GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS (chemical aspects of gas production C06D 5/00; gas-turbine plants characterised by the arrangement of the combustion chamber in the plant F02C 3/14; arrangement of afterburners in jet-propulsion plants F02K 3/10; combustion chambers of rocket engine plants F02K 9/00; using such products for specific purposes, see the relevant classes for the purposes)
| Subclass | Title |
|---|---|
| 3/00 | Continuous combustion chambers using liquid or gaseous fuel |
| 3/02 | Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration (reverse-flow combustion chambers F23R 3/54; cyclone or vortex type combustion chambers F23R 3/58) |
| 3/04 | Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration (reverse-flow combustion chambers F23R 3/54; cyclone or vortex type combustion chambers F23R 3/58) Air inlet arrangements |
| 3/06 | Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration (reverse-flow combustion chambers F23R 3/54; cyclone or vortex type combustion chambers F23R 3/58) Air inlet arrangements Arrangement of apertures along the flame tube |
| 3/08 | Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration (reverse-flow combustion chambers F23R 3/54; cyclone or vortex type combustion chambers F23R 3/58) Air inlet arrangements Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections |
| 3/10 | Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration (reverse-flow combustion chambers F23R 3/54; cyclone or vortex type combustion chambers F23R 3/58) Air inlet arrangements for primary air (F23R 3/06 takes precedence) |
| 3/12 | Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration (reverse-flow combustion chambers F23R 3/54; cyclone or vortex type combustion chambers F23R 3/58) Air inlet arrangements for primary air (F23R 3/06 takes precedence) inducing a vortex |
| 3/14 | Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration (reverse-flow combustion chambers F23R 3/54; cyclone or vortex type combustion chambers F23R 3/58) Air inlet arrangements for primary air (F23R 3/06 takes precedence) inducing a vortex by using swirl vanes |
| 3/16 | Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration (reverse-flow combustion chambers F23R 3/54; cyclone or vortex type combustion chambers F23R 3/58) with devices inside the flame tube or the combustion chamber to influence the air or gas flow |
| 3/18 | Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration (reverse-flow combustion chambers F23R 3/54; cyclone or vortex type combustion chambers F23R 3/58) with devices inside the flame tube or the combustion chamber to influence the air or gas flow Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants |
| 3/20 | Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration (reverse-flow combustion chambers F23R 3/54; cyclone or vortex type combustion chambers F23R 3/58) with devices inside the flame tube or the combustion chamber to influence the air or gas flow Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means |
| 3/22 | Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration (reverse-flow combustion chambers F23R 3/54; cyclone or vortex type combustion chambers F23R 3/58) with devices inside the flame tube or the combustion chamber to influence the air or gas flow Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants movable, e.g. to an inoperative position; adjustable, e.g. self-adjusting |
| 3/24 | Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration (reverse-flow combustion chambers F23R 3/54; cyclone or vortex type combustion chambers F23R 3/58) with devices inside the flame tube or the combustion chamber to influence the air or gas flow Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants of the fluid-screen type |
| 3/26 | Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration (reverse-flow combustion chambers F23R 3/54; cyclone or vortex type combustion chambers F23R 3/58) Controlling the air flow |
| 3/28 | Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply |
| 3/30 | Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices |
| 3/32 | Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices being tubular |
| 3/34 | Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply Feeding into different combustion zones |
| 3/36 | Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply Supply of different fuels |
| 3/38 | Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising rotary fuel injection means |
| Publication # | Title | Filing Date | Pub Date | Patent Owner |
|---|---|---|---|---|
| 2024/0141,836 | GAS TURBINE ENGINE COMPONENT WITH INTEGRAL HEAT EXCHANGER | Oct 28, 22 | May 02, 24 | Not available |
| 2024/0142,104 | COMBUSTION CHAMBER WITH WALL COOLING | Oct 02, 20 | May 02, 24 | Siemens Energy Global GmbH & Co. KG |
| 2024/0133,473 | ANTI-BACK-TRANSFER INTAKE STRUCTURE FOR ROTATING DETONATION COMBUSTION CHAMBER | Dec 29, 23 | Apr 25, 24 | Not available |
| 2024/0133,553 | GAS TURBINE ENGINE COMBUSTOR WITH DILUTION PASSAGES | Oct 19, 22 | Apr 25, 24 | Not available |
| 2024/0133,555 | COWL DAMPER FOR COMBUSTOR | May 08, 23 | Apr 25, 24 | Not available |
| 2024/0133,552 | COMPONENTS FOR COMBUSTOR | May 08, 23 | Apr 25, 24 | Not available |
| 2024/0133,554 | COMBUSTOR CYLINDER, COMBUSTOR, AND GAS TURBINE | Aug 02, 23 | Apr 25, 24 | MITSUBISHI HEAVY INDUSTRIES, LTD. |
| 2024/0133,556 | COUPLING ASSEMBLY FOR A TURBINE ENGINE | May 08, 23 | Apr 25, 24 | Not available |
| 2024/0125,476 | GAS TURBINE COMBUSTOR AND GAS TURBINE | Dec 28, 21 | Apr 18, 24 | Not available |
| 2024/0125,289 | DRIVE SYSTEM FOR AN AIRCRAFT, AIRCRAFT HAVING A DRIVE SYSTEM AND METHOD FOR OPERATING AN AIRCRAFT | Oct 11, 23 | Apr 18, 24 | Not available |
| 2024/0125,238 | WALL PROVIDED WITH A COOLING HOLE HAVING A DIFFUSION PORTION WITH A TRIANGULAR SECTION | Feb 03, 22 | Apr 18, 24 | Not available |
| 2024/0117,756 | CTE MATCHING HANGER SUPPORT FOR CMC STRUCTURES | Aug 02, 23 | Apr 11, 24 | Not available |
| 2024/0117,967 | A FUEL INJECTOR | Jul 26, 23 | Apr 11, 24 | Rolls Royce plc |
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