Henry Tubbs

Person

Tetbury, GB

People

Patents Grantslast 30 patents

Information Patent Grant
Gas turbine blade tip clearance control structure
- Patent number 6,863,495
- Issue date Mar 8, 2005
- Rolls-Royce PLC
- Mark A Halliwell
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Heatable member and temperature monitor therefor
- Patent number 6,513,971
- Issue date Feb 4, 2003
- Rolls-Royce PLC
- Henry Tubbs
- G01 - MEASURING TESTING
Information Patent Grant
Ducted fan gas turbine engine with fan shaft frangible connection
- Patent number 6,079,200
- Issue date Jun 27, 2000
- Rolls-Royce plc
- Henry Tubbs
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Apparatus for controlling cooling air in gas turbine engine
- Patent number 6,067,792
- Issue date May 30, 2000
- Rolls-Royce plc
- Henry Tubbs
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine turbine system
- Patent number 5,941,687
- Issue date Aug 24, 1999
- Rolls-Royce plc
- Henry Tubbs
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Stator vane assembly for controlling air flow in a gas turbine engien
- Patent number 5,332,357
- Issue date Jul 26, 1994
- Industria de Turbo Propulsores S.A.
- Henry Tubbs
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Gas turbine engine variable aerofoil vane actuation mechanism
- Patent number 5,316,438
- Issue date May 31, 1994
- Industria de Turbo Propulsores S.A.
- Henry Tubbs
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Cooled aerofoil blade for vane for a gas turbine engine
- Patent number 5,263,820
- Issue date Nov 23, 1993
- Rolls-Royce
- Henry Tubbs
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Grant
Variable guide vane arrangement for a compressor
- Patent number 4,978,280
- Issue date Dec 18, 1990
- Rolls-Royce plc
- Henry Tubbs
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Variable guide vane arrangement for a compressor
- Patent number 4,867,635
- Issue date Sep 19, 1989
- Rolls-Royce plc
- Henry Tubbs
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Fluid flow reversing apparatus
- Patent number 4,732,535
- Issue date Mar 22, 1988
- Rolls-Royce plc
- Henry Tubbs
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Rotor blade for a gas turbine engine
- Patent number 4,302,153
- Issue date Nov 24, 1981
- Rolls-Royce Limited
- Henry Tubbs
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Gas turbine engine having a cooled turbine
- Patent number 4,302,148
- Issue date Nov 24, 1981
- Rolls-Royce Limited
- Henry Tubbs
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Shroud ring aerofoil capture
- Patent number 4,199,300
- Issue date Apr 22, 1980
- Rolls-Royce Limited
- Henry Tubbs
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES

Patents Applicationslast 30 patents

Information Patent Application
Gas turbine blade tip clearance control structure
- Publication number 20040018084
- Publication date Jan 29, 2004
- Mark A. Halliwell
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Heatable member and temperature monitor therefor
- Publication number 20020064205
- Publication date May 30, 2002
- Henry Tubbs
- G01 - MEASURING TESTING

Henry Tubbs

Person

Patents Grantslast 30 patents

Gas turbine blade tip clearance control structure

Heatable member and temperature monitor therefor

Ducted fan gas turbine engine with fan shaft frangible connection

Apparatus for controlling cooling air in gas turbine engine

Gas turbine engine turbine system

Stator vane assembly for controlling air flow in a gas turbine engien

Gas turbine engine variable aerofoil vane actuation mechanism

Cooled aerofoil blade for vane for a gas turbine engine

Variable guide vane arrangement for a compressor

Variable guide vane arrangement for a compressor

Fluid flow reversing apparatus

Rotor blade for a gas turbine engine

Gas turbine engine having a cooled turbine

Shroud ring aerofoil capture

Patents Applicationslast 30 patents

Gas turbine blade tip clearance control structure

Heatable member and temperature monitor therefor