GB782654A - Improvements in or relating to gas turbine engines - Google Patents
Improvements in or relating to gas turbine enginesInfo
- Publication number
- GB782654A GB782654A GB1701756A GB1701756A GB782654A GB 782654 A GB782654 A GB 782654A GB 1701756 A GB1701756 A GB 1701756A GB 1701756 A GB1701756 A GB 1701756A GB 782654 A GB782654 A GB 782654A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas turbine
- control means
- fuel
- reheat
- flow
- 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.)
- Expired
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C14/00—Alloys based on titanium
-
- 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
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/15—Control or regulation
- F02K1/16—Control or regulation conjointly with another control
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
782,654. Gas turbine jet-propulsion plant. ROLLS-ROYCE, Ltd. July 30,1954 [Sept. 14, 1953], No. 17017/56. Divided out of 782,653. Drawings to Specification. Class 110 (3). A gas turbine engine comprising reheat combustion equipment in which fuel is burnt in the exhaust gases before they pass to atmosphere has basic control means to vary the flow of reheat fuel in accordance with the compressor delivery pressure and trimming control means operative on the basic control means to modify the flow of reheat fuel so as to maintain the static or total head pressure or temperature respectively in the jet pipe in preselected relation to the compressor delivery pressure. The subject-matter of this Specification is identical with that described in Specification 782,653, but the claims differ. Specifications 641,910 and 748,353, [Group XXIX], also are referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1701756A GB782654A (en) | 1953-09-14 | 1953-09-14 | Improvements in or relating to gas turbine engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1701756A GB782654A (en) | 1953-09-14 | 1953-09-14 | Improvements in or relating to gas turbine engines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB782654A true GB782654A (en) | 1957-09-11 |
Family
ID=10087727
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1701756A Expired GB782654A (en) | 1953-09-14 | 1953-09-14 | Improvements in or relating to gas turbine engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB782654A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2172056A (en) * | 1985-03-04 | 1986-09-10 | Gen Electric | Means and method for controlling augmentor liner coolant flow pressure in a mixed flow, variable cycle gas turbine engine |
-
1953
- 1953-09-14 GB GB1701756A patent/GB782654A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2172056A (en) * | 1985-03-04 | 1986-09-10 | Gen Electric | Means and method for controlling augmentor liner coolant flow pressure in a mixed flow, variable cycle gas turbine engine |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB749176A (en) | Improvements relating to jet propulsion apparatus | |
GB943839A (en) | Jet propulsion engines | |
GB1116930A (en) | Improvements in cooled flameholder assembly | |
GB1415679A (en) | Gas turbine engine powerplant | |
GB657789A (en) | Improvements relating to liquid fuel combustion equipment for gas-turbine engines | |
GB774059A (en) | Improvements in or relating to combined gas turbine plant and ram-jet units | |
GB713783A (en) | Gas turbine propulsion units | |
GB992304A (en) | Apparatus for supplying air to a blast furnace | |
GB782654A (en) | Improvements in or relating to gas turbine engines | |
GB712633A (en) | Improvements relating to gas-turbine engines | |
GB586554A (en) | Improvements in or relating to turbines | |
GB1027845A (en) | Gas blast furnace pressurised by means of a gas turbine engine | |
GB699166A (en) | Improvements in or relating to gas turbine plants | |
GB851153A (en) | Gas turbine jet-propulsion engine of the by-pass type | |
GB1126163A (en) | Gas turbine by-pass engine | |
GB666944A (en) | Method of and means for controlling the outlet area of gas turbine jet propulsion engines, equipped with means for allowing an after-combustion | |
GB701320A (en) | Improvements in or relating to combustion equipment of gas-turbine engines | |
GB948571A (en) | Gas turbine jet propulsion engine | |
GB837497A (en) | Air intakes in aircraft engines | |
GB672660A (en) | Improvements relating to internal combustion power plants | |
GB683589A (en) | Improvements in or relating to power plants including an internal combustion engine and an exhaust-driven turbine | |
GB755945A (en) | Improvements in or relating to an internal combustion turbine | |
GB992931A (en) | Gas turbine jet propulsion engine | |
GB587612A (en) | Improvements in or relating to internal combustion turbine power plants | |
GB460794A (en) | Internal combustion turbine |