| Patents for F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants (30,889) |
|---|
| 10/01/2009 | WO2009089921A3 Gas turbine engine with fuel booster |
| 10/01/2009 | US20090243222 Sealing arrangement for a gas turbine |
| 10/01/2009 | US20090241552 Utilizing inlet bleed heat to improve mixing and engine turndown |
| 10/01/2009 | US20090241547 Gas turbine fuel injector for lower heating capacity fuels |
| 10/01/2009 | US20090241510 Pressure control method and system to reduce gas turbine fuel supply pressure requirements |
| 10/01/2009 | US20090241509 Turbine engine inlet strut deicing |
| 10/01/2009 | US20090241508 Fuel nozzle to withstand a flameholding incident and a method of forming the same |
| 10/01/2009 | US20090241507 Ground based pulse detonation combustor for power generation |
| 10/01/2009 | US20090241505 Re-heat combustor for a gas turbine engine |
| 10/01/2009 | DE102009003647A1 Austauschbare Blende zur Abstimmung der Verbrennung und zugehöriges Verfahren Replaceable diaphragm for combustion and associated method |
| 10/01/2009 | DE102008015688A1 Turbinenrotor für eine Gasturbine Turbine rotor for a gas turbine |
| 10/01/2009 | CA2719575A1 Subsonic and stationary ramjet engines |
| 10/01/2009 | CA2719461A1 Turbine engine including a reversible electric machine |
| 09/30/2009 | EP2105598A2 A system for extending the turndown range of a turbomachine |
| 09/30/2009 | EP2105597A2 Acoustic liner panel for a turbofan engine |
| 09/30/2009 | CN101545404A A system for extending the turndown range of a turbomachine |
| 09/30/2009 | CN100545434C Injector for an aero-mechanical system for injecting mixture into a turbomachine combustion chamber |
| 09/30/2009 | CN100545433C Effervescent aerodynamic system for injecting an air/fuel mixture into a turbomachine combustion chamber |
| 09/30/2009 | CN100545037C Annular acoustic panel |
| 09/29/2009 | US7594623 Torsionally de-coupled engine mount system |
| 09/29/2009 | US7594405 Catenary mid-turbine frame design |
| 09/29/2009 | US7594404 Embedded mount for mid-turbine frame |
| 09/29/2009 | US7594402 Method for the introduction of fuel into a premixing burner |
| 09/29/2009 | US7594401 Combustor seal having multiple cooling fluid pathways |
| 09/29/2009 | US7594387 Modified fuel burning gas turbine |
| 09/24/2009 | WO2009116898A1 A gas turbine housing component |
| 09/24/2009 | WO2009116596A1 Coating structure and surface treating method |
| 09/24/2009 | WO2009116404A1 Rotary machine and additional ring |
| 09/24/2009 | WO2009115700A1 Aircraft nacelle acoustic panel |
| 09/24/2009 | WO2009115674A2 Air intake for aircraft engine nacelle, and nacelle equipped with such air intake |
| 09/24/2009 | WO2009115593A1 Contra-rotating propeller system with device for feathering propeller blades |
| 09/24/2009 | WO2009075897A3 Methods and systems for generating power from a turbine using pressurized nitrogen |
| 09/24/2009 | US20090235671 Partial oxidation gas turbine cooling |
| 09/24/2009 | US20090235668 Insulator bushing for combustion liner |
| 09/24/2009 | US20090235665 Position sensors, metering valve assemblies, and fuel delivery and control systems |
| 09/24/2009 | US20090235638 Variable area nozzle assisted gas turbine engine restarting |
| 09/24/2009 | US20090235637 System, method and apparatus for lean combustion with plasma from an electrical arc |
| 09/24/2009 | US20090235635 Igniter Assembly for a Gas Turbine |
| 09/24/2009 | US20090235634 System for extending the turndown range of a turbomachine |
| 09/24/2009 | US20090235632 Gas-turbine bearing oil system with improved oil return arrangement |
| 09/24/2009 | US20090235631 Turbomachine control system |
| 09/24/2009 | US20090235630 Non-interrupted oil supply for gas turbine engine |
| 09/24/2009 | DE102009003616A1 Isolatorbuchse für einen Brennkammereinsatz Insulator bushing for a combustor liner |
| 09/24/2009 | DE102008015207A1 Fluid-Injektor-Düse Fluid injector nozzle |
| 09/24/2009 | CA2718619A1 Contra-rotating propeller system with device for feathering propeller blades |
| 09/23/2009 | EP2103795A2 A gas turbine engine arrangement |
| 09/23/2009 | EP2103794A2 Non-interrupted oil supply for gas turbine engine |
| 09/23/2009 | EP2103780A2 Cold air buffer supply tube |
| 09/23/2009 | EP2102062A2 Aircraft leading edge |
| 09/23/2009 | EP2102060A2 Acoustic lining for an aircraft, including a frost treatment system using the joule effect |
| 09/23/2009 | CN101542092A Intake air heating control apparatus for gas turbine |
| 09/23/2009 | CN101539294A Insulator bushing for combustion liner |
| 09/23/2009 | CN101539058A Closed circuit blade-cooled turbine |
| 09/23/2009 | CN101539057A Air intake for a turboshaft engine equipped with a controlled filtering system |
| 09/23/2009 | CN101539056A Method and apparatus for operating gas turbine engine system |
| 09/23/2009 | CN100543289C Metal sheet comprising means for fixing to a support and a seal |
| 09/23/2009 | CN100543283C Gas turbine engine component having bypass circuit |
| 09/22/2009 | US7593803 Method for controlling fuel splits to gas turbine combustor |
| 09/22/2009 | US7591594 Turbomachine with a compact roller bearing |
| 09/22/2009 | CA2516437C Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture |
| 09/22/2009 | CA2445057C Self-aspirating high-area-ratio inter-turbine duct assembly for use in a gas turbine engine |
| 09/22/2009 | CA2436664C Aircraft gas turbine engine with tandem non-interdigitated counter rotating low pressure turbines |
| 09/22/2009 | CA2429413C Fan-stator interaction tone reduction |
| 09/22/2009 | CA2398515C Turbine airfoil for gas turbine engine |
| 09/17/2009 | WO2009114205A2 Adsorption-enhanced compressed air energy storage |
| 09/17/2009 | WO2009113897A1 Turbine comprising a flexible seal and corresponding flexible seal for a gas turbine engine |
| 09/17/2009 | WO2009113335A1 Tial-based alloy, process for production of the same, and rotor blade comprising the same |
| 09/17/2009 | WO2009113058A2 Method and system for enhancing start of a turbine engine, and ignition module |
| 09/17/2009 | WO2009112916A2 Direct heating organic ranking cycle |
| 09/17/2009 | WO2009112782A2 Aircraft engine assembly comprising a turbojet engine with reinforcing structures connecting the fan casing to the central casing |
| 09/17/2009 | WO2009112781A2 Aircraft engine assembly comprising an annular load-transfer structure surrounding the central casing of a turbojet engine |
| 09/17/2009 | WO2009112779A2 Heat exchanger system |
| 09/17/2009 | WO2009112777A2 Aircraft engine assembly comprising downwardly offset engine mounts on the fan casing |
| 09/17/2009 | WO2009112743A1 Device for supplying pressurised air between an aircraft engine and a de-icing compartment in a nacelle air-intake structure |
| 09/17/2009 | WO2009112697A2 Method for drilling an acoustic part of an aircraft nacelle |
| 09/17/2009 | WO2009112695A1 Air intake structure for an aircraft nacelle |
| 09/17/2009 | US20090232676 Single stage dual-entry centrifugal compressor, radial turbine gas generator |
| 09/17/2009 | US20090229468 Apparatus for filtering gas turbine inlet air |
| 09/17/2009 | US20090229273 Combustor wall apparatus with parts joined by mechanical fasteners |
| 09/17/2009 | US20090229272 Method of monitoring gas turbine engine operation |
| 09/17/2009 | US20090229270 Apparatus for controlling combustion device dynamics |
| 09/17/2009 | DE202009009206U1 Kolbenring Piston ring |
| 09/17/2009 | DE102009012914A1 Aktive Musterfaktorsteuerung/regelung für Gasturbinenmotoren Active pattern factor control / regulation for gas turbine engines |
| 09/17/2009 | CA2718367A1 Direct heating organic ranking cycle |
| 09/17/2009 | CA2716776A1 Adsorption-enhanced compressed air energy storage |
| 09/17/2009 | CA2716531A1 Heat exchanger system |
| 09/17/2009 | CA2715809A1 Aircraft engine assembly comprising a turbojet engine with reinforcing structures connecting the fan casing to the central casing |
| 09/17/2009 | CA2715738A1 Aircraft engine assembly comprising downwardly offset engine mounts on the fan casing |
| 09/17/2009 | CA2715734A1 Aircraft engine assembly comprising an annular load-transfer structure surrounding the central casing of a turbojet engine |
| 09/17/2009 | CA2713471A1 Air intake structure for an aircraft nacelle |
| 09/16/2009 | EP2101052A1 Gear wheel assembly for driving auxiliary units of a gas turbine |
| 09/16/2009 | EP2101043A1 Method for warming a steam turbine |
| 09/16/2009 | EP2101041A2 Cooling air manifold splash plate for a gas turbine engine |
| 09/16/2009 | EP2100011A2 Combined-cycle plant for generation of electrical energy |
| 09/16/2009 | EP1573239B1 Honeycomb seal |
| 09/16/2009 | CN101532434A Apparatus for filtering gas turbine inlet air |
| 09/16/2009 | CN101532433A Method for the controlled purging of the fuel feeding system in the combustor of a gas turbine engine |
| 09/16/2009 | CN101532432A Methods of injecting diluent into a gas turbine assembly |
| 09/16/2009 | CN100540866C Gas turbine power plant |
| 09/15/2009 | US7588650 Alloy containing silicon, nickel, carbon, at least a refractory metal which promotes work hardening is selected from molybdenum, niobium, tungsten, tantalum, rhenium, balance is cobalt; having good wear resistance, as well as good ductility due to content of hard particles (e.g. carbide) reduced |