Kioumars Najmabadi

Person

Clyde Hill, WA, US

People

Patents Grantslast 30 patents

Information Patent Grant
Sensor fault detection and identification using residual failure pa...
- Patent number 11,385,632
- Issue date Jul 12, 2022
- The Boeing Company
- Brian T. Whitehead
- G01 - MEASURING TESTING
Information Patent Grant
Systems and methods for pitch axis envelope limiting of an aircraft
- Patent number 11,194,345
- Issue date Dec 7, 2021
- The Boeing Company
- Tristan C. Flanzer
- G05 - CONTROLLING REGULATING
Information Patent Grant
Flight control system for determining estimated dynamic pressure ba...
- Patent number 11,066,189
- Issue date Jul 20, 2021
- The Boeing Company
- Sherwin Chunshek Li
- G05 - CONTROLLING REGULATING
Information Patent Grant
Flight control system for determining a fault based on error betwee...
- Patent number 11,029,706
- Issue date Jun 8, 2021
- The Boeing Company
- Sherwin Chunshek Li
- G05 - CONTROLLING REGULATING
Information Patent Grant
Flight control system for determining a common mode pneumatic fault
- Patent number 11,003,196
- Issue date May 11, 2021
- The Boeing Company
- Sherwin Chunshek Li
- G05 - CONTROLLING REGULATING
Information Patent Grant
Methods and systems for controlling aircraft flight performance
- Patent number 10,793,260
- Issue date Oct 6, 2020
- The Boeing Company
- Paul C. Strefling
- G07 - CHECKING-DEVICES
Information Patent Grant
Gust compensation system and method for aircraft
- Patent number 9,639,089
- Issue date May 2, 2017
- The Boeing Company
- Khaled Abdel-Motagaly
- G05 - CONTROLLING REGULATING
Information Patent Grant
Vertical gust suppression system for transport aircraft
- Patent number 8,774,987
- Issue date Jul 8, 2014
- The Boeing Company
- Vincent M. Walton
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Horizontal tail load alleviation system
- Patent number 8,752,789
- Issue date Jun 17, 2014
- The Boeing Company
- Chuong B. Tran
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Horizontal tail load alleviation system
- Patent number 8,342,445
- Issue date Jan 1, 2013
- The Boeing Company
- Chuong B. Tran
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Wing-body load alleviation for aircraft
- Patent number 8,024,079
- Issue date Sep 20, 2011
- The Boeing Company
- Kioumars Najmabadi
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft multi-axis modal suppression system
- Patent number 7,191,985
- Issue date Mar 20, 2007
- The Boeing Company
- Kioumars Najmabadi
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft multi-axis modal suppression system
- Patent number 6,915,989
- Issue date Jul 12, 2005
- The Boeing Company
- Kioumars Najmabadi
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft pitch-axis stability and command augmentation system
- Patent number 6,325,333
- Issue date Dec 4, 2001
- The Boeing Company
- Kioumars Najmabadi
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Method of speed protection and flare compensation for use with airc...
- Patent number 6,158,695
- Issue date Dec 12, 2000
- The Boeing Company
- Kioumars Najmabadi
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft pitch-axis stability and command augmentation system
- Patent number 5,979,835
- Issue date Nov 9, 1999
- The Boeing Company
- Kioumars Najmabadi
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
System for providing an air/ground signal to aircraft flight contro...
- Patent number 5,826,833
- Issue date Oct 27, 1998
- The Boeing Company
- Monte R. Evans
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft pitch-axis stability and command augmentation
- Patent number 5,722,620
- Issue date Mar 3, 1998
- The Boeing Company
- Kioumars Najmabadi
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Method and apparatus for automatically trimming an airplane stabilizer
- Patent number 5,692,708
- Issue date Dec 2, 1997
- The Boeing Company
- Edward E. Coleman
- G05 - CONTROLLING REGULATING

Patents Applicationslast 30 patents

Information Patent Application
Systems and Methods for Pitch Axis Envelope Limiting of an Aircraft
- Publication number 20210072769
- Publication date Mar 11, 2021
- The Boeing Company
- Tristan C. Flanzer
- G05 - CONTROLLING REGULATING
Information Patent Application
SENSOR FAULT DETECTION AND IDENTIFICATION USING RESIDUAL FAILURE PA...
- Publication number 20200201312
- Publication date Jun 25, 2020
- The Boeing Company
- Brian T. Whitehead
- G05 - CONTROLLING REGULATING
Information Patent Application
FLIGHT CONTROL SYSTEM FOR DETERMINING A FAULT BASED ON ERROR BETWEE...
- Publication number 20200183424
- Publication date Jun 11, 2020
- The Boeing Company
- Sherwin Chunshek Li
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
FLIGHT CONTROL SYSTEM FOR DETERMINING A COMMON MODE PNEUMATIC FAULT
- Publication number 20200183423
- Publication date Jun 11, 2020
- The Boeing Company
- Sherwin Chunshek Li
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
FLIGHT CONTROL SYSTEM FOR DETERMINING ESTIMATED DYNAMIC PRESSURE BA...
- Publication number 20200180789
- Publication date Jun 11, 2020
- The Boeing Company
- Sherwin Chunshek Li
- G01 - MEASURING TESTING
Information Patent Application
GUST COMPENSATION SYSTEM AND METHOD FOR AIRCRAFT
- Publication number 20160357191
- Publication date Dec 8, 2016
- The Boeing Company
- Khaled Abdel-Motagaly
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Horizontal Tail Load Alleviation System
- Publication number 20140067168
- Publication date Mar 6, 2014
- The Boeing Company
- Chuong B. Tran
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
HORIZONTAL TAIL LOAD ALLEVIATION SYSTEM
- Publication number 20100078518
- Publication date Apr 1, 2010
- Chuong B. Tran
- G05 - CONTROLLING REGULATING
Information Patent Application
WING-BODY LOAD ALLEVIATION FOR AIRCRAFT
- Publication number 20090292405
- Publication date Nov 26, 2009
- Kioumars Najmabadi
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Vertical Gust Suppression System for Transport Aircraft
- Publication number 20090157239
- Publication date Jun 18, 2009
- The Boeing Company
- Vincent M. Walton
- G05 - CONTROLLING REGULATING
Information Patent Application
AIRCRAFT MULTI-AXIS MODAL SUPPRESSION SYSTEM
- Publication number 20060237594
- Publication date Oct 26, 2006
- Kioumars Najmabadi
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Aircraft multi-axis modal suppression system
- Publication number 20030205644
- Publication date Nov 6, 2003
- Kioumars Najmabadi
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Kioumars Najmabadi

Person

Patents Grantslast 30 patents

Sensor fault detection and identification using residual failure pa...

Systems and methods for pitch axis envelope limiting of an aircraft

Flight control system for determining estimated dynamic pressure ba...

Flight control system for determining a fault based on error betwee...

Flight control system for determining a common mode pneumatic fault

Methods and systems for controlling aircraft flight performance

Gust compensation system and method for aircraft

Vertical gust suppression system for transport aircraft

Horizontal tail load alleviation system

Horizontal tail load alleviation system

Wing-body load alleviation for aircraft

Aircraft multi-axis modal suppression system

Aircraft multi-axis modal suppression system

Aircraft pitch-axis stability and command augmentation system

Method of speed protection and flare compensation for use with airc...

Aircraft pitch-axis stability and command augmentation system

System for providing an air/ground signal to aircraft flight contro...

Aircraft pitch-axis stability and command augmentation

Method and apparatus for automatically trimming an airplane stabilizer

Patents Applicationslast 30 patents

Systems and Methods for Pitch Axis Envelope Limiting of an Aircraft

SENSOR FAULT DETECTION AND IDENTIFICATION USING RESIDUAL FAILURE PA...

FLIGHT CONTROL SYSTEM FOR DETERMINING A FAULT BASED ON ERROR BETWEE...

FLIGHT CONTROL SYSTEM FOR DETERMINING A COMMON MODE PNEUMATIC FAULT

FLIGHT CONTROL SYSTEM FOR DETERMINING ESTIMATED DYNAMIC PRESSURE BA...

GUST COMPENSATION SYSTEM AND METHOD FOR AIRCRAFT

Horizontal Tail Load Alleviation System

HORIZONTAL TAIL LOAD ALLEVIATION SYSTEM

WING-BODY LOAD ALLEVIATION FOR AIRCRAFT

Vertical Gust Suppression System for Transport Aircraft

AIRCRAFT MULTI-AXIS MODAL SUPPRESSION SYSTEM

Aircraft multi-axis modal suppression system