Angled Core Engine

Patent metadata

Field	Value
Publication number	US-2016146104-A1
Application number	US-201414903609-A
Country	US
Kind code	A1
Filing date	Jun 12, 2014
Priority date	Jul 8, 2013
Publication date	May 26, 2016
Grant date	—

Abstract

A system, which may be used as a propulsion system, includes a propulsor section having a fluid operated device or free turbine, a fluid source such as a gas generator for creating an exhaust gas, and a fluid passageway for delivering the exhaust gas to the fluid operated device or free turbine. The fluid operated device may be used to drive a rotary device such as a fan.

First claim

What is claimed is:

1 . A system which comprises:
a propulsor section having a free turbine; a gas generator for creating an exhaust gas; and a fluid passageway for delivering said exhaust gas to said free turbine.

2 . The system of claim 1 , wherein said propulsor section further has a fan driven by said free turbine.

3 . The system of claim 2 , wherein said propulsor section further includes a casing surrounding said fan and a plurality of fan exit guide vanes located within said casing.

4 . The system of claim 2 , wherein said fan and said propulsor rotate about a first axis.

5 . The system of claim 4 , wherein said gas generator has a central axis and an angle between said first axis and said central axis is less than 90 degrees.

6 . The system according to claim 1 , wherein said fluid passageway comprises a plenum having an arcuately shaped conduit connected to an outlet of said gas generator and said exhaust gas flowing through said plenum turning less than 90 degrees prior to being delivered to said free turbine.

7 . The system of claim 1 , wherein said fluid passageway comprises a conduit connected to an outlet of said gas generator and having a curved section for turning said exhaust gas flow less than 90 degrees prior to being delivered to said free turbine.

8 . The system of claim 1 , further comprising said gas generator having an inlet and an air intake communicating with said inlet to deliver ambient air to said gas generator.

9 . The system of claim 2 , further comprising said gas generator having an inlet and said inlet ingesting air from said fan.

10 . The system of claim 1 , wherein said gas generator has a compressor section and a turbine section.

11 . The system of claim 10 , wherein said compressor section has at least one stage, and said turbine section has at least one stage.

12 . A method for delivering a fluid to a fluid operated device of a gas turbine engine, said method comprising the steps of:
providing a fluid source; providing a fluid flow generating device; flowing air through said fluid flow generating device in a first direction; and delivering a fluid produced by said fluid source to said fluid operated device of said gas turbine engine by turning said fluid exiting said fluid source so that said fluid flows in the first direction.

13 . The method of claim 12 , further comprising:
arranging said fluid operated device to rotate about a first axis; and orienting said fluid source so that a central axis of said fluid source is at an angle with respect to said first axis.

14 . The method of claim 13 , wherein said orienting step comprises orienting said fluid source so that said angle with respect to said first axis is less than 90 degrees.

15 . The method of claim 12 , wherein said turning of said fluid is carried out by a plenum with an arcuately shaped conduit connected to an outlet of said fluid source.

16 . The method of claim 15 , further comprising arranging said plenum between said rotary device and said fluid operated device.

17 . The method of claim 12 , wherein said turning of said fluid is carried out by a passageway connected to an outlet of said fluid source having a curved section.

18 . The method of claim 17 , further comprising positioning said passageway between said outlet of said fluid source and an inlet of said fluid operated device.

19 . The method of claim 12 , wherein said turning step comprises turning said fluid less than 90 degrees.

20 . The method of claim 12 , further comprising using said fluid operated device to drive said fluid flow generating device.

21 . The method of claim 12 , wherein said step of providing a fluid source comprises providing a gas generator.

22 . The method of claim 12 , further comprising supplying said fluid source with fluid created by said fluid flow generating device.

Assignees

• United Technologies Corp

Inventors

• Penda Allan R
• Chandler Jesse M
• Suciu Gabriel L

Classifications

• F01D9/041

  using blades (F01D5/148 takes precedence) · CPC title

• F05D2210/43

  Radial inlet and axial outlet · CPC title

• F05D2220/327

  to drive shrouded, high solidity propeller · CPC title

• F01D9/06

  Fluid supply conduits to nozzles or the like · CPC title

• F02C3/10

  with another turbine driving an output shaft but not driving the compressor · CPC title