Air intakes for gas-turbine plants or jet-propulsion plants

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F02C7/04

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Parent Industries

FMECHANICAL ENGINEERING LIGHTING HEATING WEAPONS BLASTING ENGINES OR PUMPS F02Combustion engines F02CGAS-TURBINE PLANTS AIR INTAKES FOR JET-PROPULSION PLANTS CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00 Air intakes for jet-propulsion plants

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F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants

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Patents Grantslast 30 patents

Information Patent Grant
Exhaust device and installation method thereof, turbine fracturing...
- Patent number 12,270,314
- Issue date Apr 8, 2025
- Yantai Jereh Petroleum Equipment & Technologies Co., Ltd.
- Peng Zhang
- E21 - EARTH DRILLING MINING
Information Patent Grant
Piping support structure, intake duct, and gas turbine
- Patent number 12,270,335
- Issue date Apr 8, 2025
- Mitsubishi Heavy Industries, Ltd.
- Naoto Imajo
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Shapeable inlet manifold for hypersonic scramjet
- Patent number 12,270,334
- Issue date Apr 8, 2025
- The Government of the United States of America, as represented by the Secreta...
- Jesse R Maxwell
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Defrosting and acoustic treatment device for an air intake lip of a...
- Patent number 12,269,604
- Issue date Apr 8, 2025
- SAFRAN NACELLES
- Virginie Emmanuelle Anne Marie Digeos
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Build plate integrated into additive manufactured component
- Patent number 12,264,624
- Issue date Apr 1, 2025
- RTX Corporation
- Lawrence A. Binek
- B22 - CASTING POWDER METALLURGY
Information Patent Grant
Acoustic attenuation panel and its manufacturing methods
- Patent number 12,264,625
- Issue date Apr 1, 2025
- SAFRAN NACELLES
- Pierre Caruel
- B32 - LAYERED PRODUCTS
Information Patent Grant
Anti-ice system for gas turbine engine and inlet guide vane
- Patent number 12,258,874
- Issue date Mar 25, 2025
- Rolls-Royce North American Technologies Inc.
- Eric Engebretsen
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Hypersonic large internal contraction ratio air inlet channel havin...
- Patent number 12,253,049
- Issue date Mar 18, 2025
- Nanjing University of Aeronautics and Astronautics
- Hexia Huang
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
De-ice system and apparatus for turbine engines
- Patent number 12,253,025
- Issue date Mar 18, 2025
- General Electric Company
- Jeffrey Douglas Rambo
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Combined cycle propulsion system for hypersonic flight
- Patent number 12,253,050
- Issue date Mar 18, 2025
- General Electric Company
- Arin Elspeth Lastufka Cross
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Engine nacelle anti-ice swirl system with unsteady fluid flow
- Patent number 12,241,410
- Issue date Mar 4, 2025
- The Boeing Company
- Rene Woszidlo
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Variable turbine geometry component wear mitigation in radial turbo...
- Patent number 12,234,766
- Issue date Feb 25, 2025
- BorgWarner Inc.
- Abhishek Biswas
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Air inlet for an aircraft propulsion unit comprising mobile members...
- Patent number 12,234,790
- Issue date Feb 25, 2025
- SAFRAN AIRCRAFT ENGINES
- Ulrick Souveton
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Jet pump system
- Patent number 12,234,840
- Issue date Feb 25, 2025
- Honeywell International Inc.
- Gary Kumagai
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Recirculation fan turbocharger assembly and fuel cell system
- Patent number 12,228,073
- Issue date Feb 18, 2025
- BorgWarner Inc.
- Vincent Hernandez-Gonzalez
- H01 - BASIC ELECTRIC ELEMENTS
Information Patent Grant
Compressor with anti-ice inlet
- Patent number 12,221,894
- Issue date Feb 11, 2025
- General Electric Company Polska sp. z o.o.
- Dariusz Olczak
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Passive bypass for mitigation of inlet buzz in supersonic or hypers...
- Patent number 12,221,925
- Issue date Feb 11, 2025
- Raytheon Company
- Timothy O'Brien
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine combustor with dynamics mitigation system
- Patent number 12,215,867
- Issue date Feb 4, 2025
- GE INFRASTRUCTURE TECHNOLOGY LLC
- Jonathan Dwight Berry
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Aircraft with bifurcated air inlet
- Patent number 12,208,909
- Issue date Jan 28, 2025
- Textron Innovations Inc.
- Steven Ray Ivans
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Propulsion flow path duct systems and methods
- Patent number 12,196,115
- Issue date Jan 14, 2025
- The Boeing Company
- Michael Hayes
- G10 - MUSICAL INSTRUMENTS ACOUSTICS
Information Patent Grant
Inlet turning vanes having trailing edge features for improved flow...
- Patent number 12,188,408
- Issue date Jan 7, 2025
- Rolls-Royce North American Technologies Inc.
- Scott Schwenker
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine with acoustic liner
- Patent number 12,188,409
- Issue date Jan 7, 2025
- RTX Corporation
- Anthony R. Bifulco
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Icing condition identification for gas turbine engine
- Patent number 12,188,410
- Issue date Jan 7, 2025
- Pratt & Whitney Canada Corp.
- Zubair Ahmad
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Reverse flow gas turbine engine having electric machine
- Patent number 12,188,414
- Issue date Jan 7, 2025
- General Electric Company
- Arthur William Sibbach
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Zero emission supersonic fan engine
- Patent number 12,188,434
- Issue date Jan 7, 2025
- SiriNor AS
- Pramod Vaditya
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Acoustic panel for a turbine engine
- Patent number 12,180,891
- Issue date Dec 31, 2024
- SAFRAN NACELLES
- Marc Versaevel
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Pressure control for bifurcated flow of a turbine engine
- Patent number 12,173,651
- Issue date Dec 24, 2024
- RTX Corporation
- Neil J. Terwilliger
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Acoustic management, on a turbomachine or a nacelle
- Patent number 12,173,652
- Issue date Dec 24, 2024
- SAFRAN AIRCRAFT ENGINES
- Norman Bruno André Jodet
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Ice reduction mechanism for turbofan engine
- Patent number 12,168,956
- Issue date Dec 17, 2024
- General Electric Company
- Arthur William Sibbach
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Module ensuring an attenuation of sound waves and a heat exchange
- Patent number 12,163,469
- Issue date Dec 10, 2024
- Airbus Operations SAS
- Arnaud Bourhis
- F28 - HEAT EXCHANGE IN GENERAL

Patents Applicationslast 30 patents

Information Patent Application
REVERSE FLOW GAS TURBINE ENGINE HAVING ELECTRIC MACHINE
- Publication number 20250101918
- Publication date Mar 27, 2025
- GENERAL ELECTRIC COMPANY
- Arthur William Sibbach
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRCRAFT
- Publication number 20250092823
- Publication date Mar 20, 2025
- Rolls-Royce plc
- Natalie C. WONG
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
AIRCRAFT ENGINE ASSEMBLY FOR CONTROLLING ENGINE OIL FLOW DURING FIR...
- Publication number 20250084790
- Publication date Mar 13, 2025
- Pratt & Whitney Canada Corp.
- Kashif Mohammed
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE BYPASS LOUVER AND BAFFLE RIB DESIGN
- Publication number 20250075657
- Publication date Mar 6, 2025
- Pratt & Whitney Canada Corp.
- Marco P. Convertini
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ICE REDUCTION MECHANISM FOR TURBOFAN ENGINE
- Publication number 20250067215
- Publication date Feb 27, 2025
- GENERAL ELECTRIC COMPANY
- Arthur William Sibbach
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE WITH CORE DEBRIS PROTECTION
- Publication number 20250059915
- Publication date Feb 20, 2025
- RTX Corporation
- Michael G. McCaffrey
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ANTI-ICING AND BLEED HEAT SYSTEM FOR A GAS TURBINE SYSTEM
- Publication number 20250059913
- Publication date Feb 20, 2025
- GE INFRASTRUCTURE TECHNOLOGY LLC
- Laxmikant Merchant
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ANTI-ICING AND BLEED HEAT SYSTEM FOR A GAS TURBINE SYSTEM
- Publication number 20250059914
- Publication date Feb 20, 2025
- GE INFRASTRUCTURE TECHNOLOGY LLC
- Laxmikant Merchant
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SEGMENTED NACELLE INLET LIP WITH ELECTRIC ANTI-ICING SYSTEM
- Publication number 20250052195
- Publication date Feb 13, 2025
- Jeffrey W. Moe
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
REVERSE FLOW GAS TURBINE ENGINE HAVING ELECTRIC MACHINE
- Publication number 20250052194
- Publication date Feb 13, 2025
- GENERAL ELECTRIC COMPANY
- Arthur William Sibbach
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
OUTER BARREL SUPPORT STRUCTURE FOR NACELLE INLET STRUCTURE
- Publication number 20250051022
- Publication date Feb 13, 2025
- Rohr, Inc.
- Jasen A. Miner
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRCRAFT AIR INTAKE COMPRISING AN OUTER WALL AND FRONT AND REAR FRA...
- Publication number 20250042565
- Publication date Feb 6, 2025
- Airbus Operations SAS
- Emeric CHANCERELLE
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIR INTAKE WITH CHANGING WALL THICKNESS AND ASSOCIATED NACELLE
- Publication number 20250042566
- Publication date Feb 6, 2025
- AIRBUS OPERATIONS (SAS)
- Umberto Gastaldi
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE HAVING A HEAT EXCHANGER LOCATED IN AN ANNULAR DUCT
- Publication number 20250043720
- Publication date Feb 6, 2025
- GENERAL ELECTRIC COMPANY
- Scott Alan Schimmels
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRCRAFT PROPULSION SYSTEM WITH VARIABLE AREA INLET ASSEMBLY
- Publication number 20250027446
- Publication date Jan 23, 2025
- Rohr, Inc.
- Timothy Gormley
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NACELLE INLET DUCT FOR A DUCTED FAN ENGINE
- Publication number 20250012216
- Publication date Jan 9, 2025
- GENERAL ELECTRIC COMPANY
- Nikolai Pastouchenko
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
ANTI-ICE SYSTEM FOR GAS TURBINE ENGINE AND INLET GUIDE VANE
- Publication number 20250012202
- Publication date Jan 9, 2025
- Rolls-Royce North American Technologies Inc.
- Eric Engebretsen
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
AIR INTAKE MODULE FOR AN AIRCRAFT TURBOMACHINE AND METHOD FOR DE-IC...
- Publication number 20240425191
- Publication date Dec 26, 2024
- SAFRAN NACELLES
- Pierre Charles Caruel
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
CIRCUMFERENTIALLY VARYING FAN CASING TREATMENTS FOR REDUCING FAN NO...
- Publication number 20240426247
- Publication date Dec 26, 2024
- GENERAL ELECTRIC COMPANY
- Trevor Howard Wood
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
COLLAPSIBLE COVER FOR ENGINE INLET AND METHOD FOR COVERING ENGINE I...
- Publication number 20240417104
- Publication date Dec 19, 2024
- GULFSTREAM AEROSPACE CORPORATION
- Andrew Martin
- A45 - HAND OR TRAVELLING ARTICLES
Information Patent Application
AIRCRAFT AIR SYSTEM WITH DEDICATED COMPRESSOR(S)
- Publication number 20240418122
- Publication date Dec 19, 2024
- Pratt & Whitney Canada Corp.
- Michel Bousquet
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
PIPING SUPPORT STRUCTURE, INTAKE DUCT, AND GAS TURBINE
- Publication number 20240418123
- Publication date Dec 19, 2024
- Mitsubishi Heavy Industries, Ltd.
- Naoto IMAJO
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NACELLE INLET STRUCTURES, ENGINE ASSEMBLIES AND VEHICLES INCLUDING...
- Publication number 20240410316
- Publication date Dec 12, 2024
- The Boeing Company
- Joseph B. LaBelle
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
OBJECT DIRECTION MECHANISM FOR TURBOFAN ENGINE
- Publication number 20240410317
- Publication date Dec 12, 2024
- GENERAL ELECTRIC COMPANY
- Arthur William Sibbach
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE WITH DIFFUSER STEAM INJECTION INTO A COMBUSTOR
- Publication number 20240401527
- Publication date Dec 5, 2024
- GENERAL ELECTRIC COMPANY
- Pradeep Naik
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
INLET SYSTEM FOR AUXILIARY POWER UNIT
- Publication number 20240400219
- Publication date Dec 5, 2024
- Honeywell International Inc.
- Bruce Bouldin
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Method for Designing Formable Additively Manufactured Acoustic Liners
- Publication number 20240401528
- Publication date Dec 5, 2024
- RAYTHEON TECHNOLOGIES CORPORATION
- Jackson David JOHNSON
- B22 - CASTING POWDER METALLURGY
Information Patent Application
PRESSURE CONTROL FOR BIFURCATED FLOW OF A TURBINE ENGINE
- Publication number 20240384684
- Publication date Nov 21, 2024
- Neil J. Terwilliger
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRCRAFT PRECIPITATION MONITORING SYSTEM
- Publication number 20240376844
- Publication date Nov 14, 2024
- RTX Corporation
- Luis Alexander Muniz
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ENGINE HAVING AN OPEN FAN WITH REDUCED BOUNDARY LAYER INDUCED DISTO...
- Publication number 20240369016
- Publication date Nov 7, 2024
- GENERAL ELECTRIC COMPANY
- William Joseph Bowden
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES

Air intakes for gas-turbine plants or jet-propulsion plants

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Exhaust device and installation method thereof, turbine fracturing...

Piping support structure, intake duct, and gas turbine

Shapeable inlet manifold for hypersonic scramjet

Defrosting and acoustic treatment device for an air intake lip of a...

Build plate integrated into additive manufactured component

Acoustic attenuation panel and its manufacturing methods

Anti-ice system for gas turbine engine and inlet guide vane

Hypersonic large internal contraction ratio air inlet channel havin...

De-ice system and apparatus for turbine engines

Combined cycle propulsion system for hypersonic flight

Engine nacelle anti-ice swirl system with unsteady fluid flow

Variable turbine geometry component wear mitigation in radial turbo...

Air inlet for an aircraft propulsion unit comprising mobile members...

Jet pump system

Recirculation fan turbocharger assembly and fuel cell system

Compressor with anti-ice inlet

Passive bypass for mitigation of inlet buzz in supersonic or hypers...

Gas turbine combustor with dynamics mitigation system

Aircraft with bifurcated air inlet

Propulsion flow path duct systems and methods

Inlet turning vanes having trailing edge features for improved flow...

Gas turbine engine with acoustic liner

Icing condition identification for gas turbine engine

Reverse flow gas turbine engine having electric machine

Zero emission supersonic fan engine

Acoustic panel for a turbine engine

Pressure control for bifurcated flow of a turbine engine

Acoustic management, on a turbomachine or a nacelle

Ice reduction mechanism for turbofan engine

Module ensuring an attenuation of sound waves and a heat exchange

Patents Applicationslast 30 patents

REVERSE FLOW GAS TURBINE ENGINE HAVING ELECTRIC MACHINE

AIRCRAFT

AIRCRAFT ENGINE ASSEMBLY FOR CONTROLLING ENGINE OIL FLOW DURING FIR...

GAS TURBINE ENGINE BYPASS LOUVER AND BAFFLE RIB DESIGN

ICE REDUCTION MECHANISM FOR TURBOFAN ENGINE

GAS TURBINE ENGINE WITH CORE DEBRIS PROTECTION

ANTI-ICING AND BLEED HEAT SYSTEM FOR A GAS TURBINE SYSTEM

ANTI-ICING AND BLEED HEAT SYSTEM FOR A GAS TURBINE SYSTEM

SEGMENTED NACELLE INLET LIP WITH ELECTRIC ANTI-ICING SYSTEM

REVERSE FLOW GAS TURBINE ENGINE HAVING ELECTRIC MACHINE

OUTER BARREL SUPPORT STRUCTURE FOR NACELLE INLET STRUCTURE

AIRCRAFT AIR INTAKE COMPRISING AN OUTER WALL AND FRONT AND REAR FRA...

AIR INTAKE WITH CHANGING WALL THICKNESS AND ASSOCIATED NACELLE

GAS TURBINE ENGINE HAVING A HEAT EXCHANGER LOCATED IN AN ANNULAR DUCT

AIRCRAFT PROPULSION SYSTEM WITH VARIABLE AREA INLET ASSEMBLY

NACELLE INLET DUCT FOR A DUCTED FAN ENGINE

ANTI-ICE SYSTEM FOR GAS TURBINE ENGINE AND INLET GUIDE VANE

AIR INTAKE MODULE FOR AN AIRCRAFT TURBOMACHINE AND METHOD FOR DE-IC...

CIRCUMFERENTIALLY VARYING FAN CASING TREATMENTS FOR REDUCING FAN NO...

COLLAPSIBLE COVER FOR ENGINE INLET AND METHOD FOR COVERING ENGINE I...

AIRCRAFT AIR SYSTEM WITH DEDICATED COMPRESSOR(S)

PIPING SUPPORT STRUCTURE, INTAKE DUCT, AND GAS TURBINE

NACELLE INLET STRUCTURES, ENGINE ASSEMBLIES AND VEHICLES INCLUDING...

OBJECT DIRECTION MECHANISM FOR TURBOFAN ENGINE

GAS TURBINE WITH DIFFUSER STEAM INJECTION INTO A COMBUSTOR

INLET SYSTEM FOR AUXILIARY POWER UNIT

Method for Designing Formable Additively Manufactured Acoustic Liners

PRESSURE CONTROL FOR BIFURCATED FLOW OF A TURBINE ENGINE

AIRCRAFT PRECIPITATION MONITORING SYSTEM

ENGINE HAVING AN OPEN FAN WITH REDUCED BOUNDARY LAYER INDUCED DISTO...