Michael L. Sangwin

Person

Kirkland, WA, US

People

Patents Grantslast 30 patents

Information Patent Grant
Thrust-reverser assemblies that utilize active flow-control and sys...
- Patent number 9,371,799
- Issue date Jun 21, 2016
- The Boeing Company
- Nathan Owen Packard
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Cable-actuated variable area fan nozzle with elastomeric seals
- Patent number 9,021,813
- Issue date May 5, 2015
- The Boeing Company
- Christopher Jasklowski
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft systems including cascade thrust reversers
- Patent number 7,690,190
- Issue date Apr 6, 2010
- The Boeing Company
- Russel L. Thornock
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Hybrid exhaust heat shield for pylon mounted gas turbine engines
- Patent number 6,983,912
- Issue date Jan 10, 2006
- The Boeing Company
- Thomas J. Connelly
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Method and apparatus for controlling aircraft inlet air flow
- Patent number 6,634,595
- Issue date Oct 21, 2003
- The Boeing Company
- Joseph L. Koncsek
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Flow control device to eliminate cavity resonance
- Patent number 6,050,527
- Issue date Apr 18, 2000
- The Boeing Company
- Leonard J. Hebert
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Biplanar scarfed nacelle inlet
- Patent number 5,915,403
- Issue date Jun 29, 1999
- The Boeing Company
- James M. McConachie
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Engine flow control device
- Patent number 5,906,097
- Issue date May 25, 1999
- The Boeing Company
- Leonard J. Hebert
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Flow control apparatus for gas turbine engine installation pressure...
- Patent number 5,623,820
- Issue date Apr 29, 1997
- The Boeing Company
- Ronald L. Balzer
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
THRUST-REVERSER ASSEMBLIES THAT UTILIZE ACTIVE FLOW-CONTROL AND SYS...
- Publication number 20150308377
- Publication date Oct 29, 2015
- THE BOEING COMPANY
- Nathan Owen Packard
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Cable-Actuated Variable Area Fan Nozzle with Elastomeric Seals
- Publication number 20130020408
- Publication date Jan 24, 2013
- The Boeing Company
- Christopher Jasklowski
- B25 - HAND TOOLS PORTABLE POWER-DRIVEN TOOLS MANIPULATORS
Information Patent Application
Aircraft systems including cascade thrust reversers
- Publication number 20060277895
- Publication date Dec 14, 2006
- Russel L. Thornock
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Hybrid exhaust heat shield for pylon mounted gas turbine engines
- Publication number 20030201366
- Publication date Oct 30, 2003
- Thomas J. Connelly
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
METHOD AND APPARATUS FOR CONTROLLING AIRCRAFT INLET AIR FLOW
- Publication number 20030132342
- Publication date Jul 17, 2003
- Joseph L. Koncsek
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Michael L. Sangwin

Person

Patents Grantslast 30 patents

Thrust-reverser assemblies that utilize active flow-control and sys...

Cable-actuated variable area fan nozzle with elastomeric seals

Aircraft systems including cascade thrust reversers

Hybrid exhaust heat shield for pylon mounted gas turbine engines

Method and apparatus for controlling aircraft inlet air flow

Flow control device to eliminate cavity resonance

Biplanar scarfed nacelle inlet

Engine flow control device

Flow control apparatus for gas turbine engine installation pressure...

Patents Applicationslast 30 patents

THRUST-REVERSER ASSEMBLIES THAT UTILIZE ACTIVE FLOW-CONTROL AND SYS...

Cable-Actuated Variable Area Fan Nozzle with Elastomeric Seals

Aircraft systems including cascade thrust reversers

Hybrid exhaust heat shield for pylon mounted gas turbine engines

METHOD AND APPARATUS FOR CONTROLLING AIRCRAFT INLET AIR FLOW