GB659793A - Improvements in or relating to means for securing stabilised burning of fuel in fast-moving air or gas streams - Google Patents
Improvements in or relating to means for securing stabilised burning of fuel in fast-moving air or gas streamsInfo
- Publication number
- GB659793A GB659793A GB1764144A GB1764144A GB659793A GB 659793 A GB659793 A GB 659793A GB 1764144 A GB1764144 A GB 1764144A GB 1764144 A GB1764144 A GB 1764144A GB 659793 A GB659793 A GB 659793A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fuel
- stabilised
- burning
- securing
- relating
- 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
-
- 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)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pre-Mixing And Non-Premixing Gas Burner (AREA)
Abstract
659,793. Jet propulsion engines. POWER JETS (RESEARCH & DEVELOPMENT) Ltd. Sept. 14, 1944, No. 17641. Divided out of Complete Specification of 659,794. [Class 110(iii)] In a gas turbine jet propulsion engine having a variable area propelling nozzle and means to inject reheat fuel into the turbine exhaust duct, the control means of the reheat fuel and the variable area propelling nozzle are inter-related. Reheat fuel is injected into the exhaust duct 9 of a gas turbine by one or more fuel jets 12 mounted on the fairing 8. The propelling nozzle 37 is fitted with a cone 38 axial movement of which varies its area. The reheat fuel supplied by a pump 40 is controlled by a valve 31. When the valve 31 is opened, the fuel pressure acting on the piston 34 moves the cone 38.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1764144A GB659793A (en) | 1944-09-14 | 1944-09-14 | Improvements in or relating to means for securing stabilised burning of fuel in fast-moving air or gas streams |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1764144A GB659793A (en) | 1944-09-14 | 1944-09-14 | Improvements in or relating to means for securing stabilised burning of fuel in fast-moving air or gas streams |
Publications (1)
Publication Number | Publication Date |
---|---|
GB659793A true GB659793A (en) | 1951-10-31 |
Family
ID=10098688
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1764144A Expired GB659793A (en) | 1944-09-14 | 1944-09-14 | Improvements in or relating to means for securing stabilised burning of fuel in fast-moving air or gas streams |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB659793A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE955733C (en) * | 1953-03-20 | 1957-01-10 | Materiels Hispano Suiza S A So | Recoil thrusters with devices controlled by servo fuel pressure |
-
1944
- 1944-09-14 GB GB1764144A patent/GB659793A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE955733C (en) * | 1953-03-20 | 1957-01-10 | Materiels Hispano Suiza S A So | Recoil thrusters with devices controlled by servo fuel pressure |
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