Turboshaft engines having improved inlet particle scavenge systems and methods for the manufacture thereof

Patent metadata

Field	Value
Publication number	US-9500129-B2
Application number	US-201213663281-A
Country	US
Kind code	B2
Filing date	Oct 29, 2012
Priority date	Oct 29, 2012
Publication date	Nov 22, 2016
Grant date	Nov 22, 2016

Abstract

Embodiments of a turboshaft engine are provided, as are embodiments of a method for manufacturing a turboshaft engine. In one embodiment, the turboshaft engine includes an Inlet Particle Separator (IPS) system having an IPS scavenge flow circuit fluidly coupled to the engine's inlet section. A heat exchanger and a heat exchanger bypass duct are fluidly coupled to the IPS scavenge flow circuit. The heat exchanger bypass duct is configured to direct airflow around the heat exchanger. A particle separation device, such as an IPS blower, is fluidly coupled in series with the heat exchanger in the IPS scavenge flow circuit. The particle separation device is positioned to direct particulate matter entrained within the airflow through the IPS scavenge flow circuit into an inlet of the heat exchanger bypass duct and thereby reduce the amount of particulate matter ingested by the heat exchanger during operation of the turboshaft engine.

First claim

What is claimed is:

1. A turboshaft engine, comprising:
an inlet section; and
an Inlet Particle Separator (IPS) system, comprising:
an IPS scavenge flow circuit fluidly coupled to the inlet section;
a heat exchanger fluidly coupled to the IPS scavenge flow circuit and configured to receive airflow therefrom;
an IPS blower mounted in the IPS scavenge flow circuit and having a plurality of fan blades; and
a heat exchanger bypass duct having an inlet upstream of the heat exchanger and having an outlet downstream of the heat exchanger, the heat exchanger bypass duct directing airflow received at the inlet around the heat exchanger; and
an inner conduit extending from a location immediately downstream of the fan blades to the heat exchanger to at least partially define the heat exchanger bypass duct.

2. The turboshaft engine of claim 1 , wherein the IPS blower is mounted through a wall of the inner conduit.

3. The turboshaft engine of claim 2 wherein the inlet of the heat exchanger bypass duct is fluidly coupled between the IPS blower and the heat exchanger.

4. The turboshaft engine of claim 3 wherein the IPS blower comprises blade tips generally aligning with the inlet of the heat exchanger bypass duct, as taken along the longitudinal axis of the IPS scavenge flow circuit at a location of the axial fan.

5. The turboshaft engine of claim 2 wherein the IPS system further comprises:
an outer conduit further defining the IPS scavenge flow circuit;
wherein the inner conduit is located within the outer conduit and extends along a portion of a length thereof.

6. The turboshaft engine of claim 5 , wherein the heat exchanger is mounted within the outer conduit adjacent a downstream end of the inner conduit.

7. The turboshaft engine of claim 1 wherein the heat exchanger comprises one of the group consisting of an oil cooler and a fuel cooler.

8. The turboshaft engine of claim 1 further comprising an IPS exhaust immediately downstream of the heat exchanger and into which the outlet of the heat exchanger bypass duct discharges contaminated bypass airflow.

9. The turboshaft engine of claim 1 , wherein a leading edge of the inner conduit defines a splitter structure configured to divide the airflow through the IPS scavenge flow circuit into a contaminated bypass stream and a clean core stream directed into the heat exchanger bypass duct and into the heat exchanger, respectively.

10. The turboshaft engine of claim 9 , wherein the inner conduit defines a core airflow path configured to supply the clean core stream to the heat exchanger, and wherein a cross-sectional flow area of the core airflow path is greater than a cross-sectional flow area of the heat exchanger bypass duct.

11. The turboshaft engine of claim 9 , wherein the leading edge of the inner conduit has an enlarged circumferential lip.

12. The turboshaft engine of claim 1 , wherein a leading edge portion of the inner conduit curves radially inward toward a centerline of the IPS scavenge flow circuit.

13. A turboshaft engine, comprising:
an inlet section; and
an Inlet Particle Separator (IPS) system, comprising:
an IPS scavenge flow circuit fluidly coupled to the inlet section;
a heat exchanger disposed within the IPS scavenge flow circuit;
a heat exchanger bypass duct fluidly coupled to the IPS scavenge flow circuit and configured to direct a contaminated bypass stream around the heat exchanger; and

an IPS blower mounted through at least one wall of the heat exchanger bypass duct at a location substantially adjacent and upstream of the heat exchanger, the IPS blower configured to generate centrifugal forces during operation urging particulate matter entrained in the airflow through the IPS scavenge flow circuit into the heat exchanger bypass duct to reduce an amount of particulate matter ingested by the heat exchanger during operation of the turboshaft engine.

14. A turboshaft engine, comprising:
an inlet section; and
an Inlet Particle Separator (IPS) system, comprising:
an IPS scavenge flow circuit fluidly coupled to the inlet section;
a heat exchanger fluidly coupled to the IPS scavenge flow circuit;
an outer conduit within which the heat exchanger is mounted;
an inner conduit extending within the outer conduit to the heat exchanger and defining, at least in part, a clean core airflow path through which airflow is directed into the heat exchanger; and
a heat exchanger bypass duct at least partially defined by the inner conduit and the outer conduit, the heat exchanger bypass duct configured to direct a contaminated airflow bypass stream around the heat exchanger during operation of the turboshaft engine.

15. The turboshaft engine of claim 14 wherein the heat exchanger comprises inlet and outlet flow passages extending through the heat exchanger bypass duct.

16. The turboshaft engine of claim 14 wherein the IPS system further comprises an IPS exhaust into which the heat exchanger bypass duct and the heat exchanger each discharge airflow.

17. The turboshaft engine of claim 14 further comprising a particle separation device mounted in the outer conduit at a location immediately upstream of the inner conduit and the heat exchanger bypass duct.

18. The turboshaft engine of claim 14 further comprising an IPS blower having fan blades positioned immediately upstream of the inner conduit and the heat exchanger bypass duct.

19. The turboshaft engine of claim 18 wherein IPS blower comprises an elongated shaft mounted at an acute angle with respect to a centerline of the IPS scavenge flow circuit.

20. The turboshaft engine of claim 14 wherein the inner conduit comprises a downstream end portion, which sealingly abuts the heat exchanger.

Assignees

• Honeywell Int Inc

Inventors

• Schmittenberg Marc
• Hesano Brian
• Glascoe Lee
• Sheoran Yogendra Yogi

Classifications

• Y10T29/4932

  Turbomachine making · CPC title

• B64D33/02 Primary

  of combustion air intakes · CPC title

• F02C7/05 Primary

  having provisions for obviating the penetration of damaging objects or particles · CPC title

• B64D2033/0246

  comprising particle separators · CPC title