Membership
Tour
Register
Log in
Plants characterised by the form or arrangement of the jet pipe or nozzle Jet pipes or nozzles peculiar thereto
Follow
Industry
CPC
F02K1/00
This industry / category may be too specific. Please go to a parent level for more data
Parent Industries
F
MECHANICAL ENGINEERING LIGHTING HEATING WEAPONS BLASTING ENGINES OR PUMPS
F02
Combustion engines
F02K
JET-PROPULSION PLANTS
Current Industry
F02K1/00
Plants characterised by the form or arrangement of the jet pipe or nozzle Jet pipes or nozzles peculiar thereto
Sub Industries
F02K1/002
with means to modify the direction of thrust vector
F02K1/004
by using one or more swivable nozzles rotating about their own axis
F02K1/006
within one plane only
F02K1/008
in any rearward direction
F02K1/04
Mounting of an exhaust cone in the jet pipe
F02K1/06
Varying effective area of jet pipe or nozzle
F02K1/08
by axially moving or transversely deforming an internal member
F02K1/085
by transversely deforming an internal member
F02K1/09
by axially moving an external member
F02K1/10
by distorting the jet pipe or nozzle
F02K1/11
by means of pivoted eyelids
F02K1/12
by means of pivoted flaps
F02K1/1207
of one series of flaps hinged at their upstream ends on a fixed structure
F02K1/1215
of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure, and the downstream series having its flaps hinged at their downstream ends on a fixed structure
F02K1/1223
of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the downstream series having its flaps hinged at their upstream ends on the downstream ends of the flaps of the upstream series
F02K1/123
of two series of flaps, both having their flaps hinged at their upstream ends on a fixed structure
F02K1/1238
of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the downstream series having its flaps hinged at their upstream ends on a substantially axially movable structure
F02K1/1246
of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the downstream series having its flaps hinged at their downstream ends on a substantially axially movable structure
F02K1/1253
of one series of flaps hinged at their upstream ends on a fixed structure and of a substantially axially movable external member
F02K1/1261
of one series of flaps hinged at their upstream ends on a substantially axially movable structure
F02K1/1269
of three series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the internal downstream series having its flaps hinged at their downstream ends on the downstream ends of the flaps of the external downstream series hinged on a fixed structure at their upstream ends
F02K1/1276
of three series of flaps, the upstream series having its flaps hinged at their upstream ends on a substantially axially movable structure and the downstream or external series having its flaps hinged at their upstream ends on a fixed structure
F02K1/1284
of three series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the internal downstream series having its flaps hinged at their downstream ends on the downstream ends of the flaps of the external downstream series hinged at their upstream ends on a substantially axially movable structure
F02K1/1292
of three series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure, the internal downstream series having its flaps hinged at their upstream ends on the downstream ends of the flaps of the upstream series and at their downstream ends on the downstream ends of the flaps of the external downstream series hinged at their upstream ends on a substantial...
F02K1/15
Control or regulation
F02K1/16
conjointly with another control
F02K1/165
with air intake control
F02K1/17
with control of fuel supply
F02K1/18
automatic
F02K1/28
using fluid jets to influence the jet flow
F02K1/30
for varying effective area of jet pipe or nozzle
F02K1/32
for reversing thrust
F02K1/34
for attenuating noise
F02K1/36
having an ejector
F02K1/38
Introducing air inside the jet
F02K1/383
with retractable elements
F02K1/386
mixing devices in the jet pipe
F02K1/40
Nozzles having means for dividing the jet into a plurality of partial jets or having an elongated cross-section outlet
F02K1/42
the means being movable into an inoperative position
F02K1/44
Nozzles having means
F02K1/46
Nozzles having means for adding air to the jet or for augmenting the mixing region between the jet and the ambient air
F02K1/48
Corrugated nozzles
F02K1/50
Deflecting outwardly a portion of the jet by retractable scoop-like baffles
F02K1/52
Nozzles specially constructed for positioning adjacent to another nozzle or to a fixed member
F02K1/54
Nozzles having means for reversing jet thrust
F02K1/56
Reversing jet main flow
F02K1/563
in specified direction
F02K1/566
by blocking the rearward discharge by means of a translatable member
F02K1/58
Reversers mounted on the inner cone or the nozzle housing or the fuselage
F02K1/60
by blocking the rearward discharge by means of pivoted eyelids or clamshells
F02K1/605
the aft end of the engine cowling being movable to uncover openings for the reversed flow
F02K1/62
by blocking the rearward discharge by means of flaps
F02K1/625
the aft end of the engine cowling being movable to uncover openings for the reversed flow
F02K1/64
Reversing fan flow
F02K1/645
using inflatable diaphragms
F02K1/66
using reversing fan blades
F02K1/68
Reversers mounted on the engine housing downstream of the fan exhaust section
F02K1/70
using thrust reverser flaps or doors mounted on the fan housing
F02K1/72
the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
F02K1/74
Reversing at least one flow in relation to at least one other flow in a plural- flow engine
F02K1/76
Control or regulation of thrust reversers
F02K1/763
with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
F02K1/766
with blocking systems or locking devices; Arrangement of locking devices for thrust reversers
F02K1/78
Other construction of jet pipes
F02K1/80
Couplings or connections
F02K1/805
Sealing devices therefor
F02K1/82
Jet pipe walls
F02K1/822
Heat insulating structures or liners, cooling arrangements
F02K1/825
Infra-red radiation suppressors
F02K1/827
Sound absorbing structures or liners
Industries
Overview
Organizations
People
Information
Impact
Please log in for detailed analytics
Patents Grants
last 30 patents
Information
Patent Grant
Vectoring exhaust nozzle for an aircraft powerplant
Patent number
12,320,313
Issue date
Jun 3, 2025
RTX Corporation
Michael Murphy
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Grant
Unducted single rotor engine and method for operation
Patent number
12,320,315
Issue date
Jun 3, 2025
General Electric Company
Syed Arif Khalid
F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information
Patent Grant
Pressure measurement bar improving the monitoring of unsteady aerod...
Patent number
12,320,317
Issue date
Jun 3, 2025
Airbus Operations SAS
Nicolas Dupe
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Grant
Air inlet of a nacelle of an aircraft propulsion assembly for promo...
Patent number
12,320,314
Issue date
Jun 3, 2025
SAFRAN AIRCRAFT ENGINES
Yacine Cheraga
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Grant
Thrust reverser cascade including acoustic treatment
Patent number
12,320,316
Issue date
Jun 3, 2025
SAFRAN AIRCRAFT ENGINES
Norman Bruno André Jodet
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Grant
Coupling assembly for a turbine engine
Patent number
12,313,264
Issue date
May 27, 2025
General Electric Company
Ravindra Shankar Ganiger
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Grant
Method for creating alveolar cores having open inner conical shapes
Patent number
12,315,486
Issue date
May 27, 2025
SAFRAN NACELLES
Bertrand Desjoyeaux
B29 - WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
Information
Patent Grant
Method for manufacturing a structure with cellular cores for a turb...
Patent number
12,305,592
Issue date
May 20, 2025
SAFRAN NACELLES
Bertrand Léon Marie Desjoyeaux
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Grant
Seal system using layers of seal segments forced into sealing engag...
Patent number
12,305,526
Issue date
May 20, 2025
GE INFRASTRUCTURE TECHNOLOGY LLC
Karol Filip LeszczyĆski
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Grant
Aircraft propulsive assembly comprising a nacelle with a t-shaped f...
Patent number
12,296,975
Issue date
May 13, 2025
Airbus Operations SAS
Lionel Czapla
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Grant
Cowl seal assembly for an aircraft propulsion system
Patent number
12,296,970
Issue date
May 13, 2025
Rohr, Inc.
Pratap Mallampati
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Grant
Additive manufacturing process of a part for an aircraft propulsion...
Patent number
12,297,791
Issue date
May 13, 2025
SAFRAN NACELLES
Flavie Hubert-Choinard
B22 - CASTING POWDER METALLURGY
Information
Patent Grant
Aircraft nacelle equipped with at least one thrust reversal device...
Patent number
12,292,015
Issue date
May 6, 2025
Airbus Operations SAS
Frédéric Chelin
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Grant
Gas turbine engine exhaust chevrons
Patent number
12,292,014
Issue date
May 6, 2025
Rohr, Inc.
Johann Steven Schrell
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Grant
Pressure measuring rake comprising a patched leading edge, in parti...
Patent number
12,292,349
Issue date
May 6, 2025
Airbus S.A.S.
Nicolas Dupe
F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information
Patent Grant
Bypass turbomachine for an aircraft
Patent number
12,291,978
Issue date
May 6, 2025
SAFRAN AIRCRAFT ENGINES
Eva Julie Lebeault
F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information
Patent Grant
Axial expandable exhaust duct
Patent number
12,292,016
Issue date
May 6, 2025
RTX Corporation
Lawrence A. Binek
B33 - ADDITIVE MANUFACTURING TECHNOLOGY
Information
Patent Grant
Reverse thrust turbofan engine
Patent number
12,286,941
Issue date
Apr 29, 2025
General Electric Company
Trevor Howard Wood
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Grant
Exhaust nozzle assembly, propulsion system employing the exhaust no...
Patent number
12,280,888
Issue date
Apr 22, 2025
Gulfstream Aerospace Corporation
Donald Freund
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Grant
Pressure drag jet engine
Patent number
12,276,237
Issue date
Apr 15, 2025
Isaac Erik Anderson
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Grant
Multiple turn reverser with side turning vanes
Patent number
12,276,238
Issue date
Apr 15, 2025
The Boeing Company
Chen Chuck
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Grant
Method and system for controlling a thrust reverser of an aircraft
Patent number
12,270,357
Issue date
Apr 8, 2025
SAFRAN AIRCRAFT ENGINES
Irène Bujon
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Grant
Thrust reverser cascade with one or more flow disrupters
Patent number
12,270,356
Issue date
Apr 8, 2025
Rohr, Inc.
Julian Winkler
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Grant
Locking assembly for an aircraft propulsion system thrust reverser
Patent number
12,270,358
Issue date
Apr 8, 2025
Rohr, Inc.
Timothy Gormley
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Grant
Nozzle assembly for use with a propulsion system
Patent number
12,264,638
Issue date
Apr 1, 2025
Gulfstream Aerospace Corporation
Derek Muzychka
G06 - COMPUTING CALCULATING COUNTING
Information
Patent Grant
Propulsion system with downstream section having deformable shape-m...
Patent number
12,264,637
Issue date
Apr 1, 2025
SAFRAN
Jean-Louis Robert Guy Besse
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Grant
Thrust reverser with door of a nacelle of a turbojet engine of an a...
Patent number
12,258,924
Issue date
Mar 25, 2025
SAFRAN NACELLES
Jean-Philippe Joret
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Grant
Thrust reverser comprising pivoting half-assemblies and a connectin...
Patent number
12,258,925
Issue date
Mar 25, 2025
SAFRAN NACELLES
Patrick André Boileau
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Grant
Airfoil for a turbofan engine
Patent number
12,258,875
Issue date
Mar 25, 2025
General Electric Company
Trevor Howard Wood
G10 - MUSICAL INSTRUMENTS ACOUSTICS
Information
Patent Grant
Cowl assembly for a propulsor
Patent number
12,258,923
Issue date
Mar 25, 2025
General Electric Company
Thomas Malkus
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Patents Applications
last 30 patents
Information
Patent Application
PROPULSION SYSTEMS AND VEHICLES USING THE SAME
Publication number
20250179973
Publication date
Jun 5, 2025
Morteza Vadipour
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Application
PROPULSION ASSEMBLY FOR AN AIRCRAFT COMPRISING A THRUST REVERSER WI...
Publication number
20250137418
Publication date
May 1, 2025
SAFRAN NACELLES
Patrick André BOILEAU
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Application
ACOUSTIC PANEL HAVING OBLIQUE CAVITIES
Publication number
20250122840
Publication date
Apr 17, 2025
SAFRAN NACELLES
Marc VERSAEVEL
B32 - LAYERED PRODUCTS
Information
Patent Application
TURBOMACHINE COMPRISING AN OUTLET CONE INCORPORATING COMPONENTS COO...
Publication number
20250122812
Publication date
Apr 17, 2025
SAFRAN AIRCRAFT ENGINES
Adrien Pierre Jean PERTAT
F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information
Patent Application
PLUG NOZZLE AND THRUST REVERSER FOR HIGH MACH GAS TURBINE ENGINES
Publication number
20250122847
Publication date
Apr 17, 2025
Rolls-Royce North American Technologies Inc.
Kenneth M. PESYNA
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Application
GEARBOX ASSEMBLY WITH LUBRICANT EXTRACTION VOLUME RATIO
Publication number
20250122848
Publication date
Apr 17, 2025
GENERAL ELECTRIC COMPANY
Bugra H. Ertas
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Application
THRUST REVERSER COMPRISING MOVABLE CASCADES AND A SEALING MEMBRANE
Publication number
20250109723
Publication date
Apr 3, 2025
SAFRAN NACELLES
Gina FERRIER
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Application
METHOD FOR BRAKING AN AIRCRAFT TURBINE ENGINE
Publication number
20250101930
Publication date
Mar 27, 2025
SAFRAN AIRCRAFT ENGINES
Jacques Auriol
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Application
THRUST REVERSER COMPRISING FIXED CASCADES AND A SEALING MEMBRANE
Publication number
20250101931
Publication date
Mar 27, 2025
SAFRAN NACELLES
Patrick GONIDEC
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Application
COMPACT INFRARED SUPPRESSORS WITH RING VANES FOR GAS TURBINE ENGINES
Publication number
20250101932
Publication date
Mar 27, 2025
Rolls-Royce North American Technologies Inc.
Curtlan C. Betchley
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Application
AIRCRAFT NACELLE PROVIDED WITH AT LEAST ONE THRUST REVERSAL DEVICE...
Publication number
20250092847
Publication date
Mar 20, 2025
Airbus Operations SAS
Frédéric CHELIN
B64 - AIRCRAFT AVIATION COSMONAUTICS
Information
Patent Application
EXTERNAL POWER CONTROL MODULE FOR AND METHOD TO OPEN COWLING OF AN...
Publication number
20250066029
Publication date
Feb 27, 2025
AIRBUS OPERATIONS (SAS)
Pablo REVERT
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Application
Movable-cascade thrust reverser comprising a multi-functional fixed...
Publication number
20250067231
Publication date
Feb 27, 2025
SAFRAN NACELLES
Patrick André Boileau
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Application
Exhaust Area and Flow Turning Control
Publication number
20250066015
Publication date
Feb 27, 2025
Whisper Aero Inc.
Mark Douglass Moore
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Application
ENGINE MOUNT SYSTEM FOR A GAS TURBINE ENGINE
Publication number
20250058887
Publication date
Feb 20, 2025
RTX Corporation
Gabriel L. Suciu
F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information
Patent Application
Plug Nozzle and Thrust Reverser for High Mach Gas Turbine Engines
Publication number
20250059931
Publication date
Feb 20, 2025
Rolls-Royce North American Technologies Inc.
Kenneth M. PESYNA
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Application
Thrust Reverser Actuation System Lock Tester
Publication number
20250060280
Publication date
Feb 20, 2025
WOODWARD, INC.
Jiahua Lu
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Application
MIXED FLOW EXHAUST THRUST REVERSER WITH AREA CONTROL NOZZLE SYSTEMS...
Publication number
20250052210
Publication date
Feb 13, 2025
Rohr, Inc.
JOHANN STEVEN SCHRELL
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
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
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
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
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
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
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
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
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
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
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
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