GB899913A - Improvements relating to monofuel reaction chamber apparatus - Google Patents
Improvements relating to monofuel reaction chamber apparatusInfo
- Publication number
- GB899913A GB899913A GB16334/60A GB1633460A GB899913A GB 899913 A GB899913 A GB 899913A GB 16334/60 A GB16334/60 A GB 16334/60A GB 1633460 A GB1633460 A GB 1633460A GB 899913 A GB899913 A GB 899913A
- Authority
- GB
- United Kingdom
- Prior art keywords
- valve
- reaction chamber
- pressure
- monofuel
- air
- 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
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/26—Starting; Ignition
- F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
- F02C7/27—Fluid drives
- F02C7/272—Fluid drives generated by cartridges
-
- 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
899,913. Generating combustion products under pressure. ASSOCIATED ELECTRICAL INDUSTRIES Ltd. April 19, 1961 [May 9, 1960], No. 16334/60. Class 51 (1). [Also in Group XXVI] The invention relates to apparatus for producing a flow of gaseous working fluid by the decomposition of monofuel within a reaction chamber, the gaseous fluid being utilized for example in a turbine starter for a gas turbine engine. The apparatus is shown in the Provisional Specification drawing and comprises a reaction chamber 1 which is supplied with monofuel from a tank 2 through ducting 3 which includes non-return valves 4, 5. Upon starting, air under pressure is supplied from a cartridge 9 through a non-return valve 8 to a shuttle valve 7. The valve is shown in Fig. 1 and comprises a body portion 20 containing a valve member 21 having an enlarged head 22 at its upper end and an enlarged head 23 secured at its lower end, the valve member having a longitudinal bore 24 and a transverse bore 25. The valve body portion 20 comprises a passage 26 which is connected to the air cartridge, a passage 29 which is connected to the reaction chamber 1, an outlet 28 connected to the low-pressure side of a pressure intensifier 9<SP>1</SP>, and a vent 30 open to atmosphere. The air supplied to the passage 26 at starting causes the shuttle valve 21 to rise until the head 23 abuts the shoulder 31 of the valve casing, and air then passes through passage 29 to the reaction chamber 1, also through outlet 28 to the pressure intensifier. The intensifier causes monofuel in the line 3 to pass into the reaction chamber through the atomizer 6, the monofuel mixing with the air supplied through the valve 7 and the mixture being ignited by a spark device. The pressure in the reaction chamber increases and so the shuttle valve 21 is caused to move downwardly, against the reducing pressure of air from the cartridge, to the position shown in Fig. 2 so cutting off the air supply which is vented to atmosphere. The pressure of gases within the reaction chamber is simultaneously applied to the low-pressure side of the pressure intensifier 9<SP>1</SP> through passage 29 and outlet 28 so maintaining the supply of monofuel through the line 3 and main fuel valve 10 to the reaction chamber, the valve 10 being opened by the pressure developed in the reaction chamber. An electrical control unit 11 is provided, operation of the unit causing air to be released from a cartridge 9, energizing the ignition device 14 and causing the by-pass valve 15 in the monofuel supply line to close. The high-pressure side of the pressure intensifier contains sufficient monofuel to enable a single starting operation to be performed. A stand-by cartridge 16 containing a deflagrant may be provided. Specifications 784,121, 787,572 and 816,752 are referred to.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB16334/60A GB899913A (en) | 1960-05-09 | 1960-05-09 | Improvements relating to monofuel reaction chamber apparatus |
US105668A US3095705A (en) | 1960-05-09 | 1961-04-26 | Monofuel reaction chamber apparatus |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB16334/60A GB899913A (en) | 1960-05-09 | 1960-05-09 | Improvements relating to monofuel reaction chamber apparatus |
Publications (1)
Publication Number | Publication Date |
---|---|
GB899913A true GB899913A (en) | 1962-06-27 |
Family
ID=10075418
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB16334/60A Expired GB899913A (en) | 1960-05-09 | 1960-05-09 | Improvements relating to monofuel reaction chamber apparatus |
Country Status (2)
Country | Link |
---|---|
US (1) | US3095705A (en) |
GB (1) | GB899913A (en) |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB816752A (en) * | 1955-02-04 | 1959-07-15 | British Thomson Houston Co Ltd | Improvements relating to monofuel reaction chamber apparatus |
FR947657A (en) * | 1947-05-20 | 1949-07-08 | Ile D Etude De La Propulsion P | Method and device for feeding the reaction chamber of a rocket-type reactor |
GB784121A (en) * | 1954-01-18 | 1957-10-02 | British Thomson Houston Co Ltd | Improvements in apparatus for generating a flow of gaseous working fluid for a primemover |
FR1150928A (en) * | 1955-05-27 | 1958-01-22 | Rotax Ltd | Combustion device for single fuel |
-
1960
- 1960-05-09 GB GB16334/60A patent/GB899913A/en not_active Expired
-
1961
- 1961-04-26 US US105668A patent/US3095705A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US3095705A (en) | 1963-07-02 |
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