due to high angle of attack of aircraft

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CPC
F05D2270/1022

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FMECHANICAL ENGINEERING LIGHTING HEATING WEAPONS BLASTING ENGINES OR PUMPS F05Engines, pumps F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS F05D2270/00Control

Current Industry

F05D2270/1022due to high angle of attack of aircraft

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Patents Grantslast 30 patents

Information Patent Grant
Methods and apparatus for reducing flow distortion at engine fans o...
- Patent number 11,268,399
- Issue date Mar 8, 2022
- The Boeing Company
- Arvin Shmilovich
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Methods and apparatus for reducing flow distortion at engine fans o...
- Patent number 10,605,113
- Issue date Mar 31, 2020
- The Boeing Company
- Arvin Shmilovich
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Takeoff power management system and method for gas turbine engines
- Patent number 10,293,951
- Issue date May 21, 2019
- United Technologies Corporation
- Matthew R. Feulner
- G05 - CONTROLLING REGULATING
Information Patent Grant
Protecting the operating margin of a gas turbine engine having vari...
- Patent number 9,194,301
- Issue date Nov 24, 2015
- United Technologies Corporation
- Wayne P. Parente
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Closed-loop control for a gas turbine with actively stabilized comp...
- Patent number 8,550,767
- Issue date Oct 8, 2013
- MTU Aero Engines GmbH
- Wolfgang Horn
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Fan nacelle flow control
- Patent number 8,529,188
- Issue date Sep 10, 2013
- United Technologies Corporation
- Michael Winter
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Apparatus and method for controlling a compressor
- Patent number 8,096,756
- Issue date Jan 17, 2012
- Pratt & Whitney Canada Corp.
- Huu Duc Vo
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Active vaned passage casing treatment
- Patent number 5,431,533
- Issue date Jul 11, 1995
- United Technologies Corporation
- David E. Hobbs
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES

Patents Applicationslast 30 patents

Information Patent Application
METHODS AND APPARATUS FOR REDUCING FLOW DISTORTION AT ENGINE FANS O...
- Publication number 20200182080
- Publication date Jun 11, 2020
- The Boeing Company
- Arvin Shmilovich
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
PROTECTING OPERATING MARGIN OF A GAS TURBINE ENGINE
- Publication number 20130319009
- Publication date Dec 5, 2013
- Wayne P. Parente
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
CLOSED-LOOP CONTROL FOR A GAS TURBINE WITH ACTIVELY STABILIZED COMP...
- Publication number 20100196137
- Publication date Aug 5, 2010
- MTU Aero Engines GmbH
- Wolfgang Horn
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
APPARATUS AND METHOD FOR CONTROLLING A COMPRESSOR
- Publication number 20100040453
- Publication date Feb 18, 2010
- PRATT & WHITNEY CANADA CORP.
- Huu Duc VO
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
FAN NACELLE FLOW CONTROL
- Publication number 20090155072
- Publication date Jun 18, 2009
- Michael Winter
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

due to high angle of attack of aircraft

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Methods and apparatus for reducing flow distortion at engine fans o...

Methods and apparatus for reducing flow distortion at engine fans o...

Takeoff power management system and method for gas turbine engines

Protecting the operating margin of a gas turbine engine having vari...

Closed-loop control for a gas turbine with actively stabilized comp...

Fan nacelle flow control

Apparatus and method for controlling a compressor

Active vaned passage casing treatment

Patents Applicationslast 30 patents

METHODS AND APPARATUS FOR REDUCING FLOW DISTORTION AT ENGINE FANS O...

PROTECTING OPERATING MARGIN OF A GAS TURBINE ENGINE

CLOSED-LOOP CONTROL FOR A GAS TURBINE WITH ACTIVELY STABILIZED COMP...

APPARATUS AND METHOD FOR CONTROLLING A COMPRESSOR

FAN NACELLE FLOW CONTROL