Inventor · disambiguated record
Runyon H. Tindell
Also filed as: TINDELL RUNYON H
7 granted patents·366 citations·filing 1989–1998
89Inventor score
Top patents by PatentIndex Score
7 records- 0194US5447283ABlown boundary layer control system for a jet aircraftGRUMMAN AEROSPACE CORP·Filed 1994·Granted Sep 5, 1995·117 cites·14 claims
- 0288US5934611ALow drag inlet design using injected duct flowNORTHROP GRUMMAN CORP·Filed 1997·Granted Aug 10, 1999·88 cites·21 claims
- 0378US4979699AFlight control augmentation inlet deviceGRUMMAN AEROSPACE CORP·Filed 1989·Granted Dec 25, 1990·33 cites·20 claims
- 0473US6179251B1Thin inlet lip design for low drag and reduced nacelle sizeNORTHROP GRUMMAN CORP·Filed 1998·Granted Jan 30, 2001·52 cites·12 claims
- 0568US5904320ABlockerless thrust reverserNORTHROP GUNMAN CORP·Filed 1997·Granted May 18, 1999·36 cites·11 claims
- 0658US5485975ASlotted cowl inlet lip for introducing high pressure airNORTHROP GRUMMAN CORP·Filed 1994·Granted Jan 23, 1996·18 cites·5 claims
- 0755US5713537ABlockerless thrust reverserNORTHROP GRUMMAN CORP·Filed 1995·Granted Feb 3, 1998·22 cites·10 claims
Join the waitlist — get patent alerts
Get an alert when Runyon H. Tindell files or is granted a new patent.
We store only your email — no account needed. See our privacy policy.
Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →