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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


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
12015008634403/26/15Assembly for a fluid flow machine
22015006826203/12/15Apparatus and shot peening of blade mounting areas on a rotor arrangement disc
32015007177703/12/15Turbine guide wheel
42015005931503/05/15Apparatus and bleeding off compressor air in a jet engine
52015006019403/05/15Sound absorber, sound absorber assembly and an engine with a sound absorber assembly
62015005290802/26/15Bleed duct assembly for a gas turbine engine
72015004719102/19/15Method for balancing and assembling a turbine rotor
82015002712701/29/15Combustion chamber tile of a gas turbine
92015003078701/29/15Laser depositioning device and producing a component by direct laser depositioning
102015001330701/15/15Turbofan jet engine
112015001695001/15/15Device and discharging sealing air in a turbofan engine
122015001699401/15/15Aircraft engine
132015000753101/08/15Jet engine with at least one oil separator, through which an air-oil-volume flow can be guided
142015001038501/08/15Gas turbine with high-pressure turbine cooling system
152015000024601/01/15Jet engine with at least one oil separator
162014037355512/25/14Accessory mounting for a gas turbine engine
172014036655512/18/14Accessory mounting for a gas turbine engine
182014036327712/11/14Assembly for a fluid flow machine
192014036328312/11/14Shroud arrangement for a fluid flow machine
202014035614312/04/14Assembly for a fluid flow machine
212014035614412/04/14Assembly for a fluid flow machine
222014035245012/04/14Method for determining a machining result during surface machining of components
232014031814810/30/14Burner seal for gas-turbine combustion chamber head and heat shield
242014031815010/30/14Removable swirler assembly for a combustion liner
252014031457810/23/14Securing segment for the vibration damping of turbine blades and rotor device
262014023803008/28/14Impingement-effusion cooled tile of a gas-turbine combustion chamber with elongated effusion holes
272014024186008/28/14Flight gas turbine with a first rotatable shaft
282014023408008/21/14Device and bleeding compressor air in a turbofan engine
292014023409608/21/14Turbomachine component with an erosion and corrosion resistant coating manufacturing such a component
302014016159106/12/14Lubricant system
312014015044206/05/14Gas turbine centripetal annular combustion chamber and flow guidance
322014014414505/29/14Gas turbine combustion chamber
332014014414605/29/14Tile fastening arrangement of a gas-turbine combustion chamber
342014014082005/22/14Aeroengine sealing arrangement
352014014189405/22/14Shaft of a gas-turbine engine, in particular a radial shaft or a shaft arranged at an angle to the machine axis
362014013050105/15/14Combustion chamber tile of a gas turbine
372014013096405/15/14Method 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
382014012428905/08/14Nozzle with guiding devices
392014012700105/08/14Gas-turbine engine with a telescopic air inlet in the engine lining
402014012700305/08/14Stator vane adjusting device of a gas turbine
412014012701005/08/14Nozzle with guiding devices
422014012700505/08/14Method for producing a component, component and turbomachine having a component
432014011602505/01/14Aeroengine thrust reverser arrangement
442014011602605/01/14Aeroengine thrust reverser arrangement
452014011988305/01/14Bleed flow passage
462014011994205/01/14Turbine rotor blade of a gas turbine
472014009653304/10/14Bearing chamber venting system for an aircraft engine and providing a required pressure ratio at bearing chamber seals of an air-sealed bearing chamber
482014007953903/20/14Turbine blade of a gas turbine with swirl-generating element and its manufacture
492014006492803/06/14Engine casing of an aircraft gas turbine having sound-absorbing elements in the fan inflow region
502014006495203/06/14Assembly of an axial turbomachine and manufacturing an assembly of this type
512014005056102/20/14Oil supply supplying oil for a turboprop engine
522014003372302/06/14Unknown
532014003373102/06/14Method for fuel temperature control of a gas turbine
542014002653401/30/14Oil supply system for an aircraft engine
552014002659201/30/14Assembly for a jet engine of an aircraft
562014002670001/30/14Accessory gearbox device for a jet engine
572014003010601/30/14Compressor blade of a gas turbine as well as manufacturing said blade
582014003010701/30/14Decoupled compressor blade of a gas turbine
592014003010901/30/14Low-modulus gas-turbine compressor blade
602013032687612/12/13Method for repairing compressor or turbine drums
612013031894512/05/13Aviation gas turbine thrust reversing device
622013030640111/21/13Sound absorber for a gas turbine exhaust cone, and the production thereof
632013030640211/21/13Method for the production of a sound absorber, especially for a gas turbine exhaust cone
642013030640311/21/13Method for the production of a sound absorber, especially for a gas turbine exhaust cone
652013030909111/21/13Oil supply system for a propeller turbine engine
662013030214311/14/13Cooling device for a jet engine
672013026642410/10/13Stator vane adjusting device of a gas turbine
682013025973210/03/13Method for producing engine components with a geometrically complex structure
692013023038309/05/13Aircraft gas turbine with adjustable fan
702013021998208/29/13Rolling tool device
712013021639108/22/13Method for the production of a one-piece rotor area and one-piece rotor area
722013020575308/15/13Aircraft gas turbine thrust-reversing device
732013020578808/15/13Unknown
742013020667608/15/13Measuring device having a pressure sensor
752013019904008/08/13Device and treatment of high-pressure turbine blades of a gas turbine
762013019918708/08/13Gas-turbine combustion chamber having non-symmetrical fuel nozzles
772013020208808/08/13Method for radiographically inspection a component by means of x-ray beams using a smoothing agent and smoothing agent for carrying out the method
782013019223208/01/13Annular combustion chamber of a gas turbine
792013019561008/01/13Noise-reduced turbomachine
802013018670707/25/13Unknown
812013018022707/18/13Fastening element and de-icing device of an aircraft gas-turbine engine
822013016045906/27/13Accessory mounting for a gas turbine
832013016605606/27/13Method for selecting a geometry of a blade
842013015662606/20/13Method for manufacturing a part by metal injection moulding
852013015700006/20/13Component and turbomachine having a component
862013013957806/06/13Pressure-measuring device and pressure-measuring a turbomachine
872013014246706/06/13Method and device for adjusting the bearing play in a ceramic hybrid bearing
882013012950405/23/13Bearing device and turbomachine having a bearing device
892013012950505/23/13Bearing device and turbomachine having a bearing device
902013012411405/16/13Method for determining a flow behaviour of a medium
912013009817904/25/13Accessory gearbox device for a jet engine
922013009170404/18/13Method for repairing rotor blades
932013008690804/11/13Gas turbine combustion chamber arrangement of axial type of construction
942013005571603/07/13Gas-turbine combustion chamber with a holding means of a seal for an attachment
952013005709303/07/13Generator and accessory gearbox device with a generator
962013004262702/21/13Combustion chamber head of a gas turbine with cooling and damping functions
972013004509302/21/13Method for the manufacture of a component for high thermal loads, a component producible by this method and an aircraft engine provided with the component
982013002596201/31/13Gas-turbine exhaust cone with three-dimensionally profiled partition wall and plate-type wall element
992013000814701/10/13Aircraft gas turbine with variable bypass nozzle
1002013001124601/10/13Gas-turbine aircraft engine with structural surface cooler
1012012032535412/27/12Apparatus and the creation of an impingement jet generating annular swirls as well as turbomachine with an apparatus of this type
1022012032147712/20/12Rotor device for a jet engine with a disk wheel and several rotor blades
1032012030465812/06/12Segment 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
1042012029880211/29/12De-icing device of an aircraft gas-turbine engine
1052012028513811/15/12Aircraft gas-turbine engine with oil cooler in the engine cowling
1062012028835911/15/12Gas-turbine engine with bleed-air tapping device
1072012028208211/08/12Gas-turbine balancing device
1082012026642610/25/12Method and surface strengthening and/or smoothing of an integrally bladed rotor area of a jet engine
1092012026961910/25/12Fluid-flow machine
1102012024711010/04/12Device for mixing fuel and air of a jet engine
1112012025131210/04/12Stator of an axial compressor stage of a turbomachine
1122012025132410/04/12Rotor of an axial compressor stage of a turbomachine
1132012024058309/27/12Segmented combustion chamber head
1142012024059509/27/12Combustion chamber head with holding means for seals on burners in gas turbines
1152012022239609/06/12Jet engine device with a bypass duct
1162012020472308/16/12Centrifugal oil separator for an aircraft engine
1172012017458807/12/12Gas-turbine lean combustor with fuel nozzle with controlled fuel inhomogeneity
1182012014839606/14/12Fluid-flow machine - blade with hybrid profile configuration
1192012012552305/24/12Repair a sandwich-like component
1202012011797305/17/12Gas-turbine combustion chamber with a cooling-air supply device
1212012009477704/19/12Drive shaft, in particular radial shaft for a gas-turbine engine
1222012007666503/29/12Cooled turbine blades for a gas-turbine engine
1232012006702503/22/12Bloom mixer for a turbofan engine
1242012006710103/22/12Forging tool
1252012004503202/23/12Method for filmless radiographoc inspection of components
1262012003378702/09/12Method for radiographic inspection of components
1272012003433302/09/12Injection moulding tool for the manufacture of a hybrid component
1282012001766301/26/12Method for the manufacture of a workpiece with defined surface
1292012002080201/26/12Compressor blade of a gas-turbine engine with a self-sharpening leading-edge structure
1302012001182701/19/12Bleed air outlet in the bypass duct of a turbofan engine
1312012001478001/19/12Fan downstream guide vanes of a turbofan engine
1322012000661401/12/12Gas-turbine exhaust cone
1332011030896612/22/11Method for manufacturing blisks
1342011028874011/24/11Engine synchronization method
1352011027168011/10/11Lean premix burner of a gas-turbine engine provided with a concentric annular central body
1362011027168111/10/11Lean premix burner of a gas-turbine engine provided with a flow-guiding element
1372011027176511/10/11Method and the detection of defects in the raceways of bearing shells and in the rolling elements of ceramic hybrid bearings
1382011027183711/10/11Centrifugal oil separator for an aircraft engine
1392011025596410/20/11Bypass duct of a turbofan engine
1402011021978209/15/11Aerodynamically shaped supporting and/or fairing element in the bypass duct of a gas-turbine engine
1412011021517209/08/11Aircraft engine with optimized oil heat exchanger
1422011020945809/01/11Aircraft gas turbine engine
1432011021194709/01/11Bypass duct of a turbo engine
1442011017984407/28/11Method and surface strengthening of blisk blades
1452011018249907/28/11Method for determining the surface coverage obtained by shot peening
1462011017399007/21/11Intermediate casing for a gas-turbine engine
1472011014622306/23/11Arrangement for the discharge of exhaust air separated from the lubricating oil de-aeration system of a gas-turbine engine
1482011014622406/23/11Arrangement for the discharge of oil-venting air on a gas-turbine engine
1492011013992506/16/11Arrangement for the suspension of a jet engine to a supporting structure
1502011012772806/02/11Sealing rings for a labyrinth seal
1512011012113605/26/11Aircraft de-icing device and engine nacelle of an aircraft gas turbine with de-icing device
1522011011690805/19/11Gas turbine engine with an arrangement for measuring the shaft rotation speed
1532011007007403/24/11Gas turbine with a shroud and labyrinth-type sealing arrangement
1542011003866602/17/11Engine shaft of hybrid design
1552011002709102/03/11Axial-flow compressor, more particularly one for an aircraft gas-turbine engine
1562011001688301/27/11Cross-sectional profile for the struts or the fairing of struts and service lines of a turbofan engine
1572011001105801/20/11Turbofan engine
1582011001109301/20/11Gas-turbine combustion chamber with starter film for cooling the combustion chamber wall
1592011001403701/20/11Axial-flow compressor with a flow pulse generator
1602011001404001/20/11Fluid flow machine with blade row group
1612011001405701/20/11Engine blade with excessive leading edge loading
1622011001405801/20/11Propeller
1632011000523301/13/11Combustion chamber head of a gas turbine
1642011000585801/13/11Noise-reduced aircraft engine and reducing noise emissions of an aircraft engine
1652010030362912/02/10Fluid flow machine with a blade row group featuring a meridional edge distance
1662010028777211/18/10Method for surface strengthening and smoothening of metallic components
1672010028864811/18/10Method and etching the surfaces of integrally bladed rotors
1682010025819910/14/10Intake cone in a fiber compound material for a gas-turbine engine
1692010025901310/14/10Abradable labyrinth seal for a fluid-flow machine
1702010023295409/16/10Bypass duct of a turbofan engine
1712010022390509/09/10Scoop of a running-gap control system of an aircraft gas turbine
1722010022434809/09/10Method for the manufacture of an ejector nozzle tube
1732010021228508/26/10Turboprop propulsion unit with pusher propeller
1742010021548108/26/10Running-gap control system of an aircraft gas turbine
1752010019258808/05/10Method 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
1762010017525607/15/10Method for the manufacture of the blade tips of rotor wheels made in blisk design
1772010017609707/15/10Arrangement for the repair of the blades of blisk drums by means of laser deposition welding
1782010015552606/24/10Aircraft with tail propeller-engine layout
1792010016110706/24/10Machine control for a numerically controlled machine tool
1802010014802706/17/10Sensor bracket for at least one sensor on a gas turbine
1812010014844906/17/10Segmented sealing lips for labyrinth sealing rings
1822010015069606/17/10Fan casing for a jet engine
1832010013924106/10/10Flow divider for a fan engine
1842010013927806/10/10Method and the operation of a turboprop aircraft engine provided with pusher propellers
1852010014023006/10/10Method for the manufacture of a welded rotor for a gas-turbine engine
1862010014314006/10/10Fluid flow machine with sidewall boundary layer barrier
1872010012658905/27/10Device for the prevention of high oil tank pressures under negative g conditions
1882010012666205/27/10Method for the manufacture of hybrid components for aircraft gas turbines
1892010012965105/27/10Hybrid component for a gas-turbine engine
1902010012251805/20/10Oil system heating for aircraft gas turbines
1912010012448705/20/10Multi-vane variable stator unit of a fluid flow machine
1922010010918405/06/10Method for the manufacture of an engine shaft
1932010011170205/06/10Hub cone for an aircraft engine
1942010011317005/06/10Engine shaft for a gas-turbine engine
1952010011317105/06/10Engine shaft in the form of a fiber-composite plastic tube with metallic driving and driven protrusions
1962010009852704/22/10Fluid flow machine with peripheral energization near the suction side
1972010009853004/22/10Compressor for a gas turbine
1982010009853604/22/10Fluid flow machine with running gap retraction
1992010005111203/04/10Intake cone for a gas-turbine engine
2002010003463702/11/10Fluid flow machine
2012010002421402/04/10Method for the manufacture of metallic components
2022010002131001/28/10Method for improving the flow conditions on the propeller or fan of an aircraft engine and accordingly designed hub cone
2032010001495601/21/10Fluid flow machine featuring a groove on a running gap of a blade end
2042010001496001/21/10Gas-turbine engine with variable stator vanes
2052010000577601/14/10Fuel supply system for a gas-turbine engine
2062010000019801/07/10Gas turbine with at least one multi-stage compressor unit including several compressor modules
2072010000022601/07/10Turbofan engine with at least one driving at least one generator
2082009031400412/24/09Turboprop engine with an the generation of a cooling airflow
2092009031723212/24/09Blade shroud with aperture
2102013032687612/12/13Method for repairing compressor or turbine drums
2112010002131001/28/10Method for improving the flow conditions on the propeller or fan of an aircraft engine and accordingly designed hub cone
2122010001496001/21/10Gas-turbine engine with variable stator vanes
2132010000577601/14/10Fuel supply system for a gas-turbine engine
2142010000022601/07/10Turbofan engine with at least one driving at least one generator



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This listing is an abstract for educational and research purposes is only meant as a recent sample of applications filed, not a comprehensive history. Freshpatents.com is not affiliated or associated with Rolls royce Deutschland Ltd & Co Kg in any way and there may be associated servicemarks. This data is also published to the public by the USPTO and available for free on their website. Note that there may be alternative spellings for Rolls royce Deutschland Ltd & Co Kg with additional patents listed. Browse our Agent directory for other possible listings. Page by FreshPatents.com

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