United Kingdom
102
2024-10-03
102
2025-01-28
These are the the leading inventors for applications assigned to Rolls-Royce PLC:
Rolls-Royce PLC based in , GB has been assigned the rights to these inventions. The list includes both Pending Applications and Patent Grants:
Gas turbine engine
#2 | 2024-08-08 ✅ Patent 12,215,632 granted on 2025-02-04Aircraft engine
#3 | 2024-01-11 ✅ Patent 11,946,645 granted on 2024-04-02Combustor casing component for a gas turbine engine
#4 | 2023-03-02 ✅ Patent 12,025,015 granted on 2024-07-02Cleaning system and a method of cleaning
#5 | 2020-08-06 ✅ Patent 10,711,621 granted on 2020-07-14Turbine vane assembly with ceramic matrix composite components and temperature management features
#6 | 2020-02-27 ✅ Patent 10,605,103 granted on 2020-03-31CMC airfoil assembly
#7 | 2019-10-24 ✅ Patent 10,577,961 granted on 2020-03-03Turbine disk with blade supported platforms
#8 | 2019-05-16 ✅ Patent 10,571,244 granted on 2020-02-25Measuring surface roughness
#9 | 2019-05-09 ✅ Patent 10,680,474 granted on 2020-06-09Permanent magnet electrical machine
#10 | 2019-04-11 ✅ Patent 10,641,112 granted on 2020-05-05Bladed disk
#11 | 2018-09-27 ✅ Patent 10,410,102 granted on 2019-09-10Direct part marking
#12 | 2018-09-06 ✅ Patent 10,439,320 granted on 2019-10-08Electrical connector arrangement
#13 | 2018-05-03 ✅ Patent 10,605,201 granted on 2020-03-31Gas turbine exhaust cooling system
#14 | 2017-12-28 ✅ Patent 10,584,605 granted on 2020-03-10Split line flow path seals
#15 | 2017-10-05 ✅ Patent 10,429,071 granted on 2019-10-01Fuel injector
#16 | 2017-05-25 ✅ Patent 10,317,084 granted on 2019-06-11Additive layer manufacturing for fuel injectors
#17 | 2017-02-09 ✅ Patent 10,295,187 granted on 2019-05-21Fuel nozzle having aerodynamically shaped helical turning vanes
#18 | 2016-12-22 ✅ Patent 10,767,864 granted on 2020-09-08Turbine cooled cooling air by tubular arrangement
#19 | 2016-11-17 ✅ Patent 10,316,682 granted on 2019-06-11Composite keystoned blade track
#20 | 2016-11-03 ✅ Patent 10,563,535 granted on 2020-02-18Keystoned blade track
#21 | 2016-11-03 ✅ Patent 10,550,709 granted on 2020-02-04Full hoop blade track with flanged segments
#22 | 2016-11-03 ✅ Patent 10,494,935 granted on 2019-12-03Brazed blade track for a gas turbine engine
#23 | 2016-05-26 ✅ Patent 10,030,540 granted on 2018-07-24Fan case liner removal with external heat mat
#24 | 2016-03-17 ✅ Patent 9,500,080 granted on 2016-11-22Method of replacing damaged aerofoil
#25 | 2014-09-04 ✅ Patent 9,816,963 granted on 2017-11-14High pressure compressor thermal management
#26 | 2013-09-12 ✅ Patent 8,821,119 granted on 2014-09-02Blade
#27 | 2013-08-08 ✅ Patent 9,228,741 granted on 2016-01-05Liquid fuel swirler
#28 | 2013-05-16 ✅ Patent 9,330,231 granted on 2016-05-03Method for determining a flow behavior of a medium
#29 | 2013-02-14 ✅ Patent 8,461,704 granted on 2013-06-11Gas turbine engine apparatus
#30 | 2012-09-13 ✅ Patent 9,310,073 granted on 2016-04-12Liquid swirler flow control
#31 | 2012-09-13 ✅ Patent 9,383,097 granted on 2016-07-05Systems and method for cooling a staged airblast fuel injector
#32 | 2012-03-01 ✅ Patent 9,046,039 granted on 2015-06-02Staged pilots in pure airblast injectors for gas turbine engines
#33 | 2011-12-01 ✅ Patent 8,406,690 granted on 2013-03-26Data transmission system
#34 | 2011-09-29 ✅ Patent 8,864,451 granted on 2014-10-21Interstage seal
#35 | 2011-09-22 ✅ Patent 8,521,493 granted on 2013-08-27Rotating blade analysis
#36 | 2011-07-28 ✅ Patent 8,689,440 granted on 2014-04-08Method of forming a hollow component with an internal structure
#37 | 2011-04-07 ✅ Patent 8,764,382 granted on 2014-07-01Method for forming a pressure measurement hole in a component
#38 | 2011-03-31 ✅ Patent 8,591,172 granted on 2013-11-26Containment casing for an aero engine
#39 | 2011-03-10 ✅ Patent 8,607,542 granted on 2013-12-17Valveless pulse combustor
#40 | 2011-02-17 ✅ Patent 8,636,474 granted on 2014-01-28Rotor assembly for a gas turbine
#41 | 2011-02-10 ✅ Patent 8,833,084 granted on 2014-09-16Combustor tile mounting arrangement
#42 | 2011-01-13 ✅ Patent 9,429,074 granted on 2016-08-30Aerodynamic swept vanes for fuel injectors
#43 | 2010-12-30 ✅ Patent 8,608,448 granted on 2013-12-17Shroudless blade
#44 | 2010-12-23 ✅ Patent 8,596,981 granted on 2013-12-03Annulus filler for a gas turbine engine
#45 | 2010-11-18 ✅ Patent 8,425,192 granted on 2013-04-23Annulus filler
#46 | 2010-11-18 ✅ Patent 8,727,707 granted on 2014-05-20Intake duct liner for a turbofan gas turbine engine
#47 | 2010-11-04 ✅ Patent 8,014,929 granted on 2011-09-06Method of monitoring a gas turbine engine
#48 | 2010-10-21 ✅ Patent 8,096,106 granted on 2012-01-17Drive mechanism
#49 | 2010-10-07 ✅ Patent 9,095,894 granted on 2015-08-04Single crystal casting apparatus
#50 | 2010-09-23 ✅ Patent 8,579,181 granted on 2013-11-12Method of forming an internal structure in a hollow component
#51 | 2010-08-19 ✅ Patent 9,513,009 granted on 2016-12-06Fuel nozzle having aerodynamically shaped helical turning vanes
#52 | 2010-08-12 ✅ Patent 8,596,980 granted on 2013-12-03Vibration damper assembly
#53 | 2010-08-05 ✅ Patent 8,307,882 granted on 2012-11-13Casting method
#54 | 2010-07-29 ✅ Patent 8,366,393 granted on 2013-02-05Rotor blade
#55 | 2010-07-29 ✅ Patent 8,419,351 granted on 2013-04-16Rotation arrangement
#56 | 2010-07-22 ✅ Patent 8,578,700 granted on 2013-11-12Gas turbine engine with fluid mixing arrangement
#57 | 2010-06-24 ✅ Patent 8,864,465 granted on 2014-10-21Test blade
#58 | 2010-06-24 ✅ Patent 8,702,382 granted on 2014-04-22Composite component
#59 | 2010-06-17 ✅ Patent 8,584,442 granted on 2013-11-19Gas turbine engine variable area exhaust nozzle
#60 | 2010-05-13 ✅ Patent 8,733,105 granted on 2014-05-27Fuel injector
#61 | 2010-03-18 ✅ Patent 8,159,081 granted on 2012-04-17Controlling propeller rotor overspeed
#62 | 2010-03-04 ✅ Patent 8,366,378 granted on 2013-02-05Blade assembly
#63 | 2010-03-04 ✅ Patent 8,568,082 granted on 2013-10-29Blade and a method for making a blade
#64 | 2010-03-04 ✅ Patent 8,430,623 granted on 2013-04-30Blade
#65 | 2010-01-28 ✅ Patent 8,418,953 granted on 2013-04-16Gas turbine engine nacelle
#66 | 2010-01-21 ✅ Patent 8,429,914 granted on 2013-04-30Fuel injection system
#67 | 2009-12-17 ✅ Patent 8,152,094 granted on 2012-04-10Engine mounting apparatus
#68 | 2009-12-10 ✅ Patent 8,291,710 granted on 2012-10-23Gas turbine engine exhaust nozzle having a composite article having a shape memory material member
#69 | 2009-12-03 ✅ Patent 8,429,892 granted on 2013-04-30Combustion apparatus having a fuel controlled valve that temporarily flows purging air
#70 | 2009-11-12 ✅ Patent 8,061,699 granted on 2011-11-22Clamping system
#71 | 2009-10-29 ✅ Patent 8,535,013 granted on 2013-09-17Aeroengine fan assembly
#72 | 2009-10-29 ✅ Patent 8,074,923 granted on 2011-12-13Engine mounting apparatus
#73 | 2009-09-10 ✅ Patent 8,287,239 granted on 2012-10-16Annulus filler
#74 | 2009-08-27 ✅ Patent 8,529,204 granted on 2013-09-10Gas turbine engine having a nose cone assembly rigidly attached in an axial direction but flexible in a radial direction
#75 | 2009-08-06 ✅ Patent 8,256,224 granted on 2012-09-04Combustion apparatus
#76 | 2009-07-09 ✅ Patent 8,617,460 granted on 2013-12-31Gas heater
#77 | 2009-06-25 ✅ Patent 8,133,032 granted on 2012-03-13Rotor blades
#78 | 2009-05-21 ✅ Patent 8,186,938 granted on 2012-05-29Turbine apparatus
#79 | 2009-05-21 ✅ Patent 7,688,081 granted on 2010-03-30Apparatus to measure the clearance between a first component and a second component
#80 | 2009-04-23 ✅ Patent 8,137,053 granted on 2012-03-20Assembly having first and second members distinguishable by respective first and second compositions each including one or more isotopes of a same element
#81 | 2009-04-23 ✅ Patent 8,113,004 granted on 2012-02-14Wall element for use in combustion apparatus
#82 | 2009-04-09 ✅ Patent 8,508,095 granted on 2013-08-13Flux-switching machine
#83 | 2009-03-19 ✅ Patent 8,322,595 granted on 2012-12-04Joining method and resultant article
#84 | 2009-02-19 ✅ Patent 7,703,976 granted on 2010-04-27Sensor apparatus
#85 | 2009-02-12 ✅ Patent 7,830,105 granted on 2010-11-09Electrical machine
#86 | 2008-12-11 ✅ Patent 8,779,022 granted on 2014-07-15Polymer components
#87 | 2008-12-11 ✅ Patent 8,266,801 granted on 2012-09-18Method for producing abrasive tips for gas turbine blades
#88 | 2008-11-06 ✅ Patent 9,028,219 granted on 2015-05-12Turbomachine blade
#89 | 2008-11-06 ✅ Patent 8,206,079 granted on 2012-06-26Temperature controlling apparatus
#90 | 2008-10-30 ✅ Patent 8,192,153 granted on 2012-06-05Aerofoil members for a turbomachine
#91 | 2008-10-23 ✅ Patent 8,251,640 granted on 2012-08-28Blade assembly
#92 | 2008-10-16 ✅ Patent 8,132,398 granted on 2012-03-13Apparatus and method of operating a gas turbine engine at start-up
#93 | 2008-09-18 ✅ Patent 8,186,934 granted on 2012-05-29Casing assembly
#94 | 2008-09-04 ✅ Patent 7,915,565 granted on 2011-03-29Apparatus and method for calibrating a laser deposition system
#95 | 2008-08-28 ✅ Patent 7,867,423 granted on 2011-01-11Mould lining
#96 | 2008-08-14 ✅ Patent 8,418,574 granted on 2013-04-16Linear actuator
#97 | 2008-07-31 ✅ Patent 8,328,504 granted on 2012-12-11Aeroengine drain assembly
#98 | 2008-07-31 ✅ Patent 8,430,622 granted on 2013-04-30Turbofan gas turbine engine
#99 | 2008-07-17 ✅ Patent 8,168,046 granted on 2012-05-01Method and apparatus for treating a component of a gas turbine engine
#100 | 2008-07-10 ✅ Patent 8,161,754 granted on 2012-04-24Continuously variable flow nozzle assembly
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