GB749921A - Improvements in fuel supply systems for reaction chambers - Google Patents
Improvements in fuel supply systems for reaction chambersInfo
- Publication number
- GB749921A GB749921A GB2923053A GB2923053A GB749921A GB 749921 A GB749921 A GB 749921A GB 2923053 A GB2923053 A GB 2923053A GB 2923053 A GB2923053 A GB 2923053A GB 749921 A GB749921 A GB 749921A
- Authority
- GB
- United Kingdom
- Prior art keywords
- chamber
- monofuel
- nozzle
- hot gases
- main chamber
- 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
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/60—Constructional parts; Details not otherwise provided for
- F02K9/68—Decomposition chambers
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physical Or Chemical Processes And Apparatus (AREA)
Abstract
749,921. Generating combustion products under pressure. BRITISH-THOMSONHOUSTON CO., Ltd. Oct. 22, 1954 [Oct. 22, 1953], No. 29230/53. Class 51(1). An apparatus for producing a flow of gaseous working fluid, which may be supplied for example to a turbo-starter of a prime mover, comprises an auxiliary reaction chamber 2 and a main reaction' chamber 1, hot gases produced by decomposition of a monofuel within the auxiliary chamber passing into the main chamber. The flow of hot gases is so directed upon admission to the main chamber as to impinge substantially directly upon a jet of monofuel injected into the main chamber whereby atomisation of the monofuel is effected. The hot gases issue into the main chamber 1 through a nozzle 5 which is disposed opposite the nozzle 6 through which the monofuel is injected. The gases from the main chamber pass through an outlet nozzle 7. The auxiliary chamber has a monofuel supply at 3 and a heater 4. The hot gases from the auxiliary chamber may alternatively be led through a pipe to the vicinity of the monofuel injected through the nozzle 6 in which case the nozzles 5 and 6 are not necessarily in alignment. Specifications 726,897, 731,977 and 749,920 are referred to.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2923053A GB749921A (en) | 1953-10-22 | 1953-10-22 | Improvements in fuel supply systems for reaction chambers |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2923053A GB749921A (en) | 1953-10-22 | 1953-10-22 | Improvements in fuel supply systems for reaction chambers |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB749921A true GB749921A (en) | 1956-06-06 |
Family
ID=10288203
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2923053A Expired GB749921A (en) | 1953-10-22 | 1953-10-22 | Improvements in fuel supply systems for reaction chambers |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB749921A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3059429A (en) * | 1958-03-25 | 1962-10-23 | Sunstrand Corp | Reaction chamber |
-
1953
- 1953-10-22 GB GB2923053A patent/GB749921A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3059429A (en) * | 1958-03-25 | 1962-10-23 | Sunstrand Corp | Reaction chamber |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB727720A (en) | Improvements in or relating to power units | |
| GB622513A (en) | Improvements in or relating to combustion apparatus | |
| GB579424A (en) | Improvements relating to liquid fuel combustion apparatus for generating gases for power purposes | |
| GB271706A (en) | Improvements in motive fluid generators for use particularly in torpedoes | |
| GB749921A (en) | Improvements in fuel supply systems for reaction chambers | |
| GB840914A (en) | Rocket engines | |
| GB733383A (en) | Improvements in and relating to fuel-reaction-chambers | |
| GB845676A (en) | An improved spraying device | |
| GB785210A (en) | Combustion chambers | |
| GB784122A (en) | Apparatus for generating a flow of gaseous working fluid for a prime mover | |
| GB676640A (en) | Vapourizing system for a gas turbine engine | |
| GB749670A (en) | Improvements in or relating to jet reaction motors | |
| GB733385A (en) | Improvements in and relating to fuel-reaction-chambers | |
| GB960056A (en) | Improvements in liquid fuel burners | |
| GB826861A (en) | Rocket motors | |
| GB726897A (en) | Improvements in apparatus for producing a supply of gaseous working fluid for a prime mover such as a turbo-starter for a gas turbine | |
| SE197021C1 (en) | ||
| GB626174A (en) | Improvements relating to combustion turbines | |
| GB1129403A (en) | Internal combustion engine | |
| GB789701A (en) | Improvements in or relating to oscillating column combustion apparatus | |
| GB932980A (en) | Combustion chambers for liquid fuels | |
| GB190827718A (en) | Improved Means for Producing a Gas under Pressure for Motive Power Purposes. | |
| GB832771A (en) | Ignition of gas turbine and jet propulsion engines | |
| GB777948A (en) | Improvements in or relating to combustion equipment for gas turbine engines | |
| GB1010407A (en) | Burner for thermally working minerals |