JPS54130717A - Gas turbine - Google Patents

Gas turbine

Info

Publication number
JPS54130717A
JPS54130717A JP3665378A JP3665378A JPS54130717A JP S54130717 A JPS54130717 A JP S54130717A JP 3665378 A JP3665378 A JP 3665378A JP 3665378 A JP3665378 A JP 3665378A JP S54130717 A JPS54130717 A JP S54130717A
Authority
JP
Japan
Prior art keywords
liquid fuel
heat exchanger
feed system
atomized air
heating
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP3665378A
Other languages
Japanese (ja)
Inventor
Kazuhiko Kumada
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hitachi Ltd
Original Assignee
Hitachi Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hitachi Ltd filed Critical Hitachi Ltd
Priority to JP3665378A priority Critical patent/JPS54130717A/en
Publication of JPS54130717A publication Critical patent/JPS54130717A/en
Pending legal-status Critical Current

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Landscapes

  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

PURPOSE: To efficiently heat liquid fuel without using outside electric power, by simultaneously performing the heating of liquid fuel and the cooling of atomized air by mounting a heat exchanger between a liquid fuel feed system and an atomized air feed system.
CONSTITUTION: A heat exchanger 16 is installed between a liquid fuel feed system A and an atomized air feed system B, and functions as heating at the system A and as cooling at the system B. The heating temperature of liquid fuel in the heat exchanger 16 is controlled by adjusting a flow rate of atommized air by the action of a temperature detector 17 at an outlet for the liquid fuel of the heat exchanger 16 and a flow rate adjusting valve 18 located between an inlet and an outlet for the atomized air of the heat exchanger 16.
COPYRIGHT: (C)1979,JPO&Japio
JP3665378A 1978-03-31 1978-03-31 Gas turbine Pending JPS54130717A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3665378A JPS54130717A (en) 1978-03-31 1978-03-31 Gas turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3665378A JPS54130717A (en) 1978-03-31 1978-03-31 Gas turbine

Publications (1)

Publication Number Publication Date
JPS54130717A true JPS54130717A (en) 1979-10-11

Family

ID=12475805

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3665378A Pending JPS54130717A (en) 1978-03-31 1978-03-31 Gas turbine

Country Status (1)

Country Link
JP (1) JPS54130717A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140060057A1 (en) * 2012-09-05 2014-03-06 General Electric Company Method and apparatus for heating liquid fuel supplied to a gas turbine combustor

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140060057A1 (en) * 2012-09-05 2014-03-06 General Electric Company Method and apparatus for heating liquid fuel supplied to a gas turbine combustor
US9057327B2 (en) * 2012-09-05 2015-06-16 General Electric Company Method and apparatus for heating liquid fuel supplied to a gas turbine combustor

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