GB892143A - A combustion gas generator - Google Patents
A combustion gas generatorInfo
- Publication number
- GB892143A GB892143A GB2058/59A GB205859A GB892143A GB 892143 A GB892143 A GB 892143A GB 2058/59 A GB2058/59 A GB 2058/59A GB 205859 A GB205859 A GB 205859A GB 892143 A GB892143 A GB 892143A
- Authority
- GB
- United Kingdom
- Prior art keywords
- chamber
- combustion
- duct
- port
- pressure
- 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/02—Gas-turbine plants characterised by the use of combustion products as the working fluid using exhaust-gas pressure in a pressure exchanger to compress combustion-air
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Air Bags (AREA)
Abstract
892,143. Generating combustion products under pressure. LALONDE, R. Jan. 20, 1959 [Jan. 20, 1958], No. 2058/59. Class 51 (1). [Also in Group XXVI] A combustion gas generator comprises a rotor having a plurality of combustion chambers and a non-rotary means of leading gas to and from the combustion chambers, air under pressure supplied to one chamber being further compressed by means of pressure developed in a second chamber in which combustion is taking place. The gas generator shown comprises a rotary assembly of five combustion chambers 62, 63, 64, 65, 66 mounted on a shaft 71 by means of support plates 69, 70 and having end plates 67, 68. The rotary assembly is supported within a cylindrical shell 43 having end closure plates 44, 45 with which the rotor assembly end-plates 67, 68 engage. The endplate 44 has two ports 47, 48, air under pressure from a compressor 75 being led through duct 49 to the port 47, while the port 48 is covered by a cap 50 having a fuel injection device 51 and an igniter 52. The end-plate 45 has five ports 53, 54, 55, 56, 57, the port 53 being a discharge port for high-pressure combustion gases, port 54 a discharge port for low-pressure combustion gases, 55 a scavenging port, and the ports 56 and 57 being interconnected by a duct 61. In the first position of a combustion chamber, say 65, air under pressure from the duct 49 blows through the chamber which is open to the scavenging duct 60 at its other end. In the second position of the chamber it is open to the interconnector duct 61, so that air or gases under pressure in the preceding chamber which is in full combustion act through the interconnector duct to further compress the air in the chamber 65. In the next position of the chamber 65 it is aligned with the cap 50, fuel is injected through injector 51 and combustion initiated by igniter 52, the resulting gases acting through the interconnector duct 61 to compress the air in the following chamber. In the next position, the chamber 65 is opened to the high-pressure discharge duct 58 and the gases pass to the gas-turbine 74 which drives the compressor 75, while in the final position, the chamber is opened to the low-pressure gas-discharge duct 59 and the gases pass to the gas-turbine 74 or to another point of use.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US892143XA | 1958-01-20 | 1958-01-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB892143A true GB892143A (en) | 1962-03-21 |
Family
ID=22216359
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2058/59A Expired GB892143A (en) | 1958-01-20 | 1959-01-20 | A combustion gas generator |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB892143A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2377257A (en) * | 2001-07-06 | 2003-01-08 | Hubert Michael Benians | Compound gas turbine engines |
-
1959
- 1959-01-20 GB GB2058/59A patent/GB892143A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2377257A (en) * | 2001-07-06 | 2003-01-08 | Hubert Michael Benians | Compound gas turbine engines |
WO2003004846A1 (en) * | 2001-07-06 | 2003-01-16 | Hubert Michael Benians | Compound gas turbine engines and methods of operation thereof |
GB2377257B (en) * | 2001-07-06 | 2004-09-01 | Hubert Michael Benians | Compound gas turbine engines and methods of operation thereof |
US7000402B2 (en) | 2001-07-06 | 2006-02-21 | Hubert Michael Benians | Compound gas turbine engines and methods of operation thereof |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP0371759A3 (en) | Intensifier-injector for gaseous fuel for positive displacement engines | |
ES2147715A2 (en) | Internal combustion engine with constant-volume independent combustion chamber | |
GB1367955A (en) | Rotary internal combustion engine | |
GB1436538A (en) | Manufacture of articles such as collapsible tubes | |
GB1495877A (en) | Combined gas/steam power plant with combustible gas producer | |
US2523379A (en) | Combustion products generator with combustion type precompressor | |
GB1037287A (en) | Hot gas generating installation | |
GB1023752A (en) | Improvements in or relating to an oscillating gas column combustion apparatus | |
GB892143A (en) | A combustion gas generator | |
GB781482A (en) | Gas turbine engine | |
GB1269123A (en) | Detonation apparatus | |
GB783913A (en) | Improved rotary engine | |
US3225539A (en) | Explosion inertia turbine engine | |
GB699166A (en) | Improvements in or relating to gas turbine plants | |
GB1429363A (en) | Rotary internal-combustion engine | |
GB1518098A (en) | Rotary internal combustion engines | |
ES323562A1 (en) | Rotating internal combustion engine | |
GB1178399A (en) | Rotary Piston Machines. | |
GB730383A (en) | Improvements in or relating to gas turbines | |
FR2406073A1 (en) | Gas turbine with combustion chambers controlled by valves - which are operated by cams mounted on main shaft | |
FR2252764A5 (en) | Rotary I.C. engine with several rotors - has pair of spring loaded pistons perpendicular to rotor shaft in each rotor | |
GB818063A (en) | Gas turbine plant acting as generator of gas under pressure | |
GB805786A (en) | Improvements in gas turbine plants associated with gas producers | |
GB104244A (en) | Improvements in and relating to Rotary Engines. | |
GB1491000A (en) | Rotary internal-combustion engines |