Runyon H. Tindell

Person

Old Bethpage, NY, US

People

Patents Grantslast 30 patents

Information Patent Grant
Thin inlet lip design for low drag and reduced nacelle size
- Patent number 6,179,251
- Issue date Jan 30, 2001
- Northrop Grumman Corporation
- Runyon H. Tindell
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Low drag inlet design using injected duct flow
- Patent number 5,934,611
- Issue date Aug 10, 1999
- Northrop Grumman Corporation
- Runyon H. Tindell
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Blockerless thrust reverser
- Patent number 5,904,320
- Issue date May 18, 1999
- Northrop Gunman Corporation
- Runyon H. Tindell
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Blockerless thrust reverser
- Patent number 5,713,537
- Issue date Feb 3, 1998
- Northrop Grumman Corporation
- Runyon H. Tindell
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Slotted cowl inlet lip for introducing high pressure air
- Patent number 5,485,975
- Issue date Jan 23, 1996
- Northrop Grumman Corporation
- Runyon H. Tindell
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Blown boundary layer control system for a jet aircraft
- Patent number 5,447,283
- Issue date Sep 5, 1995
- Grumman Aerospace Corporation
- Runyon H. Tindell
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Flight control augmentation inlet device
- Patent number 4,979,699
- Issue date Dec 25, 1990
- Grumman Aerospace Corporation
- Runyon H. Tindell
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Runyon H. Tindell

Person

Patents Grantslast 30 patents

Thin inlet lip design for low drag and reduced nacelle size

Low drag inlet design using injected duct flow

Blockerless thrust reverser

Blockerless thrust reverser

Slotted cowl inlet lip for introducing high pressure air

Blown boundary layer control system for a jet aircraft

Flight control augmentation inlet device