Patents
Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580)
10/2013
10/22/2013CA2499675C Methods and apparatus for operating gas turbine engines
10/17/2013WO2013154649A2 Gas turbine engine with high speed low pressure turbine section
10/17/2013WO2013154648A1 Gas turbine engine with high speed low pressure turbine section
10/17/2013WO2013154646A1 Compressor flowpath
10/17/2013WO2013154639A2 Gas turbine engine with improved fuel efficiency
10/17/2013US20130269312 Device for controlling a variable section nozzle of an aircraft
10/17/2013CA2856723A1 Gas turbine engine with high speed low pressure turbine section
10/17/2013CA2856561A1 Gas turbine engine with high speed low pressure turbine section
10/17/2013CA2811821A1 Modular louver system
10/16/2013EP2650520A2 Aircraft gas turbine engine having a relief channel in a guide blade base element of a bypass channel
10/15/2013CA2631849C Dual flow turbine engine equipped with a precooler
10/15/2013CA2545761C Methods and apparatus for assembling gas turbine engines
10/10/2013WO2013151875A1 Combustor having a beveled grommet
10/10/2013WO2013151842A1 Turbomachine thermal management
10/10/2013WO2013151841A1 Differential geared architecture for gas turbine engine
10/10/2013WO2013151304A1 Power transmission apparatus for jet engine
10/10/2013WO2013150248A1 Exit guide vanes
10/10/2013WO2013106119A3 Mounting apparatus for a trailing edge box of a gas turbine augmentor
10/10/2013US20130266423 Self-mounted cascade for a thrust reverser
10/10/2013DE102012007130A1 Fluggasturbine mit einem Entlastungskanal in einem Leitschaufelfußelement eines Nebenstromkanals Aircraft gas turbine with a discharge channel in a Leitschaufelfußelement a bypass duct
10/09/2013EP2647847A1 Guide vane attachment structure and fan
10/08/2013US8549834 Gas turbine engine with variable area fan nozzle
10/03/2013WO2013149249A1 Air blocker ring assembly with radial retention
10/03/2013WO2013148542A1 Gas turbine engine fan drive gear system damper
10/03/2013WO2013148445A1 Blade wedge attachment
10/03/2013WO2013148419A1 Torque frame bushing arrangement for gas turbine engine fan drive gear system
10/03/2013WO2013147969A2 Mid-turbine frame buffer system
10/03/2013WO2013147968A1 Gas turbine engine shaft bearing configuration
10/03/2013WO2013147967A2 Variable area fan nozzle with wall thickness distribution
10/03/2013WO2013147951A1 Gas turbine engine with fan variable area nozzle for low fan pressure ratio
10/03/2013US20130255225 Gas turbine engine thrust reverser system
10/03/2013US20130255224 Reverse core gear turbofan
10/02/2013EP2435303B1 Actuator arrangement for pitch adjustment of a turbofan engine, the actuator rotating together with the turbofan blades
09/2013
09/30/2013CA2810523A1 Gas turbine engine nose cone
09/26/2013WO2013142460A1 Trailing edge cooling
09/26/2013WO2013141933A1 Gas turbine engine with fan variable area nozzle to reduce fan instability
09/26/2013WO2013139974A1 Ignition unit for turbojet engine
09/25/2013CN203214192U Multi-functional turbofan engine
09/19/2013WO2013138808A1 Gas turbine engine control system with gas monitor
09/19/2013WO2013138217A1 Constant-speed pump system for engine thermal management system aoc reduction and environmental control system loss elimination
09/19/2013WO2013138215A1 Pump system for tms aoc reduction
09/19/2013WO2013138212A1 Gas turbine engine variable stator vane assembly
09/19/2013WO2013138104A1 Turbine engine case mount and dismount
09/19/2013WO2013138103A1 Turbine engine case mount
09/19/2013WO2013138050A1 Fuel air premixer for gas turbine engine
09/19/2013WO2013137980A1 Aerospace engine with augmenting turbojet
09/18/2013CN103314206A Nacelle for an aircraft bypass turbojet engine
09/17/2013US8534077 Turbine engine with a power turbine equipped with an electric power generator
09/17/2013US8534071 Engine hot section vane with tapered flame holder surface
09/17/2013US8534043 Air-oil heat exchanger
09/12/2013WO2013133997A1 Erosion resistant and hydrophobic article
09/12/2013WO2013133935A1 Gas turbine engine fuel heating system
09/11/2013CN103299084A Turbofan engine
09/11/2013CN103291453A Counter-rotating low pressure turbine with splitter gear system
09/11/2013CN101560890B Intermediate casing of turbojet
09/10/2013US8529189 Linear quadratic regulator control for bleed air system fan air valve
09/10/2013US8528318 Cambered aero-engine inlet
09/06/2013WO2013130296A1 Gas turbine engine driving multiple fans
09/06/2013WO2013130295A1 Geared gas turbine engine with reduced fan noise
09/06/2013WO2013130172A1 Hybrid turbofan engine
09/05/2013US20130227930 Gas turbine frame stiffening rails
09/04/2013CN101922379B Translating variable area fan nozzle providing an upstream bypass flow exit
09/03/2013US8522572 Adaptive power and thermal management system
09/03/2013US8522528 System for diffusing bleed air flow
09/03/2013US8522527 Burner for a gas turbine and method for feeding a gaseous fuel in a burner
09/03/2013US8522526 Two-shaft engine for aircraft with high electric power demand
08/2013
08/29/2013WO2013126728A1 Turbine engine with thrust vectoring exhaust nozzle
08/29/2013WO2013126123A1 Gas turbine engine with axial movable fan variable area nozzle
08/29/2013US20130223983 Counter rotating low pressure turbine with splitter gear system
08/29/2013US20130219860 Counter-rotating low pressure turbine without turbine exhaust case
08/29/2013US20130219859 Counter rotating low pressure compressor and turbine each having a gear system
08/29/2013US20130219857 Bypass duct with angled drag links
08/29/2013US20130219856 Counter-rotating low pressure turbine with gear system mounted to mid turbine frame
08/29/2013US20130219855 Method of Using an Afterburner to Reduce High Velocity Jet Engine Noise
08/29/2013US20130219854 Air-cooled oil cooler for turbofan engine
08/29/2013CA2807200A1 Airfoils for use in rotary machines
08/29/2013CA2805282A1 Counter rotating low pressure turbine with splitter gear system
08/29/2013CA2805279A1 Counter-rotating low pressure turbine with gear system mounted to mid turbine frame
08/29/2013CA2805186A1 Counter rotating low pressure compressor and turbine each having a gear system
08/27/2013US8517672 Epicyclic gearbox
08/27/2013US8516790 Spring for a cascade-type thrust reverser shutter for an aircraft jet engine
08/27/2013US8516789 Gas turbine engine with aft core driven fan section
08/22/2013WO2013122713A2 Low noise compressor rotor for geared turbofan engine
08/22/2013WO2013122687A2 Gas turbine engine bifurcation located fan variable area nozzle
08/21/2013EP2628934A2 Thermoelectric generator in turbine engine nozzles
08/21/2013CN103256122A Seal for a variable area fan nozzle
08/21/2013CN102046983B Air collector in a turbomachine
08/20/2013US8511061 Gas turbine engine shaft bearing configuration
08/15/2013WO2013119535A1 Gas turbine engine with modular cores and propulsion unit
08/15/2013WO2013119527A1 Gas turbine engine with separate core and propulsion unit
08/15/2013WO2013119520A1 Customer bleed air pressure loss reduction
08/15/2013WO2013081714A3 Guide vane assembly for a gas turbine engine
08/15/2013US20130205753 Aircraft gas turbine thrust-reversing device
08/15/2013US20130205752 Gas turbine engine with separate core and propulsion unit
08/13/2013CA2520471C Methods and apparatus for assembling a gas turbine engine
08/13/2013CA2519823C Methods and apparatus for assembling a gas turbine engine
08/08/2013WO2013116262A1 Geared turbofan gas turbine engine architecture
08/08/2013WO2013116259A1 Geared turbofan gas turbine engine architecture
08/08/2013WO2013116257A1 Geared turbofan gas turbine engine architecture
08/08/2013WO2013115921A1 Speed sensor probe location in gas turbine engine
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