Nicholas D. Lappos

Person

Madison, CT, US

People

Patents Grantslast 30 patents

Information Patent Grant
Helicopter integrated fire and flight control having a pre-launch a...
- Patent number 5,465,212
- Issue date Nov 7, 1995
- United Technologies Corporation
- Donald W. Fowler
- G05 - CONTROLLING REGULATING
Information Patent Grant
Helicopter integrated fire and flight control having azimuth and pi...
- Patent number 5,431,084
- Issue date Jul 11, 1995
- United Technologies Corporation
- Donald W. Fowler
- G05 - CONTROLLING REGULATING
Information Patent Grant
Integrated time/limit exceedance cue system
- Patent number 5,339,244
- Issue date Aug 16, 1994
- United Technologies Corporation
- Lorren Stiles
- G05 - CONTROLLING REGULATING
Information Patent Grant
Helicopter integrated fire and flight control having azimuth and pi...
- Patent number 5,331,881
- Issue date Jul 26, 1994
- United Technologies Corporation
- Donald W. Fowler
- G05 - CONTROLLING REGULATING
Information Patent Grant
Helicopter integrated fire and flight control having constraint lim...
- Patent number 5,310,136
- Issue date May 10, 1994
- United Technologies Corporation
- Donald W. Fowler
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Helicopter integrated fire and flight control having coordinated ar...
- Patent number 5,310,135
- Issue date May 10, 1994
- United Technologies Corporation
- Donald W. Fowler
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Helicopter integrated fire and flight control system having turn co...
- Patent number 5,263,662
- Issue date Nov 23, 1993
- United Technologies Corporation
- Donald W. Fowler
- G05 - CONTROLLING REGULATING
Information Patent Grant
Automatic turn coordination trim control for rotary wing aircraft
- Patent number 5,222,691
- Issue date Jun 29, 1993
- United Technologies Corporation
- Phillip J. Gold
- G05 - CONTROLLING REGULATING
Information Patent Grant
Range maximizing, stable, helicopter cruise fuel conservation
- Patent number 5,023,797
- Issue date Jun 11, 1991
- United Technologies Corporation
- Nicholas D. Lappos
- G05 - CONTROLLING REGULATING
Information Patent Grant
Helicopter control with multiple schedule rotor speed decay anticip...
- Patent number 5,020,316
- Issue date Jun 4, 1991
- Coltec Industries Inc.
- David H. Sweet
- G05 - CONTROLLING REGULATING
Information Patent Grant
Helicopter, high rotor load speed enhancement
- Patent number 4,998,202
- Issue date Mar 5, 1991
- United Technologies Corporation
- David M. Walsh
- G05 - CONTROLLING REGULATING
Information Patent Grant
Detection of engine failure in a multi-engine aircraft
- Patent number 4,817,046
- Issue date Mar 28, 1989
- United Technologies Corporation
- Robert W. Rice
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Collective stick force-check device
- Patent number 4,770,375
- Issue date Sep 13, 1988
- United Technologies Corporation
- Nicholas D. Lappos
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Helicopter power available to hover indicator
- Patent number 4,736,331
- Issue date Apr 5, 1988
- United Technologies Corporation
- Nicholas D. Lappos
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Super contingency aircraft engine control
- Patent number 4,500,966
- Issue date Feb 19, 1985
- Chandler Evans Inc.
- Raymond D. Zagranski
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Nicholas D. Lappos

Person

Patents Grantslast 30 patents

Helicopter integrated fire and flight control having a pre-launch a...

Helicopter integrated fire and flight control having azimuth and pi...

Integrated time/limit exceedance cue system

Helicopter integrated fire and flight control having azimuth and pi...

Helicopter integrated fire and flight control having constraint lim...

Helicopter integrated fire and flight control having coordinated ar...

Helicopter integrated fire and flight control system having turn co...

Automatic turn coordination trim control for rotary wing aircraft

Range maximizing, stable, helicopter cruise fuel conservation

Helicopter control with multiple schedule rotor speed decay anticip...

Helicopter, high rotor load speed enhancement

Detection of engine failure in a multi-engine aircraft

Collective stick force-check device

Helicopter power available to hover indicator

Super contingency aircraft engine control