Patents
Patents for F02K 99 - Subject matter not provided for in other groups of this subclass (464)
03/2015
03/05/2015DE102008062088B4 Vorrichtung zur Energie-Rückgewinnung in Flugzeugtriebwerken beim Landeanflug. An energy recovery in aircraft engines during the landing approach.
03/04/2015EP2841753A1 Thermal management system for a gas turbine engine
03/03/2015US8967545 Microsatellite comprising a propulsion module and an imaging device
02/2015
02/19/2015DE10126926B4 Brennkammer mit Innenmantel aus einem keramischen Komposit-Material und Verfahren zur Herstellung Combustion chamber with inner shell made from a ceramic composite material and method for producing
02/17/2015US8955304 Gas turbine engine with modular cores and propulsion unit
02/11/2015EP2834497A1 Turbomachine thermal management
02/10/2015US8950191 System and method for gas turbine chilled water storage discharge control and/or gas turbine output control
02/04/2015EP2831403A1 Gas turbine engine fan drive gear system damper
01/2015
01/27/2015US8938944 Aircraft gas-turbine engine with oil cooler in the engine cowling
01/21/2015EP2825824A1 Fuel air premixer for gas turbine engine
01/21/2015EP2825758A1 Pump system for tms aoc reduction
01/21/2015EP2825757A1 Constant-speed pump system for engine thermal management system aoc reduction and environmental control system loss elimination
01/14/2015EP2823174A1 Erosion resistant and hydrophobic article
12/2014
12/24/2014CN104246197A 燃气涡轮发动机的风扇驱动齿轮传动系统的阻尼器 Gas turbine engine fan drive gear system damper
12/09/2014US8904753 Thermal management system for gas turbine engine
09/2014
09/09/2014US8826641 Thermal management system integrated pylon
07/2014
07/01/2014US8763404 Systems, apparatuses, and methods of harnessing thermal energy of gas turbine engines
07/01/2014US8763363 Method and system for cooling fluid in a turbine engine
06/2014
06/25/2014CN102308078B 包括推进模块和成像装置的航天器 Including spacecraft propulsion module and imaging apparatus
06/24/2014US8756910 Gas turbine engine and cooling system
06/03/2014US8739516 Turboreactor for aircraft
04/2014
04/24/2014WO2014062220A1 Structural guide vane circumferential load bearing shear pin
04/17/2014WO2014058466A1 Geared turbofan engine with optimized diffuser case flange location
04/17/2014WO2014058354A1 Method for producing reactive thrust, and reactive engine
04/15/2014CA2820943A1 Spacecraft propellant tank mount
04/10/2014WO2014055124A1 Method of defining gas turbine engine control ratings
04/10/2014WO2014055122A1 Geared turbofan high gearbox power density
04/10/2014WO2014055110A1 Static guide vane with internal hollow channels
04/10/2014US20140096510 Slotted multi-nozzle grid with integrated cooling channels
04/03/2014WO2014051700A1 Radially coacting ring seal
04/03/2014WO2014051691A1 Buffer airflow to bearing compartment
04/03/2014WO2014051688A1 Seal damper with improved retention
03/2014
03/06/2014WO2014033091A1 Electrothermal device for a propulsion system, especially for a turbojet, propulsion system comprising such an electrothermal device, and associated method
03/04/2014US8661783 Heat exchanger having swirling means
01/2014
01/09/2014WO2014007994A1 Airfoil for improved flow distribution with high radial offset
01/08/2014EP2681088A1 Air cushion transport
01/07/2014US8621867 Rotary heat engine powered by radiant energy
01/03/2014WO2014004122A1 Pre-turbine exhaust case variable area mixing plane
12/2013
12/19/2013WO2013188722A1 High durability turbine exhaust case
12/12/2013WO2013184426A1 Nacelle bifurcation for gas turbine engine
12/10/2013US8601792 Oil cooler having adjustable heat transfer effectiveness
12/10/2013US8601791 Integration of a surface heat exchanger to the wall of an aerodynamic flowpath by a structure of reinforcement rods
11/2013
11/14/2013WO2013167529A1 Energy-optimised jet propulsion method and jet engine for performing same
10/2013
10/31/2013WO2013162752A1 Thermal management system for a gas turbine engine
10/30/2013EP2655843A1 Cooled gas turbine engine member
10/22/2013US8561386 Wall cooling device
10/10/2013WO2013151842A1 Turbomachine thermal management
10/03/2013WO2013148542A1 Gas turbine engine fan drive gear system damper
10/01/2013US8544256 Gas turbine engine and integrated heat exchange system
09/2013
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
09/19/2013WO2013138104A1 Turbine engine case mount and dismount
09/19/2013WO2013138103A1 Turbine engine case mount
09/19/2013WO2013138050A1 Fuel air premixer for gas turbine engine
09/17/2013US8534044 Systems and methods for thermal management in a gas turbine powerplant
09/12/2013WO2013133997A1 Erosion resistant and hydrophobic article
09/03/2013US8522572 Adaptive power and thermal management system
09/03/2013US8522529 Propulsion unit for aircraft with heat exchanger having front inlet faces for cooling air flow and hot air flow
09/03/2013US8522525 Apparatus and method for drawing off and recirculating a cooling stream
09/03/2013US8522521 Combined air turbine starter, air-oil cooler, and fan
08/2013
08/29/2013US20130220435 Nacelle
08/27/2013US8516792 System for managing the heat fluxes of an aircraft
08/27/2013US8516791 Methods and apparatus for mixing fluid in turbine engines
08/06/2013US8499544 Turbogenerator with cooling system
07/2013
07/30/2013US8495857 Gas turbine engine thermal management system
07/02/2013US8474241 Engine with intake air temperature control system
06/2013
06/26/2013EP2605961A2 Device for sandblasting uses exhaust gas from a jet engine for blasting
05/2013
05/29/2013CN103124674A Sand blasting device using exhaust from jet engine for sand blasting
05/21/2013US8443582 Gas turbine engine with geared turbofan and oil thermal management system
05/16/2013US20130118599 Nacelle
05/14/2013US8439061 Emergency ram air inlet valve of an aircraft
05/14/2013US8438835 Methods and apparatus for mixing fluid in turbine engines
04/2013
04/09/2013US8413419 Regeneratively cooled porous media jacket
04/04/2013US20130081706 Air intake with double inlet door
03/2013
03/19/2013US8397487 Environmental control system supply precooler bypass
03/05/2013US8387362 Method and apparatus for operating gas turbine engine heat exchangers
02/2013
02/14/2013US20130037122 Pressure influencing assembly for an aircraft auxiliary system
12/2012
12/20/2012US20120317957 Aircraft powerplant
11/2012
11/27/2012US8316632 Thrust reverser configuration for a short fan duct
11/20/2012US8313056 Engine heat exchanger with thermoelectric generation
11/07/2012CN101427018B Propulsion device with enclosed plenum
10/2012
10/16/2012USRE43731 Integrated air inlet system for multi-propulsion aircraft engines
09/2012
09/27/2012US20120240551 Heat engine
09/18/2012US8266889 Gas turbine engine fan bleed heat exchanger system
09/18/2012US8266888 Cooler in nacelle with radial coolant
09/07/2012WO2012119044A1 Replaceable thrust generating structures attached to an air vehicle
09/07/2012WO2012118987A1 Air cushion transport
08/2012
08/08/2012EP1718857B1 Integrated air inlet system for multi-propulsion aircraft engines
07/2012
07/03/2012US8210498 Gate valve for a system for circulating cooling air through a turbomachine
06/2012
06/28/2012WO2012088493A1 Cooled gas turbine engine member
06/21/2012WO2011144210A9 Device for sandblasting uses exhaust gas from a jet engine for blasting
05/2012
05/17/2012US20120118400 Leading edge structure, in particular for the air intake of the nacelle of an aircraft engine
05/17/2012US20120118398 Turbomachine nozzle cowl having patterns with lateral fins for reducing jet noise
05/03/2012WO2011144210A3 Device for sandblasting uses exhaust gas from a jet engine for blasting
04/2012
04/26/2012US20120097260 Aircraft cover including means for limiting the scoop phenomena of electromagnetic type
04/24/2012CA2444984C Reading device for identification connectors
04/19/2012US20120090694 Aircraft nacelle including a rear frame inclined to the rear
04/19/2012US20120090693 Acoustic processing panel, more particularly adapted for an air intake in an aircraft nacelle
03/2012
03/20/2012US8138753 Measuring arrangement for detecting a 1/rotary momentum of an engine rotor, and associated method
03/15/2012US20120060938 Aircraft nacelle comprising a reinforced outer wall
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