GB2069612B - Gas turbine power plant - Google Patents

Gas turbine power plant

Info

Publication number: GB2069612B
Authority: GB; United Kingdom
Prior art keywords: gas turbine; power plant; turbine power; plant; gas
Prior art date: 1980-02-15
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.): Expired

Application number

GB8005146A

Other versions

GB2069612A (en

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.)

Rolls Royce PLC

Original Assignee

Rolls Royce PLC

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.)

1980-02-15

Filing date

1980-02-15

Publication date

1983-06-22

1980-02-15 Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC

1980-02-15 Priority to GB8005146A priority Critical patent/GB2069612B/en

1981-08-26 Publication of GB2069612A publication Critical patent/GB2069612A/en

1983-06-22 Application granted granted Critical

1983-06-22 Publication of GB2069612B publication Critical patent/GB2069612B/en

Status Expired legal-status Critical Current

Classifications

- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/78—Other construction of jet pipes
- F02K1/80—Couplings or connections
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
- F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

Engineering & Computer Science (AREA)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Fluidized-Bed Combustion And Resonant Combustion (AREA)
Jet Pumps And Other Pumps (AREA)

GB8005146A 1980-02-15 1980-02-15 Gas turbine power plant Expired GB2069612B (en)

Priority Applications (1)

Application Number	Priority Date	Filing Date	Title
GB8005146A GB2069612B (en)	1980-02-15	1980-02-15	Gas turbine power plant

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
GB8005146A GB2069612B (en)	1980-02-15	1980-02-15	Gas turbine power plant

Publications (2)

Publication Number	Publication Date
GB2069612A GB2069612A (en)	1981-08-26
GB2069612B true GB2069612B (en)	1983-06-22

Family

ID=10511381

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
GB8005146A Expired GB2069612B (en)	1980-02-15	1980-02-15	Gas turbine power plant

Country Status (1)

Country	Link
GB (1)	GB2069612B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE07873413T1 (en)	2006-06-09	2009-07-30	Bell Helicopter Textron, Inc., Fort Worth	ENGINE EXHAUST SYSTEM WITH DIRECTIONAL NOZZLE
WO2008097247A2 (en)	2006-06-09	2008-08-14	Bell Helicopter Textron Inc.	Engine exhaust system

1980
- 1980-02-15 GB GB8005146A patent/GB2069612B/en not_active Expired

Also Published As

Publication number	Publication date
GB2069612A (en)	1981-08-26

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Legal Events

Date	Code	Title	Description
1984-10-24	PCNP	Patent ceased through non-payment of renewal fee