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Rolls royce Deutschland Ltd & Co Kg patents


      
Recent patent applications related to Rolls royce Deutschland Ltd & Co Kg. Rolls royce Deutschland Ltd & Co Kg is listed as an Agent/Assignee. Note: Rolls royce Deutschland Ltd & Co Kg may have other listings under different names/spellings. We're not affiliated with Rolls royce Deutschland Ltd & Co Kg, we're just tracking patents.

ARCHIVE: New 2016 2015 2014 2013 2012 2011 2010 2009 | Company Directory "R" | Rolls royce Deutschland Ltd & Co Kg-related inventors




Date Rolls royce Deutschland Ltd & Co Kg patents (updated weekly) - BOOKMARK this page
06/30/16Housing device for a compressor stage of a compressor device that is embodied with multiple stages and manufacturing a housing device
06/23/16Vibration damper
06/23/16Blade arrangement of a jet engine or an aircraft propeller
06/23/16Aircraft engine having a device for separating oil
06/23/16Equipment health monitoring method and system and engine
06/23/16Compressor blade of a gas turbine
06/23/16Gas turbine combustion chamber with modified wall thickness
06/23/16Method for detecting a fuel leak in a fuel system of an aircraft having at least two engines
06/09/16Aircraft engine with an separating oil and a device for increasing pressure
06/09/16Air intake arrangement
06/09/16Device with a torque-proof first structural component and a second structural component that is connected at least in certain parts in a rotatable manner to the first structural component
06/09/16Device with a torque-proof first structural component and a second structural component that is connected at least in certain parts in a rotatable manner to the first structural component
06/02/16Turbo engine with an energy harvesting device, energy harvesting device and a energy harvesting
05/19/16Fully integrated air guide element
05/19/16Air guiding device and turbo engine with air guiding device
05/19/16Gas turbine engine
05/19/16Device for determining a fuel split, as gas turbine or an aircraft engine comprising such a device and application of the same
05/12/16Engine cowling of a gas turbine with thrust-reversing device and adjustable outlet nozzle
05/05/16Arrangement and blowing-off compressor air in a jet engine
04/28/16Aircraft gas turbine thrust-reversing device having a guide rail
04/07/16Gas turbine having at least two shafts designed as hollow shafts at least in some areas and arranged coaxially relative to one another
04/07/16Gas turbine architecture
04/07/16Gas turbine architecture
04/07/16Aircraft gas turbine engine with shock-absorbing element for fan blade loss
03/31/16Stator vane adjusting device of a gas turbine
03/31/16Aircraft engine with a compressor device
03/24/16Method and device for machining the blade tips of a compressor rotor of a gas turbine
03/17/16Tank device of an aero engine with an appliance for introducing oil
03/17/16Aero engine with a bearing chamber and an appliance for introducing oil
03/17/16Sound-damping arrangement for an engine nacelle and engine nacelle comprising such an arrangement
03/10/16Shroud device of a jet engine
03/10/16Panels of a fan of a gas turbine
03/10/16Air guiding device and aircraft engine with air guiding device
03/10/16Device for the extraction of bleed air and aircraft engine with at least one device for the extraction of bleed air
03/10/16Device for the extraction of bleed air and aircraft engine with at least one device for the extraction of bleed air
03/10/16Panels of a fan of a gas turbine
03/03/16Aircraft engine and operating an aircraft engine
02/18/16Blade
02/18/16Thrust reverser cascade element of an aircraft gas turbine
02/04/16Slide bearing device
01/28/16Thrust reverser unit
01/28/16Aircraft gas turbine with a seal for sealing an igniter plug on the combustion chamber wall of a gas turbine
01/14/16Combustion chamber of a gas turbine with bolted combustion chamber head
12/24/15Rolling tool device
12/24/15Rolling tool device
12/24/15Accessory gearbox device
12/03/15Variable stator vane arrangement
10/15/15Aircraft gas turbine having a core engine casing with cooling-air tubes
10/08/15Gas turbine inlet
10/01/15Flow guiding system, turbo engine with a flow guiding manufacturing a flow guiding system
10/01/15Measuring detecting ferromagnetic particles
09/24/15Group of blade rows
09/24/15Pressure-measuring device for measuring dynamic pressure and gas-turbine combustion chamber having pressure-measuring device
09/24/15Group of blade rows
09/24/15Group of blade rows
09/17/15Flow guiding system and rotary combustion engine
09/17/15Combustion chamber shingle of a gas turbine
09/17/15Combustion chamber of a gas turbine
09/17/15Combustion chamber of a gas turbine
09/17/15Combustion chamber of a gas turbine
09/17/15Combustion chamber of a gas turbine
09/17/15Gas turbine combustion chamber and manufacturing the same
09/17/15Structural unit for arrangement on a hydraulic fluid tank of a jet engine
09/10/15Method for producing a tandem blade wheel for a jet engine and tandem blade wheel
08/27/15Group of blade rows
08/27/15Group of blade rows
08/27/15Group of blade rows
08/27/15Group of blade rows
08/27/15Group of blade rows
08/27/15Gearing arrangement
07/30/15Method for repairing an abradable coating of a compressor of a gas turbine
06/25/15Cooled flange connection of a gas-turbine engine
06/25/15Washer of a combustion chamber tile of a gas turbine
06/25/15Jet engine device with at least one component that is arranged in a casing and that is rotatable to the casing
06/25/15Aircraft gas turbine comprising an engine cowling with a thrust-reverser device
06/25/15Aircraft gas turbine comprising a thrust-reverser device with cascade elements and an integrated rack and pinion drive
06/18/15Joint between components
06/11/15Turbine rotor blade of a gas turbine and cooling a blade tip of a turbine rotor blade of a gas turbine
05/28/15Housing arrangement for a gas turbine
05/21/15Jet engine comprising a device for spraying oil into an air-oil volume flow
05/21/15Gas turbine combustor with tile having access hole for spark plug
05/21/15Jet engine comprising a device for spraying oil
05/14/15Heat shield for a gas turbine combustion chamber
05/14/15Gas-turbine combustion chamber and its manufacture
05/07/15Inductive sensor and manufacturing an inductive sensor
04/23/15Unknown
03/26/15Assembly for a fluid flow machine
03/12/15Apparatus and shot peening of blade mounting areas on a rotor arrangement disc
03/12/15Turbine guide wheel
03/05/15Apparatus and bleeding off compressor air in a jet engine
03/05/15Sound absorber, sound absorber assembly and an engine with a sound absorber assembly
02/26/15Bleed duct assembly for a gas turbine engine
02/19/15Method for balancing and assembling a turbine rotor
01/29/15Combustion chamber tile of a gas turbine
01/29/15Laser depositioning device and producing a component by direct laser depositioning
01/15/15Turbofan jet engine
01/15/15Device and discharging sealing air in a turbofan engine
01/15/15Aircraft engine
01/08/15Jet engine with at least one oil separator, through which an air-oil-volume flow can be guided
01/08/15Gas turbine with high-pressure turbine cooling system
01/01/15Jet engine with at least one oil separator
12/25/14Accessory mounting for a gas turbine engine
12/18/14Accessory mounting for a gas turbine engine
12/11/14Assembly for a fluid flow machine
12/11/14Shroud arrangement for a fluid flow machine
12/04/14Assembly for a fluid flow machine
12/04/14Assembly for a fluid flow machine
12/04/14Method for determining a machining result during surface machining of components
10/30/14Burner seal for gas-turbine combustion chamber head and heat shield
10/30/14Removable swirler assembly for a combustion liner
10/23/14Securing segment for the vibration damping of turbine blades and rotor device
08/28/14Impingement-effusion cooled tile of a gas-turbine combustion chamber with elongated effusion holes
08/28/14Flight gas turbine with a first rotatable shaft
08/21/14Device and bleeding compressor air in a turbofan engine
08/21/14Turbomachine component with an erosion and corrosion resistant coating manufacturing such a component
06/12/14Lubricant system
06/05/14Gas turbine centripetal annular combustion chamber and flow guidance
05/29/14Gas turbine combustion chamber
05/29/14Tile fastening arrangement of a gas-turbine combustion chamber
05/22/14Aeroengine sealing arrangement
05/22/14Shaft of a gas-turbine engine, in particular a radial shaft or a shaft arranged at an angle to the machine axis
05/15/14Combustion chamber tile of a gas turbine
05/15/14Method for manufacturing a shaft of a gas-turbine engine, in particular a radial shaft or a shaft arranged at an angle to the machine axis
05/08/14Nozzle with guiding devices
05/08/14Gas-turbine engine with a telescopic air inlet in the engine lining
05/08/14Stator vane adjusting device of a gas turbine
05/08/14Nozzle with guiding devices
05/08/14Method for producing a component, component and turbomachine having a component
05/01/14Aeroengine thrust reverser arrangement
05/01/14Aeroengine thrust reverser arrangement
05/01/14Bleed flow passage
05/01/14Turbine rotor blade of a gas turbine
04/10/14Bearing chamber venting system for an aircraft engine and providing a required pressure ratio at bearing chamber seals of an air-sealed bearing chamber
03/20/14Turbine blade of a gas turbine with swirl-generating element and its manufacture
03/06/14Engine casing of an aircraft gas turbine having sound-absorbing elements in the fan inflow region
03/06/14Assembly of an axial turbomachine and manufacturing an assembly of this type
02/20/14Oil supply supplying oil for a turboprop engine
02/06/14Unknown
02/06/14Method for fuel temperature control of a gas turbine
01/30/14Oil supply system for an aircraft engine
01/30/14Assembly for a jet engine of an aircraft
01/30/14Accessory gearbox device for a jet engine
01/30/14Compressor blade of a gas turbine as well as manufacturing said blade
01/30/14Decoupled compressor blade of a gas turbine
01/30/14Low-modulus gas-turbine compressor blade
12/12/13Method for repairing compressor or turbine drums
12/05/13Aviation gas turbine thrust reversing device
11/21/13Sound absorber for a gas turbine exhaust cone, and the production thereof
11/21/13Method for the production of a sound absorber, especially for a gas turbine exhaust cone
11/21/13Method for the production of a sound absorber, especially for a gas turbine exhaust cone
11/21/13Oil supply system for a propeller turbine engine
11/14/13Cooling device for a jet engine
10/10/13Stator vane adjusting device of a gas turbine
10/03/13Method for producing engine components with a geometrically complex structure
09/05/13Aircraft gas turbine with adjustable fan
08/29/13Rolling tool device
08/22/13Method for the production of a one-piece rotor area and one-piece rotor area
08/15/13Aircraft gas turbine thrust-reversing device
08/15/13Unknown
08/15/13Measuring device having a pressure sensor
08/08/13Device and treatment of high-pressure turbine blades of a gas turbine
08/08/13Gas-turbine combustion chamber having non-symmetrical fuel nozzles
08/08/13Method for radiographically inspection a component by means of x-ray beams using a smoothing agent and smoothing agent for carrying out the method
08/01/13Annular combustion chamber of a gas turbine
08/01/13Noise-reduced turbomachine
07/25/13Unknown
07/18/13Fastening element and de-icing device of an aircraft gas-turbine engine
06/27/13Accessory mounting for a gas turbine
06/27/13Method for selecting a geometry of a blade
06/20/13Method for manufacturing a part by metal injection moulding
06/20/13Component and turbomachine having a component
06/06/13Pressure-measuring device and pressure-measuring a turbomachine
06/06/13Method and device for adjusting the bearing play in a ceramic hybrid bearing
05/23/13Bearing device and turbomachine having a bearing device
05/23/13Bearing device and turbomachine having a bearing device
05/16/13Method for determining a flow behaviour of a medium
04/25/13Accessory gearbox device for a jet engine
04/18/13Method for repairing rotor blades
04/11/13Gas turbine combustion chamber arrangement of axial type of construction
03/07/13Gas-turbine combustion chamber with a holding means of a seal for an attachment
03/07/13Generator and accessory gearbox device with a generator
02/21/13Combustion chamber head of a gas turbine with cooling and damping functions
02/21/13Method for the manufacture of a component for high thermal loads, a component producible by this method and an aircraft engine provided with the component
01/31/13Gas-turbine exhaust cone with three-dimensionally profiled partition wall and plate-type wall element
01/10/13Aircraft gas turbine with variable bypass nozzle
01/10/13Gas-turbine aircraft engine with structural surface cooler
12/27/12Apparatus and the creation of an impingement jet generating annular swirls as well as turbomachine with an apparatus of this type
12/20/12Rotor device for a jet engine with a disk wheel and several rotor blades
12/06/12Segment component in high-temperature casting material for an annular combustion chamber, annular combustion chamber for an aircraft engine, aircraft engine and the manufacture of an annular combustion chamber
11/29/12De-icing device of an aircraft gas-turbine engine
11/15/12Aircraft gas-turbine engine with oil cooler in the engine cowling
11/15/12Gas-turbine engine with bleed-air tapping device
11/08/12Gas-turbine balancing device
10/25/12Method and surface strengthening and/or smoothing of an integrally bladed rotor area of a jet engine
10/25/12Fluid-flow machine
10/04/12Device for mixing fuel and air of a jet engine
10/04/12Stator of an axial compressor stage of a turbomachine
10/04/12Rotor of an axial compressor stage of a turbomachine
09/27/12Segmented combustion chamber head
09/27/12Combustion chamber head with holding means for seals on burners in gas turbines
09/06/12Jet engine device with a bypass duct
08/16/12Centrifugal oil separator for an aircraft engine
07/12/12Gas-turbine lean combustor with fuel nozzle with controlled fuel inhomogeneity
06/14/12Fluid-flow machine - blade with hybrid profile configuration
05/24/12Repair a sandwich-like component
05/17/12Gas-turbine combustion chamber with a cooling-air supply device
04/19/12Drive shaft, in particular radial shaft for a gas-turbine engine
03/29/12Cooled turbine blades for a gas-turbine engine
03/22/12Bloom mixer for a turbofan engine
03/22/12Forging tool
02/23/12Method for filmless radiographoc inspection of components
02/09/12Method for radiographic inspection of components
02/09/12Injection moulding tool for the manufacture of a hybrid component
01/26/12Method for the manufacture of a workpiece with defined surface
01/26/12Compressor blade of a gas-turbine engine with a self-sharpening leading-edge structure
01/19/12Bleed air outlet in the bypass duct of a turbofan engine
01/19/12Fan downstream guide vanes of a turbofan engine
01/12/12Gas-turbine exhaust cone
12/22/11Method for manufacturing blisks
11/24/11Engine synchronization method
11/10/11Lean premix burner of a gas-turbine engine provided with a concentric annular central body
11/10/11Lean premix burner of a gas-turbine engine provided with a flow-guiding element
11/10/11Method and the detection of defects in the raceways of bearing shells and in the rolling elements of ceramic hybrid bearings
11/10/11Centrifugal oil separator for an aircraft engine
10/20/11Bypass duct of a turbofan engine
09/15/11Aerodynamically shaped supporting and/or fairing element in the bypass duct of a gas-turbine engine
09/08/11Aircraft engine with optimized oil heat exchanger
09/01/11Aircraft gas turbine engine
09/01/11Bypass duct of a turbo engine
07/28/11Method and surface strengthening of blisk blades
07/28/11Method for determining the surface coverage obtained by shot peening
07/21/11Intermediate casing for a gas-turbine engine
06/23/11Arrangement for the discharge of exhaust air separated from the lubricating oil de-aeration system of a gas-turbine engine
06/23/11Arrangement for the discharge of oil-venting air on a gas-turbine engine
06/16/11Arrangement for the suspension of a jet engine to a supporting structure
06/02/11Sealing rings for a labyrinth seal
05/26/11Aircraft de-icing device and engine nacelle of an aircraft gas turbine with de-icing device
05/19/11Gas turbine engine with an arrangement for measuring the shaft rotation speed
03/24/11Gas turbine with a shroud and labyrinth-type sealing arrangement
02/17/11Engine shaft of hybrid design
02/03/11Axial-flow compressor, more particularly one for an aircraft gas-turbine engine
01/27/11Cross-sectional profile for the struts or the fairing of struts and service lines of a turbofan engine
01/20/11Turbofan engine
01/20/11Gas-turbine combustion chamber with starter film for cooling the combustion chamber wall
01/20/11Axial-flow compressor with a flow pulse generator
01/20/11Fluid flow machine with blade row group
01/20/11Engine blade with excessive leading edge loading
01/20/11Propeller
01/13/11Combustion chamber head of a gas turbine



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