JET-PROPULSION PLANTS

Industry

CPC
F02K

Parent Industries

FMECHANICAL ENGINEERING LIGHTING HEATING WEAPONS BLASTING ENGINES OR PUMPS F02Combustion engines

Current Industry

Sub Industries

F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle Jet pipes or nozzles peculiar thereto F02K3/00Plants including a gas turbine driving a compressor or a ducted fan F02K5/00Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan F02K7/00Plants in which the working fluid is used in a jet only F02K9/00Rocket- engine plants F02K99/00Subject matter not provided for in other groups of this subclass

Industries

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Patents Grantslast 30 patents

Information Patent Grant
Engine backbone bending reduction
- Patent number 12,214,891
- Issue date Feb 4, 2025
- General Electric Company
- Jonathan E. Coleman
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Integral propulsion and auxiliary power generation system for rocke...
- Patent number 12,214,889
- Issue date Feb 4, 2025
- Venus Aerospace Corp.
- Andrew Thomas Duggleby
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Cascade element for a thrust reverser system of an engine
- Patent number 12,215,654
- Issue date Feb 4, 2025
- FACC AG
- Ludwig Loretz
- B33 - ADDITIVE MANUFACTURING TECHNOLOGY
Information Patent Grant
Propulsion apparatus, flying body and propulsion method
- Patent number 12,208,906
- Issue date Jan 28, 2025
- Mitsubish Heavy Industries, Ltd.
- Masayuki Eguchi
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Thrust reverser having three gates
- Patent number 12,209,554
- Issue date Jan 28, 2025
- SAFRAN NACELLES
- Romain Gardel
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Propulsion systems and vehicles using the same
- Patent number 12,209,555
- Issue date Jan 28, 2025
- Morteza Vadipour
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Thrust reverser provided with a lightweight thrust reverser flap
- Patent number 12,209,556
- Issue date Jan 28, 2025
- SAFRAN NACELLES
- Romain Billault
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Rocket engine with dual contour nozzle
- Patent number 12,209,558
- Issue date Jan 28, 2025
- Innovative Rocket Technologies, Inc.
- Asad Malik
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Aircraft assembly fitted with at least one hydrogen-powered thrust...
- Patent number 12,208,915
- Issue date Jan 28, 2025
- SAFRAN NACELLES
- Jihane Bellahbib
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Composite fan case containment hook and improved forward debris cap...
- Patent number 12,209,506
- Issue date Jan 28, 2025
- Rolls-Royce North American Technologies Inc.
- Robert W. Heeter
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Gas turbine engine with forward swept outlet guide vanes
- Patent number 12,209,557
- Issue date Jan 28, 2025
- General Electric Company
- Brandon Wayne Miller
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Transpiration-cooled systems having permeable and non-permeable por...
- Patent number 12,209,559
- Issue date Jan 28, 2025
- Blue Origin, LLC
- Weidong Song
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Hot-gas-generating apparatus with ionic monopropellant and low volt...
- Patent number 12,202,778
- Issue date Jan 21, 2025
- LABORBITAL GMBH
- Saverio Nobbe
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Engine exhaust reverse flow prevention
- Patent number 12,203,415
- Issue date Jan 21, 2025
- Pratt & Whitney Canada Corp.
- John Sgouromitis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Midshaft rating for turbomachine engines
- Patent number 12,203,377
- Issue date Jan 21, 2025
- General Electric Company
- Bhaskar Nanda Mondal
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Air conditioning system equipped with a system for the thermal mana...
- Patent number 12,202,607
- Issue date Jan 21, 2025
- Liebherr-Aerospace Toulouse SAS
- Guillaume Galzin
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Jam detection and jam tolerant motion control
- Patent number 12,203,428
- Issue date Jan 21, 2025
- Woodward, Inc.
- Matthew Polley
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Aircraft power plant with detonation combustion tube
- Patent number 12,203,429
- Issue date Jan 21, 2025
- Pratt & Whitney Canada Corp.
- Etienne Plamondon
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Symmetric cascade thrust reversers and related methods
- Patent number 12,196,156
- Issue date Jan 14, 2025
- The Boeing Company
- Eric S. Samson
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Turbomachine turbine assembly
- Patent number 12,196,157
- Issue date Jan 14, 2025
- SAFRAN CERAMICS
- Eric Conete
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Multimode propulsion system
- Patent number 12,196,158
- Issue date Jan 14, 2025
- PHASE FOUR, INC.
- Jesse Sidhu
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Rocket engine injector
- Patent number 12,196,159
- Issue date Jan 14, 2025
- Rocket Lab USA, Inc.
- Peter Joseph Beck
- B22 - CASTING POWDER METALLURGY
Information Patent Grant
Trailing edge fuel injection enhancement for flame holding mitigation
- Patent number 12,196,421
- Issue date Jan 14, 2025
- Power Systems Mfg., LLC
- Dwain Terrell
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Thermal management system for a gas turbine engine
- Patent number 12,188,433
- Issue date Jan 7, 2025
- Rolls-Royce PLC
- Zahid M Hussain
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Dual-mode ramjet engine with variable fuel injection
- Patent number 12,188,435
- Issue date Jan 7, 2025
- Agency for Defense Development
- Juhyun Bae
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Guide systems for installing aircraft structures
- Patent number 12,187,445
- Issue date Jan 7, 2025
- The Boeing Company
- Luke D. Torjesen
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine bearing and gearbox arrangement
- Patent number 12,188,407
- Issue date Jan 7, 2025
- RTX Corporation
- William G. Sheridan
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Device for attaching a connecting rod small end for a thrust revers...
- Patent number 12,188,432
- Issue date Jan 7, 2025
- SAFRAN NACELLES
- Xavier Cazuc
- 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
Levered counterweight feathering system
- Patent number 12,180,886
- Issue date Dec 31, 2024
- General Electric Company
- Nicholas M. Daggett
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Patents Applicationslast 30 patents

Information Patent Application
METHOD OF ASSEMBLY FOR GAS TURBINE FAN DRIVE GEAR SYSTEM
- Publication number 20250043732
- Publication date Feb 6, 2025
- RTX Corporation
- Michael E. McCune
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
INLETS FOR GAS TURBINE ENGINE BYPASS DUCT HEAT EXCHANGERS
- Publication number 20250043750
- Publication date Feb 6, 2025
- Rolls-Royce North American Technologies Inc.
- Patrick C. Sweeney
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
METHOD FOR COMBUSTING OF HYBRID ROCKET FUEL AND DEVICE FOR COMBUSTING
- Publication number 20250043751
- Publication date Feb 6, 2025
- National University Corporation Hokkaido University
- Harunori NAGATA
- 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
LOCKING ASSEMBLY FOR AN AIRCRAFT PROPULSION SYSTEM THRUST REVERSER
- Publication number 20250043749
- Publication date Feb 6, 2025
- Rohr, Inc.
- Timothy Gormley
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TRANSPIRATION-COOLED SYSTEMS HAVING PERMEABLE AND NON-PERMEABLE POR...
- Publication number 20250035071
- Publication date Jan 30, 2025
- Blue Origin, LLC
- Weidong Song
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
RESIN FORMULATIONS AND RELATED ARTICLES AND METHODS
- Publication number 20250034048
- Publication date Jan 30, 2025
- Northrop Grumman Systems Corporation
- Benjamin W. C. Garcia
- B28 - WORKING CEMENT, CLAY, OR STONE
Information Patent Application
GEARED GAS TURBINE ENGINE
- Publication number 20250035050
- Publication date Jan 30, 2025
- Rolls-Royce plc
- Mark Spruce
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ASSEMBLY FOR AN EXHAUST CONE OF AN AIRCRAFT TURBOMACHINE
- Publication number 20250035069
- Publication date Jan 30, 2025
- SAFRAN NACELLES
- Tony MIOSSEC
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBINE ENGINE CORE AND BYPASS FLOWS
- Publication number 20250035037
- Publication date Jan 30, 2025
- Rolls-Royce plc
- Richard G. STRETTON
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
SOLID ADHESIVE FILM FOR ACOUSTIC LINER AND METHOD
- Publication number 20250037691
- Publication date Jan 30, 2025
- GENERAL ELECTRIC COMPANY
- Wendy Wenling Lin
- G10 - MUSICAL INSTRUMENTS ACOUSTICS
Information Patent Application
SOLID-PROPELLANT THRUSTER WITH AN INTEGRATED CONTROL MEANS AND SYST...
- Publication number 20250035507
- Publication date Jan 30, 2025
- ROXEL FRANCE
- Claude ALARY
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ACTUATION MECHANISM
- Publication number 20250035067
- Publication date Jan 30, 2025
- INDUSTRIA DE TURBO PROPULSORES, S.A.U.
- Alberto GÓMEZ GARCÍA
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
HYBRID ROCKET ENGINE FUEL GRAINS WITH COMPOSITIONAL VARIATIONS
- Publication number 20250035070
- Publication date Jan 30, 2025
- Firehawk Aerospace, Inc.
- Ronald D. Jones
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
HIGH-POWER HYBRID-ELECTRIC PROPULSION SYSTEMS AND METHODS
- Publication number 20250035068
- Publication date Jan 30, 2025
- ePropelled Inc.
- Narotam Singh GREWAL
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TRIPLE-FLOW AXIAL TURBOMACHINE COMPRISING A DIVERGING HEAT EXCHANGE...
- Publication number 20250020077
- Publication date Jan 16, 2025
- SAFRAN AERO BOOSTERS SA
- David WEICKER
- F28 - HEAT EXCHANGE IN GENERAL
Information Patent Application
Vertical Take-Off and Landing Aircraft
- Publication number 20250019072
- Publication date Jan 16, 2025
- Darius Sharifzadeh
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
REUSABLE UPPER STAGE ROCKET WITH AEROSPIKE ENGINE
- Publication number 20250020090
- Publication date Jan 16, 2025
- Blue Origin, LLC
- James R. French
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
FLUID CONTROL VALVE
- Publication number 20250020217
- Publication date Jan 16, 2025
- Rolls-Royce plc
- Jack F. COLEBROOKE
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TRIPLE-FLOW AXIAL TURBOMACHINE COMPRISING A DIVERGING HEAT EXCHANGE...
- Publication number 20250020079
- Publication date Jan 16, 2025
- SAFRAN AERO BOOSTERS SA
- David WEICKER
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINES COMPRISING PITCHED NOSE SPLITTER STRUCTURES AND...
- Publication number 20250012233
- Publication date Jan 9, 2025
- Honeywell International Inc.
- Hasham Chougule
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
INDUCER ASSEMBLY FOR A TURBINE ENGINE
- Publication number 20250010231
- Publication date Jan 9, 2025
- GENERAL ELECTRIC COMPANY
- Timothy Deryck STONE
- B01 - PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
Information Patent Application
THRUST VECTOR CONTROL FOR HYBRID PROPELLANTS ROCKET ENGINE WITH EMB...
- Publication number 20250012237
- Publication date Jan 9, 2025
- LABORATOIRE REACTION DYNAMICS INC.
- Bachar ELZEIN
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE WITH THIRD STREAM
- Publication number 20250012235
- Publication date Jan 9, 2025
- GENERAL ELECTRIC COMPANY
- Brandon Wayne Miller
- 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 20250012236
- Publication date Jan 9, 2025
- GENERAL ELECTRIC COMPANY
- Scott Alan Schimmels
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
PROPULSION DEVICE WITH THRUST REVERSER LOCATING ARRANGEMENT
- Publication number 20250012234
- Publication date Jan 9, 2025
- Rolls-Royce plc
- Richard G. STRETTON
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
FAN APPARATUS WITH LIFT FAN AND LOUVERED COVER
- Publication number 20250010987
- Publication date Jan 9, 2025
- Aurora Flight Sciences Corporation, a subsidiary of The Boeing Company
- Michael J. Duffy
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
LOW-FREQUENCY ACOUSTIC CENTER BODY
- Publication number 20250003374
- Publication date Jan 2, 2025
- Rohr, Inc.
- Jose S. Alonso-Miralles
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE WITH THIRD STREAM
- Publication number 20250003375
- Publication date Jan 2, 2025
- GENERAL ELECTRIC COMPANY
- Joseph George Rose
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
LOW NOISE TURBINE FOR GEARED TURBOFAN ENGINE
- Publication number 20250003426
- Publication date Jan 2, 2025
- RTX Corporation
- Bruce L. Morin
- G06 - COMPUTING CALCULATING COUNTING

JET-PROPULSION PLANTS

Industry

Parent Industries

Current Industry

Sub Industries

Patents Grantslast 30 patents

Engine backbone bending reduction

Integral propulsion and auxiliary power generation system for rocke...

Cascade element for a thrust reverser system of an engine

Propulsion apparatus, flying body and propulsion method

Thrust reverser having three gates

Propulsion systems and vehicles using the same

Thrust reverser provided with a lightweight thrust reverser flap

Rocket engine with dual contour nozzle

Aircraft assembly fitted with at least one hydrogen-powered thrust...

Composite fan case containment hook and improved forward debris cap...

Gas turbine engine with forward swept outlet guide vanes

Transpiration-cooled systems having permeable and non-permeable por...

Hot-gas-generating apparatus with ionic monopropellant and low volt...

Engine exhaust reverse flow prevention

Midshaft rating for turbomachine engines

Air conditioning system equipped with a system for the thermal mana...

Jam detection and jam tolerant motion control

Aircraft power plant with detonation combustion tube

Symmetric cascade thrust reversers and related methods

Turbomachine turbine assembly

Multimode propulsion system

Rocket engine injector

Trailing edge fuel injection enhancement for flame holding mitigation

Thermal management system for a gas turbine engine

Dual-mode ramjet engine with variable fuel injection

Guide systems for installing aircraft structures

Gas turbine engine bearing and gearbox arrangement

Device for attaching a connecting rod small end for a thrust revers...

Zero emission supersonic fan engine

Levered counterweight feathering system

Patents Applicationslast 30 patents

METHOD OF ASSEMBLY FOR GAS TURBINE FAN DRIVE GEAR SYSTEM

INLETS FOR GAS TURBINE ENGINE BYPASS DUCT HEAT EXCHANGERS

METHOD FOR COMBUSTING OF HYBRID ROCKET FUEL AND DEVICE FOR COMBUSTING

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

LOCKING ASSEMBLY FOR AN AIRCRAFT PROPULSION SYSTEM THRUST REVERSER

TRANSPIRATION-COOLED SYSTEMS HAVING PERMEABLE AND NON-PERMEABLE POR...

RESIN FORMULATIONS AND RELATED ARTICLES AND METHODS

GEARED GAS TURBINE ENGINE

ASSEMBLY FOR AN EXHAUST CONE OF AN AIRCRAFT TURBOMACHINE

TURBINE ENGINE CORE AND BYPASS FLOWS

SOLID ADHESIVE FILM FOR ACOUSTIC LINER AND METHOD

SOLID-PROPELLANT THRUSTER WITH AN INTEGRATED CONTROL MEANS AND SYST...

ACTUATION MECHANISM

HYBRID ROCKET ENGINE FUEL GRAINS WITH COMPOSITIONAL VARIATIONS

HIGH-POWER HYBRID-ELECTRIC PROPULSION SYSTEMS AND METHODS

TRIPLE-FLOW AXIAL TURBOMACHINE COMPRISING A DIVERGING HEAT EXCHANGE...

Vertical Take-Off and Landing Aircraft

REUSABLE UPPER STAGE ROCKET WITH AEROSPIKE ENGINE

FLUID CONTROL VALVE

TRIPLE-FLOW AXIAL TURBOMACHINE COMPRISING A DIVERGING HEAT EXCHANGE...

GAS TURBINE ENGINES COMPRISING PITCHED NOSE SPLITTER STRUCTURES AND...

INDUCER ASSEMBLY FOR A TURBINE ENGINE

THRUST VECTOR CONTROL FOR HYBRID PROPELLANTS ROCKET ENGINE WITH EMB...

GAS TURBINE ENGINE WITH THIRD STREAM

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

PROPULSION DEVICE WITH THRUST REVERSER LOCATING ARRANGEMENT

FAN APPARATUS WITH LIFT FAN AND LOUVERED COVER

LOW-FREQUENCY ACOUSTIC CENTER BODY

GAS TURBINE ENGINE WITH THIRD STREAM

LOW NOISE TURBINE FOR GEARED TURBOFAN ENGINE