

• F05D2250/232

  conical · CPC title