Integrated air cycle-gas turbine engine

• US 5,323,603 A
• Filed: 03/09/1993
• Issued: 06/28/1994
• Est. Priority Date: 11/09/1990
• Status: Expired due to Fees

• Current Assignee: Tiernay Turbines
• Original Assignee: Tiernay Turbines
• Inventors: Malohn, Donald A.
• Primary Examiner(s): Casaregola, Louis J.
• Application Number:
  US08/028,358
• Time in Patent Office: 476 Days
• Field of Search: 60/39.04, 60/39.07, 60/39.161, 60/39.17, 60/39.183, 60/39.511, 60/728
• US Class Current: 60/784
• CPC Class Codes: F02C 7/10 by means of regenerative heat-exchangers
• CPC Class Codes: F28D 9/0012 the apparatus having an annular form
• CPC Class Codes: F28D 9/0025 the conduits being formed by zig-zag bend plates
• CPC Class Codes: F28F 13/12 by creating turbulence, e.g. by stirring, by increasing the force of circulation F28F13/08 takes precedence
• CPC Class Codes: F28F 2265/26 for allowing differential expansion between elements
• CPC Class Codes: Y02E 20/14 Combined heat and power generation [CHP]
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

An additional turbine, an air-to-water heat exchanger, and an air-to-air heat exchanger are added upstream of a recuperated gas turbine engine. Incoming air at atmospheric temperature is expanded and cooled in the additional turbine and then passes through the air-to-water heat exchanger where it is used to cool warm water to a suitable drinking temperature. The cool air then passes through the air-to-air heat exchanger, where it precools the incoming atmospheric temperature air. The output shaft of the additional turbine is coupled to an additional compressor downstream of the original compressor of the engine, thus resulting in a higher net pressure ratio.

Claims

1. An integrated air cycle-gas turbine engine comprising:

a) air entry means for receiving air at atmospheric conditions;

b) a first turbine downstream of said air entry means for expanding and cooling said air;

c) an air-to-water heat exchanger downstream of said first turbine, said air-to-water heat exchanger including

i) air inlet means for admitting cooled expanded air from said first turbine;

ii) air outlet means for expelling said expanded air;

iii) water inlet means for admitting warm water;

iv) water outlet means for discharging said water; and

v) separator means for separating said expanded air from said water and conducting heat therebetween;

d) an air-to-air heat exchanger downstream of said air-to-water heat exchanger, said air-to-air heat exchanger including

i) first inlet means for receiving expanded air from said air outlet means of said air-to-water heat exchanger;

ii) first outlet means for discharging said expanded air;

iii) second inlet means communicating with said air entry means for receiving atmospheric air;

iv) second outlet means for discharging said atmospheric air into said first turbine; and

v) separator means for separating said expanded air from said atmospheric air and conducting heat therebetween;

e) a combustion chamber having means supplying fuel thereto;

f) a first compressor, driven by said first turbine, for supplying compressed air to said combustion chamber;

g) a second compressor, downstream of said air-to-air heat exchanger and upstream of said first compressor, for receiving expanded air from said first outlet means and pre-compressing said air prior to entry into said first compressor;

h) a second turbine, downstream of said combustion chamber, for extracting energy produced in said combustion chamber and driving said second compressor; and

i) a recuperator including

i) first inlet means for admitting compressed air from said first compressor;

ii) first outlet means for expelling said compressed air;

iii) second inlet means for admitting high temperature exhaust from said second turbine;

iv) second outlet means for expelling said exhaust; and

v) separator means for separating said compressed air from said turbine exhaust and for conducting heat therebetween.

2. An integrated air cycle-gas turbine engine according to claim 1, wherein said recuperator is a primary surface counterflow heat exchanger encircling said second turbine and said combustion chamber.