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Rolls royce Deutschland Ltd x26 Co Kg
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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 2015 2014 2013 2012 2011 2010 2009 | Company Directory "R" | Rolls royce Deutschland Ltd & Co Kg-related inventors



Laser depositioning device and  producing a component by direct laser depositioning

Rolls-royce Deutschland Ltd & Co Kg

Laser depositioning device and producing a component by direct laser depositioning

Search recent Press Releases: Rolls royce Deutschland Ltd & Co Kg-related press releases
Count Application # Date Rolls royce Deutschland Ltd & Co Kg patents (updated weekly) - BOOKMARK this page
12015002712701/29/15 new patent  Combustion chamber tile of a gas turbine
22015003078701/29/15 new patent  Laser depositioning device and producing a component by direct laser depositioning
32015001330701/15/15Turbofan jet engine
42015001695001/15/15Device and discharging sealing air in a turbofan engine
52015001699401/15/15Aircraft engine
62015000753101/08/15Jet engine with at least one oil separator, through which an air-oil-volume flow can be guided
72015001038501/08/15Gas turbine with high-pressure turbine cooling system
82015000024601/01/15Jet engine with at least one oil separator
92014037355512/25/14Accessory mounting for a gas turbine engine
102014036655512/18/14Accessory mounting for a gas turbine engine
112014036327712/11/14Assembly for a fluid flow machine
122014036328312/11/14Shroud arrangement for a fluid flow machine
132014035614312/04/14Assembly for a fluid flow machine
142014035614412/04/14Assembly for a fluid flow machine
152014035245012/04/14Method for determining a machining result during surface machining of components
162014031814810/30/14Burner seal for gas-turbine combustion chamber head and heat shield
172014031815010/30/14Removable swirler assembly for a combustion liner
182014031457810/23/14Securing segment for the vibration damping of turbine blades and rotor device
192014023803008/28/14Impingement-effusion cooled tile of a gas-turbine combustion chamber with elongated effusion holes
202014024186008/28/14Flight gas turbine with a first rotatable shaft
212014023408008/21/14Device and bleeding compressor air in a turbofan engine
222014023409608/21/14Turbomachine component with an erosion and corrosion resistant coating manufacturing such a component
232014016159106/12/14Lubricant system
242014015044206/05/14Gas turbine centripetal annular combustion chamber and flow guidance
252014014414505/29/14Gas turbine combustion chamber
262014014414605/29/14Tile fastening arrangement of a gas-turbine combustion chamber
272014014082005/22/14Aeroengine sealing arrangement
282014014189405/22/14Shaft of a gas-turbine engine, in particular a radial shaft or a shaft arranged at an angle to the machine axis
292014013050105/15/14Combustion chamber tile of a gas turbine
302014013096405/15/14Method 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
312014012428905/08/14Nozzle with guiding devices
322014012700105/08/14Gas-turbine engine with a telescopic air inlet in the engine lining
332014012700305/08/14Stator vane adjusting device of a gas turbine
342014012701005/08/14Nozzle with guiding devices
352014012700505/08/14Method for producing a component, component and turbomachine having a component
362014011602505/01/14Aeroengine thrust reverser arrangement
372014011602605/01/14Aeroengine thrust reverser arrangement
382014011988305/01/14Bleed flow passage
392014011994205/01/14Turbine rotor blade of a gas turbine
402014009653304/10/14Bearing chamber venting system for an aircraft engine and providing a required pressure ratio at bearing chamber seals of an air-sealed bearing chamber
412014007953903/20/14Turbine blade of a gas turbine with swirl-generating element and its manufacture
422014006492803/06/14Engine casing of an aircraft gas turbine having sound-absorbing elements in the fan inflow region
432014006495203/06/14Assembly of an axial turbomachine and manufacturing an assembly of this type
442014005056102/20/14Oil supply supplying oil for a turboprop engine
452014003372302/06/14Unknown
462014003373102/06/14Method for fuel temperature control of a gas turbine
472014002653401/30/14Oil supply system for an aircraft engine
482014002659201/30/14Assembly for a jet engine of an aircraft
492014002670001/30/14Accessory gearbox device for a jet engine
502014003010601/30/14Compressor blade of a gas turbine as well as manufacturing said blade
512014003010701/30/14Decoupled compressor blade of a gas turbine
522014003010901/30/14Low-modulus gas-turbine compressor blade
532013032687612/12/13Method for repairing compressor or turbine drums
542013031894512/05/13Aviation gas turbine thrust reversing device
552013030640111/21/13Sound absorber for a gas turbine exhaust cone, and the production thereof
562013030640211/21/13Method for the production of a sound absorber, especially for a gas turbine exhaust cone
572013030640311/21/13Method for the production of a sound absorber, especially for a gas turbine exhaust cone
582013030909111/21/13Oil supply system for a propeller turbine engine
592013030214311/14/13Cooling device for a jet engine
602013026642410/10/13Stator vane adjusting device of a gas turbine
612013025973210/03/13Method for producing engine components with a geometrically complex structure
622013023038309/05/13Aircraft gas turbine with adjustable fan
632013021998208/29/13Rolling tool device
642013021639108/22/13Method for the production of a one-piece rotor area and one-piece rotor area
652013020575308/15/13Aircraft gas turbine thrust-reversing device
662013020578808/15/13Unknown
672013020667608/15/13Measuring device having a pressure sensor
682013019904008/08/13Device and treatment of high-pressure turbine blades of a gas turbine
692013019918708/08/13Gas-turbine combustion chamber having non-symmetrical fuel nozzles
702013020208808/08/13Method for radiographically inspection a component by means of x-ray beams using a smoothing agent and smoothing agent for carrying out the method
712013019223208/01/13Annular combustion chamber of a gas turbine
722013019561008/01/13Noise-reduced turbomachine
732013018670707/25/13Unknown
742013018022707/18/13Fastening element and de-icing device of an aircraft gas-turbine engine
752013016045906/27/13Accessory mounting for a gas turbine
762013016605606/27/13Method for selecting a geometry of a blade
772013015662606/20/13Method for manufacturing a part by metal injection moulding
782013015700006/20/13Component and turbomachine having a component
792013013957806/06/13Pressure-measuring device and pressure-measuring a turbomachine
802013014246706/06/13Method and device for adjusting the bearing play in a ceramic hybrid bearing
812013012950405/23/13Bearing device and turbomachine having a bearing device
822013012950505/23/13Bearing device and turbomachine having a bearing device
832013012411405/16/13Method for determining a flow behaviour of a medium
842013009817904/25/13Accessory gearbox device for a jet engine
852013009170404/18/13Method for repairing rotor blades
862013008690804/11/13Gas turbine combustion chamber arrangement of axial type of construction
872013005571603/07/13Gas-turbine combustion chamber with a holding means of a seal for an attachment
882013005709303/07/13Generator and accessory gearbox device with a generator
892013004262702/21/13Combustion chamber head of a gas turbine with cooling and damping functions
902013004509302/21/13Method for the manufacture of a component for high thermal loads, a component producible by this method and an aircraft engine provided with the component
912013002596201/31/13Gas-turbine exhaust cone with three-dimensionally profiled partition wall and plate-type wall element
922013000814701/10/13Aircraft gas turbine with variable bypass nozzle
932013001124601/10/13Gas-turbine aircraft engine with structural surface cooler
942012032535412/27/12Apparatus and the creation of an impingement jet generating annular swirls as well as turbomachine with an apparatus of this type
952012032147712/20/12Rotor device for a jet engine with a disk wheel and several rotor blades
962012030465812/06/12Segment 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
972012029880211/29/12De-icing device of an aircraft gas-turbine engine
982012028513811/15/12Aircraft gas-turbine engine with oil cooler in the engine cowling
992012028835911/15/12Gas-turbine engine with bleed-air tapping device
1002012028208211/08/12Gas-turbine balancing device
1012012026642610/25/12Method and surface strengthening and/or smoothing of an integrally bladed rotor area of a jet engine
1022012026961910/25/12Fluid-flow machine
1032012024711010/04/12Device for mixing fuel and air of a jet engine
1042012025131210/04/12Stator of an axial compressor stage of a turbomachine
1052012025132410/04/12Rotor of an axial compressor stage of a turbomachine
1062012024058309/27/12Segmented combustion chamber head
1072012024059509/27/12Combustion chamber head with holding means for seals on burners in gas turbines
1082012022239609/06/12Jet engine device with a bypass duct
1092012020472308/16/12Centrifugal oil separator for an aircraft engine
1102012017458807/12/12Gas-turbine lean combustor with fuel nozzle with controlled fuel inhomogeneity
1112012014839606/14/12Fluid-flow machine - blade with hybrid profile configuration
1122012012552305/24/12Repair a sandwich-like component
1132012011797305/17/12Gas-turbine combustion chamber with a cooling-air supply device
1142012009477704/19/12Drive shaft, in particular radial shaft for a gas-turbine engine
1152012007666503/29/12Cooled turbine blades for a gas-turbine engine
1162012006702503/22/12Bloom mixer for a turbofan engine
1172012006710103/22/12Forging tool
1182012004503202/23/12Method for filmless radiographoc inspection of components
1192012003378702/09/12Method for radiographic inspection of components
1202012003433302/09/12Injection moulding tool for the manufacture of a hybrid component
1212012001766301/26/12Method for the manufacture of a workpiece with defined surface
1222012002080201/26/12Compressor blade of a gas-turbine engine with a self-sharpening leading-edge structure
1232012001182701/19/12Bleed air outlet in the bypass duct of a turbofan engine
1242012001478001/19/12Fan downstream guide vanes of a turbofan engine
1252012000661401/12/12Gas-turbine exhaust cone
1262011030896612/22/11Method for manufacturing blisks
1272011028874011/24/11Engine synchronization method
1282011027168011/10/11Lean premix burner of a gas-turbine engine provided with a concentric annular central body
1292011027168111/10/11Lean premix burner of a gas-turbine engine provided with a flow-guiding element
1302011027176511/10/11Method and the detection of defects in the raceways of bearing shells and in the rolling elements of ceramic hybrid bearings
1312011027183711/10/11Centrifugal oil separator for an aircraft engine
1322011025596410/20/11Bypass duct of a turbofan engine
1332011021978209/15/11Aerodynamically shaped supporting and/or fairing element in the bypass duct of a gas-turbine engine
1342011021517209/08/11Aircraft engine with optimized oil heat exchanger
1352011020945809/01/11Aircraft gas turbine engine
1362011021194709/01/11Bypass duct of a turbo engine
1372011017984407/28/11Method and surface strengthening of blisk blades
1382011018249907/28/11Method for determining the surface coverage obtained by shot peening
1392011017399007/21/11Intermediate casing for a gas-turbine engine
1402011014622306/23/11Arrangement for the discharge of exhaust air separated from the lubricating oil de-aeration system of a gas-turbine engine
1412011014622406/23/11Arrangement for the discharge of oil-venting air on a gas-turbine engine
1422011013992506/16/11Arrangement for the suspension of a jet engine to a supporting structure
1432011012772806/02/11Sealing rings for a labyrinth seal
1442011012113605/26/11Aircraft de-icing device and engine nacelle of an aircraft gas turbine with de-icing device
1452011011690805/19/11Gas turbine engine with an arrangement for measuring the shaft rotation speed
1462011007007403/24/11Gas turbine with a shroud and labyrinth-type sealing arrangement
1472011003866602/17/11Engine shaft of hybrid design
1482011002709102/03/11Axial-flow compressor, more particularly one for an aircraft gas-turbine engine
1492011001688301/27/11Cross-sectional profile for the struts or the fairing of struts and service lines of a turbofan engine
1502011001105801/20/11Turbofan engine
1512011001109301/20/11Gas-turbine combustion chamber with starter film for cooling the combustion chamber wall
1522011001403701/20/11Axial-flow compressor with a flow pulse generator
1532011001404001/20/11Fluid flow machine with blade row group
1542011001405701/20/11Engine blade with excessive leading edge loading
1552011001405801/20/11Propeller
1562011000523301/13/11Combustion chamber head of a gas turbine
1572011000585801/13/11Noise-reduced aircraft engine and reducing noise emissions of an aircraft engine
1582010030362912/02/10Fluid flow machine with a blade row group featuring a meridional edge distance
1592010028777211/18/10Method for surface strengthening and smoothening of metallic components
1602010028864811/18/10Method and etching the surfaces of integrally bladed rotors
1612010025819910/14/10Intake cone in a fiber compound material for a gas-turbine engine
1622010025901310/14/10Abradable labyrinth seal for a fluid-flow machine
1632010023295409/16/10Bypass duct of a turbofan engine
1642010022390509/09/10Scoop of a running-gap control system of an aircraft gas turbine
1652010022434809/09/10Method for the manufacture of an ejector nozzle tube
1662010021228508/26/10Turboprop propulsion unit with pusher propeller
1672010021548108/26/10Running-gap control system of an aircraft gas turbine
1682010019258808/05/10Method for the provision of a cooling-air opening in a wall of a gas-turbine combustion chamber as well as a combustion-chamber wall produced in accordance with this method
1692010017525607/15/10Method for the manufacture of the blade tips of rotor wheels made in blisk design
1702010017609707/15/10Arrangement for the repair of the blades of blisk drums by means of laser deposition welding
1712010015552606/24/10Aircraft with tail propeller-engine layout
1722010016110706/24/10Machine control for a numerically controlled machine tool
1732010014802706/17/10Sensor bracket for at least one sensor on a gas turbine
1742010014844906/17/10Segmented sealing lips for labyrinth sealing rings
1752010015069606/17/10Fan casing for a jet engine
1762010013924106/10/10Flow divider for a fan engine
1772010013927806/10/10Method and the operation of a turboprop aircraft engine provided with pusher propellers
1782010014023006/10/10Method for the manufacture of a welded rotor for a gas-turbine engine
1792010014314006/10/10Fluid flow machine with sidewall boundary layer barrier
1802010012658905/27/10Device for the prevention of high oil tank pressures under negative g conditions
1812010012666205/27/10Method for the manufacture of hybrid components for aircraft gas turbines
1822010012965105/27/10Hybrid component for a gas-turbine engine
1832010012251805/20/10Oil system heating for aircraft gas turbines
1842010012448705/20/10Multi-vane variable stator unit of a fluid flow machine
1852010010918405/06/10Method for the manufacture of an engine shaft
1862010011170205/06/10Hub cone for an aircraft engine
1872010011317005/06/10Engine shaft for a gas-turbine engine
1882010011317105/06/10Engine shaft in the form of a fiber-composite plastic tube with metallic driving and driven protrusions
1892010009852704/22/10Fluid flow machine with peripheral energization near the suction side
1902010009853004/22/10Compressor for a gas turbine
1912010009853604/22/10Fluid flow machine with running gap retraction
1922010005111203/04/10Intake cone for a gas-turbine engine
1932010003463702/11/10Fluid flow machine
1942010002421402/04/10Method for the manufacture of metallic components
1952010002131001/28/10Method for improving the flow conditions on the propeller or fan of an aircraft engine and accordingly designed hub cone
1962010001495601/21/10Fluid flow machine featuring a groove on a running gap of a blade end
1972010001496001/21/10Gas-turbine engine with variable stator vanes
1982010000577601/14/10Fuel supply system for a gas-turbine engine
1992010000019801/07/10Gas turbine with at least one multi-stage compressor unit including several compressor modules
2002010000022601/07/10Turbofan engine with at least one driving at least one generator
2012009031400412/24/09Turboprop engine with an the generation of a cooling airflow
2022009031723212/24/09Blade shroud with aperture
2032013032687612/12/13Method for repairing compressor or turbine drums
2042010002131001/28/10Method for improving the flow conditions on the propeller or fan of an aircraft engine and accordingly designed hub cone
2052010001496001/21/10Gas-turbine engine with variable stator vanes
2062010000577601/14/10Fuel supply system for a gas-turbine engine
2072010000022601/07/10Turbofan engine with at least one driving at least one generator


ARCHIVE: New 2015 2014 2013 2012 2011 2010 2009



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