for supercritical or transonic flow

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CPC
B64C2003/149

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BPERFORMING OPERATIONS TRANSPORTING B64Aviation B64CAEROPLANES HELICOPTERS

Current Industry

B64C2003/149for supercritical or transonic flow

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Patents Grantslast 30 patents

Information Patent Grant
Structural arrangement and method for counteracting a vertical mome...
- Patent number 11,787,524
- Issue date Oct 17, 2023
- The Boeing Company
- Robert E. Grip
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft portion with reduced wave drag
- Patent number 11,745,849
- Issue date Sep 5, 2023
- Dassault Aviation
- Aurélien Merlet
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft portion with reduced wave drag
- Patent number 11,267,552
- Issue date Mar 8, 2022
- Dassault Aviation
- Aurélien Merlet
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Wing, aircraft, and method for delaying wing stall of an aircraft
- Patent number 11,214,351
- Issue date Jan 4, 2022
- The Boeing Company
- Robert Hoffenberg
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Wing and aircraft
- Patent number 10,988,233
- Issue date Apr 27, 2021
- Japan Aerospace Exploration Agency
- Yoshine Ueda
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft with strut-braced wing system
- Patent number 10,933,970
- Issue date Mar 2, 2021
- The Boeing Company
- Neal A. Harrison
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Methods and apparatus to monitor a shock wave proximate a transonic...
- Patent number 10,472,060
- Issue date Nov 12, 2019
- The Boeing Company
- Steve G. Mackin
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft wing roughness strip and method
- Patent number 10,384,766
- Issue date Aug 20, 2019
- Airbus Operations Limited
- Stephen Rolston
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aerodynamic structure with asymmetrical shock bump
- Patent number 9,896,193
- Issue date Feb 20, 2018
- Airbus Operations Limited
- Norman Wood
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aerodynamic structure with series of shock bumps
- Patent number 9,463,870
- Issue date Oct 11, 2016
- Airbus Operations Limited
- Norman Wood
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aerodynamic structure with non-uniformly spaced shock bumps
- Patent number 9,334,045
- Issue date May 10, 2016
- Airbus Operations Limited
- Norman Wood
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Highly efficient supersonic laminar flow wing structure
- Patent number 9,233,755
- Issue date Jan 12, 2016
- Aerion Corporation
- James D. Chase
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Method for designing a natural laminar flow wing of a supersonic ai...
- Patent number 9,031,817
- Issue date May 12, 2015
- Japan Aerospace Exploration Agency
- Kenji Yoshida
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Shock bump
- Patent number 8,302,912
- Issue date Nov 6, 2012
- Airbus Operations Limited
- Norman Wood
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft configured for flight in an atmosphere having low density
- Patent number 8,196,858
- Issue date Jun 12, 2012
- The United States of America as represented by the administrator of the Natio...
- Mark A. Croom
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Methods and systems for controlling lower surface shocks
- Patent number 7,118,071
- Issue date Oct 10, 2006
- The Boeing Company
- David R. Bogue
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Laminar-flow airfoil
- Patent number 7,093,792
- Issue date Aug 22, 2006
- Honda Giken Kogyo Kabushiki Kaisha
- Michimasa Fujino
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Slotted aircraft wing
- Patent number 7,048,228
- Issue date May 23, 2006
- The Boeing Company
- John C. Vassberg
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Slotted aircraft wing
- Patent number 7,048,235
- Issue date May 23, 2006
- The Boeing Company
- James D. McLean
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Main wing structure
- Patent number 6,834,830
- Issue date Dec 28, 2004
- Honda Giken Kogyo Kabushiki Kaisha
- Michimasa Fujino
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Airfoil trailing edge
- Patent number 6,651,927
- Issue date Nov 25, 2003
- QinetiQ Limited
- Kevin C Hackett
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Wing airfoil
- Patent number 6,607,164
- Issue date Aug 19, 2003
- Toyota Motor Sales, U.S.A., Inc.
- Dan M. Somers
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Airplane with unswept slotted cruise wing airfoil
- Patent number 6,293,497
- Issue date Sep 25, 2001
- The Boeing Company
- Robert H. Kelley-Wickemeyer
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Divergent trailing-edge airfoil
- Patent number 4,858,852
- Issue date Aug 22, 1989
- McDonnell Douglas Corporation
- Preston A. Henne
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Manoeuverable supercritical wing section
- Patent number 4,718,619
- Issue date Jan 12, 1988
- Ministry of Defence
- Patrick R. Ashill
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Wing-sections, in particular aircraft lift-wing sections
- Patent number 4,524,928
- Issue date Jun 25, 1985
- Dornier Gmbh
- Wolfgang Schmidt
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Wing for short take-off and landing aircraft
- Patent number 4,498,646
- Issue date Feb 12, 1985
- Dornier Gmbh
- Hans-Jorg Proksch
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Mono-element combined supercritical high lift airfoil
- Patent number 4,457,480
- Issue date Jul 3, 1984
- The United States of America as represented by the Secretary of the Navy
- Robert J. Englar
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Supercritical air-foil profile
- Patent number 4,455,003
- Issue date Jun 19, 1984
- VFW
- Reinhard Hilbig
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Airfoil shape for aircraft
- Patent number 4,413,796
- Issue date Nov 8, 1983
- Societe Nationale Industrielle et Aerospatiale
- Jean Bousquet
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
TRANSONIC AIRCRAFT WITH TENSION-BASED WING SUPPORT
- Publication number 20250002135
- Publication date Jan 2, 2025
- The Boeing Company
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Airfoil With Supersonic Wave-Tripping Structure
- Publication number 20230174231
- Publication date Jun 8, 2023
- Patrick O'LEARY
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
STRUCTURAL ARRANGEMENT AND METHOD FOR COUNTERACTING A VERTICAL MOME...
- Publication number 20230140102
- Publication date May 4, 2023
- The Boeing Company
- Robert E. Grip
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
FREE STREAMLINE AIRFOIL
- Publication number 20220161920
- Publication date May 26, 2022
- Brown University
- Matteo DI LUCA
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
AIRCRAFT PORTION WITH REDUCED WAVE DRAG
- Publication number 20220111947
- Publication date Apr 14, 2022
- Aurélien MERLET
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
WING, AIRCRAFT, AND METHOD FOR DELAYING WING STALL OF AN AIRCRAFT
- Publication number 20190367152
- Publication date Dec 5, 2019
- The Boeing Company
- Robert Hoffenberg
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
AIRCRAFT WITH STRUT-BRACED WING SYSTEM
- Publication number 20190300143
- Publication date Oct 3, 2019
- The Boeing Company
- Neal A. Harrison
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
WING AND AIRCRAFT
- Publication number 20190217941
- Publication date Jul 18, 2019
- JAPAN AEROSPACE EXPLORATION AGENCY
- Yoshine Ueda
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Aircraft With Integrated Lift And Propulsion System
- Publication number 20140061392
- Publication date Mar 6, 2014
- Abe Karem
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
METHOD OF DESIGNING NATURAL LAMINAR FLOW WING FOR REYNOLDS NUMBERS...
- Publication number 20120166148
- Publication date Jun 28, 2012
- JAPAN AEROSPACE EXPLORATION AGENCY
- Kenji Yoshida
- G06 - COMPUTING CALCULATING COUNTING
Information Patent Application
SHOCK BUMP
- Publication number 20100314500
- Publication date Dec 16, 2010
- Norman Wood
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
AERODYNAMIC STRUCTURE WITH NON-UNIFORMLY SPACED SHOCK BUMPS
- Publication number 20100308176
- Publication date Dec 9, 2010
- Norman Wood
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
AERODYNAMIC STRUCTURE WITH SERIES OF SHOCK BUMPS
- Publication number 20100301172
- Publication date Dec 2, 2010
- AIRBUS UK Limited
- Norman Wood
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Methods and systems for controlling lower surface shocks
- Publication number 20060060720
- Publication date Mar 23, 2006
- David R. Bogue
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Slotted aircraft wing
- Publication number 20050017126
- Publication date Jan 27, 2005
- James D. McLean
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Slotted aircraft wing
- Publication number 20040195464
- Publication date Oct 7, 2004
- John C. Vassberg
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Main wing structure
- Publication number 20030230670
- Publication date Dec 18, 2003
- Michimasa Fujino
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Trailing edge shape of laminar-flow airfoil
- Publication number 20030230669
- Publication date Dec 18, 2003
- Michimasa Fujino
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Wing airfoil
- Publication number 20030127561
- Publication date Jul 10, 2003
- TOYOTA MOTOR SALES U.S.A., INC
- Dan M. Somers
- B64 - AIRCRAFT AVIATION COSMONAUTICS

for supercritical or transonic flow

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Structural arrangement and method for counteracting a vertical mome...

Aircraft portion with reduced wave drag

Aircraft portion with reduced wave drag

Wing, aircraft, and method for delaying wing stall of an aircraft

Wing and aircraft

Aircraft with strut-braced wing system

Methods and apparatus to monitor a shock wave proximate a transonic...

Aircraft wing roughness strip and method

Aerodynamic structure with asymmetrical shock bump

Aerodynamic structure with series of shock bumps

Aerodynamic structure with non-uniformly spaced shock bumps

Highly efficient supersonic laminar flow wing structure

Method for designing a natural laminar flow wing of a supersonic ai...

Shock bump

Aircraft configured for flight in an atmosphere having low density

Methods and systems for controlling lower surface shocks

Laminar-flow airfoil

Slotted aircraft wing

Slotted aircraft wing

Main wing structure

Airfoil trailing edge

Wing airfoil

Airplane with unswept slotted cruise wing airfoil

Divergent trailing-edge airfoil

Manoeuverable supercritical wing section

Wing-sections, in particular aircraft lift-wing sections

Wing for short take-off and landing aircraft

Mono-element combined supercritical high lift airfoil

Supercritical air-foil profile

Airfoil shape for aircraft

Patents Applicationslast 30 patents

TRANSONIC AIRCRAFT WITH TENSION-BASED WING SUPPORT

Airfoil With Supersonic Wave-Tripping Structure

STRUCTURAL ARRANGEMENT AND METHOD FOR COUNTERACTING A VERTICAL MOME...

FREE STREAMLINE AIRFOIL

AIRCRAFT PORTION WITH REDUCED WAVE DRAG

WING, AIRCRAFT, AND METHOD FOR DELAYING WING STALL OF AN AIRCRAFT

AIRCRAFT WITH STRUT-BRACED WING SYSTEM

WING AND AIRCRAFT

Aircraft With Integrated Lift And Propulsion System

METHOD OF DESIGNING NATURAL LAMINAR FLOW WING FOR REYNOLDS NUMBERS...

SHOCK BUMP

AERODYNAMIC STRUCTURE WITH NON-UNIFORMLY SPACED SHOCK BUMPS

AERODYNAMIC STRUCTURE WITH SERIES OF SHOCK BUMPS

Methods and systems for controlling lower surface shocks

Slotted aircraft wing

Slotted aircraft wing

Main wing structure

Trailing edge shape of laminar-flow airfoil

Wing airfoil