WO2002006115A9 - Flight control modules merged into the integrated modular avionics - Google Patents
Flight control modules merged into the integrated modular avionicsInfo
- Publication number
- WO2002006115A9 WO2002006115A9 PCT/US2001/022063 US0122063W WO0206115A9 WO 2002006115 A9 WO2002006115 A9 WO 2002006115A9 US 0122063 W US0122063 W US 0122063W WO 0206115 A9 WO0206115 A9 WO 0206115A9
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- aiφlane
- control
- flight control
- flight
- fcm
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
- B64C13/38—Transmitting means with power amplification
- B64C13/50—Transmitting means with power amplification using electrical energy
- B64C13/503—Fly-by-Wire
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/0055—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements
- G05D1/0077—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements using redundant signals or controls
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Abstract
Description
Claims
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE60108637T DE60108637T2 (en) | 2000-07-14 | 2001-07-13 | AIR CONTROL MODULES, BUILT IN THE INTEGRATED MODULAR AVIONICS |
EP01952701A EP1301393B1 (en) | 2000-07-14 | 2001-07-13 | Flight control modules merged into the integrated modular avionics |
JP2002512025A JP2004506561A (en) | 2000-07-14 | 2001-07-13 | Flight control module merged with integrated modular avionics |
AT01952701T ATE287822T1 (en) | 2000-07-14 | 2001-07-13 | FLIGHT CONTROL MODULES BUILT INTO THE INTEGRATED MODULAR AVIONICS |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/616,196 US6443399B1 (en) | 2000-07-14 | 2000-07-14 | Flight control module merged into the integrated modular avionics |
US09/616,196 | 2000-07-14 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2002006115A1 WO2002006115A1 (en) | 2002-01-24 |
WO2002006115A9 true WO2002006115A9 (en) | 2002-09-06 |
Family
ID=24468413
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2001/022063 WO2002006115A1 (en) | 2000-07-14 | 2001-07-13 | Flight control modules merged into the integrated modular avionics |
Country Status (6)
Country | Link |
---|---|
US (1) | US6443399B1 (en) |
EP (1) | EP1301393B1 (en) |
JP (1) | JP2004506561A (en) |
AT (1) | ATE287822T1 (en) |
DE (1) | DE60108637T2 (en) |
WO (1) | WO2002006115A1 (en) |
Families Citing this family (41)
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US7142131B2 (en) * | 2002-07-03 | 2006-11-28 | The Boeing Company | Method and apparatus for displaying aircraft engine characteristics |
US20040059474A1 (en) * | 2002-09-20 | 2004-03-25 | Boorman Daniel J. | Apparatuses and methods for displaying autoflight information |
US6675076B1 (en) * | 2002-10-21 | 2004-01-06 | The Boeing Company | System, autopilot supplement assembly and method for increasing autopilot control authority |
WO2004074094A2 (en) | 2003-02-15 | 2004-09-02 | Gulfstream Aerospace Corporation | System and method for aircraft cabin atmospheric composition control |
US8777719B2 (en) * | 2003-04-22 | 2014-07-15 | Battle Born Gaming, Inc. | Gaming device and method of conducting a game with a changeable bonus value feature |
US7148814B2 (en) | 2003-06-06 | 2006-12-12 | The Boeing Company | Methods and systems for displaying aircraft engine characteristics |
US7209809B2 (en) * | 2003-10-15 | 2007-04-24 | The Boeing Company | Method and apparatus for obtaining high integrity and availability in multi-channel systems |
US7460029B2 (en) * | 2003-12-24 | 2008-12-02 | The Boeing Company | Systems and methods for presenting and obtaining flight control information |
US7188007B2 (en) * | 2003-12-24 | 2007-03-06 | The Boeing Company | Apparatuses and methods for displaying and receiving tactical and strategic flight guidance information |
FR2866627B1 (en) * | 2004-02-24 | 2006-05-05 | Airbus France | METHOD AND DEVICE FOR OPTIMIZING THE BRAQUING OF DETOURING SHUTTERS OF AN AIRCRAFT IN FLIGHT |
US7577501B2 (en) | 2004-02-26 | 2009-08-18 | The Boeing Company | Methods and systems for automatically tracking information during flight |
US7177731B2 (en) * | 2004-03-10 | 2007-02-13 | The Boeing Company | Systems and methods for handling aircraft information received from an off-board source |
US7363119B2 (en) * | 2004-03-10 | 2008-04-22 | The Boeing Company | Methods and systems for automatically displaying information, including air traffic control instructions |
US7881833B2 (en) * | 2004-03-12 | 2011-02-01 | Brian E. Turung | Airplane emergency navigational system |
US7321318B2 (en) | 2004-03-31 | 2008-01-22 | The Boeing Company | Methods and systems for controlling the display of information at an aircraft flight deck |
US7751947B2 (en) | 2004-03-31 | 2010-07-06 | The Boeing Company | Methods and systems for displaying assistance messages to aircraft operators |
US7418319B2 (en) * | 2004-03-31 | 2008-08-26 | The Boeing Company | Systems and methods for handling the display and receipt of aircraft control information |
US7203577B2 (en) | 2004-06-30 | 2007-04-10 | The Boeing Company | Methods and systems for displaying the source of aircraft control instructions |
US20060005147A1 (en) * | 2004-06-30 | 2006-01-05 | Hammack Jason L | Methods and systems for controlling the display of maps aboard an aircraft |
US7256710B2 (en) * | 2004-06-30 | 2007-08-14 | The Boeing Company | Methods and systems for graphically displaying sources for and natures of aircraft flight control instructions |
US20060064699A1 (en) * | 2004-09-21 | 2006-03-23 | Bonk Ted J | Method and system for processing resource allocations |
US7580235B2 (en) | 2004-10-12 | 2009-08-25 | The Boeing Company | Systems and methods for monitoring and controlling circuit breakers |
EP1977292A2 (en) * | 2006-01-17 | 2008-10-08 | Gulfstream Aerospace Corporation | System and method for an integrated backup control system |
BRPI0706613A2 (en) * | 2006-01-17 | 2011-04-05 | Gulfstream Aerospace Corp | apparatus and method for backup control in a distributed video control system |
US7551989B2 (en) * | 2006-06-21 | 2009-06-23 | Calspan Corporation | Autonomous outer loop control of man-rated fly-by-wire aircraft |
FR2903384B1 (en) * | 2006-07-04 | 2009-05-29 | Airbus France Sas | FLIGHT CONTROL SYSTEM FOR AIRCRAFT, AND TEST SYSTEM FOR TESTING SUCH A FLIGHT CONTROL SYSTEM. |
DE102006039671A1 (en) * | 2006-08-24 | 2008-03-20 | Liebherr-Aerospace Lindenberg Gmbh | Modular electronic flight control system has actuator control-electronics having selection logic to decide whether to use directly received pilot guidelines or reference values of flight control processor for controlling actuator module |
EP1942054B1 (en) * | 2007-01-08 | 2013-05-29 | Saab Ab | A method, an electrical system, a digital control module, and an actuator control module in a vehicle |
FR2920410B1 (en) * | 2007-09-03 | 2009-10-30 | Airbus France Sas | DISTRIBUTED ARCHITECTURE BETWEEN A FADEC AND AVIONIC COMPONENTS |
US7840316B2 (en) * | 2007-12-17 | 2010-11-23 | Honeywell International Inc. | Limited authority and full authority mode fly-by-wire flight control surface actuation control system |
US8180562B2 (en) | 2008-06-04 | 2012-05-15 | The Boeing Company | System and method for taxi route entry parsing |
FR2934065B1 (en) * | 2008-07-17 | 2010-08-27 | Airbus France | DEVICE FOR DETERMINING THE POSITION OF A GAS LEVER IN AN AIRCRAFT |
US8386167B2 (en) | 2008-11-14 | 2013-02-26 | The Boeing Company | Display of taxi route control point information |
FR2943036B1 (en) * | 2009-03-11 | 2011-04-15 | Airbus France | DISTRIBUTED FLIGHT CONTROL SYSTEM IMPLEMENTED ACCORDING TO AN INTEGRATED MODULAR AVIONIC ARCHITECTURE. |
EP2296064B1 (en) * | 2009-09-10 | 2019-04-24 | Sikorsky Aircraft Corporation | Life improving flight control system |
JP5607919B2 (en) * | 2009-12-16 | 2014-10-15 | 川崎重工業株式会社 | Integrated airborne electronic system |
US20120203401A1 (en) * | 2011-02-08 | 2012-08-09 | Jonathan Mark Dunsdon | Onboard Maintenance System Network Optimization |
US9126677B1 (en) | 2014-10-16 | 2015-09-08 | Sydney Robert Curtis | Universal multi-role aircraft protocol |
US10759520B2 (en) | 2017-09-29 | 2020-09-01 | The Boeing Company | Flight control system and method of use |
US11235885B2 (en) * | 2019-12-20 | 2022-02-01 | Pratt & Whitney Canada Corp. | Method and system for determining a throttle position of an aircraft |
CN113386949A (en) * | 2021-08-16 | 2021-09-14 | 中国商用飞机有限责任公司 | Control system for controlling flaps and/or slats of an aircraft, and aircraft |
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US3679156A (en) * | 1970-07-20 | 1972-07-25 | Ltv Electrosystems Inc | Fly-by-wire |
US3905241A (en) * | 1973-10-29 | 1975-09-16 | Mc Donnell Douglas Corp | Electrical primary flight control system |
DE2363801C3 (en) | 1973-12-21 | 1980-08-21 | Vereinigte Flugtechnische Werke- Fokker Gmbh, 2800 Bremen | Vehicle control |
US4150686A (en) * | 1976-11-15 | 1979-04-24 | Textron Inc. | Electrohydraulic control module |
US4244277A (en) * | 1979-03-02 | 1981-01-13 | Parker-Hannifin Corporation | Redundant servo with fail-safe electric system |
US4472780A (en) * | 1981-09-28 | 1984-09-18 | The Boeing Company | Fly-by-wire lateral control system |
US4567813A (en) | 1982-05-06 | 1986-02-04 | Moog Inc. | Pressure equalization of multiple valves |
US4807516A (en) | 1987-04-23 | 1989-02-28 | The Boeing Company | Flight control system employing three controllers operating a dual actuator |
US4887214A (en) | 1987-10-27 | 1989-12-12 | The Boeing Company | Flight control system employing two dual controllers operating a dual actuator |
US5036469A (en) | 1989-03-02 | 1991-07-30 | The Boeing Company | Pitch attitude command flight control system for landing flare |
FR2686310B1 (en) | 1992-01-20 | 1994-04-08 | Aerospatiale Ste Nationale Indle | SYSTEM FOR CONTROLLING AN AERODYNAMIC SURFACE OF AN AIRCRAFT. |
US5493497A (en) | 1992-06-03 | 1996-02-20 | The Boeing Company | Multiaxis redundant fly-by-wire primary flight control system |
JP3168448B2 (en) | 1994-07-08 | 2001-05-21 | 川崎重工業株式会社 | Digital flight control system |
US5670856A (en) | 1994-11-07 | 1997-09-23 | Alliedsignal Inc. | Fault tolerant controller arrangement for electric motor driven apparatus |
US5823468A (en) * | 1995-10-24 | 1998-10-20 | Bothe; Hans-Jurgen | Hybrid aircraft |
US5764502A (en) * | 1996-05-28 | 1998-06-09 | Sundstrand Corporation | Integrated electric power system |
US5806805A (en) | 1996-08-07 | 1998-09-15 | The Boeing Company | Fault tolerant actuation system for flight control actuators |
-
2000
- 2000-07-14 US US09/616,196 patent/US6443399B1/en not_active Expired - Fee Related
-
2001
- 2001-07-13 AT AT01952701T patent/ATE287822T1/en not_active IP Right Cessation
- 2001-07-13 DE DE60108637T patent/DE60108637T2/en not_active Expired - Fee Related
- 2001-07-13 JP JP2002512025A patent/JP2004506561A/en not_active Withdrawn
- 2001-07-13 EP EP01952701A patent/EP1301393B1/en not_active Expired - Lifetime
- 2001-07-13 WO PCT/US2001/022063 patent/WO2002006115A1/en active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
DE60108637D1 (en) | 2005-03-03 |
US6443399B1 (en) | 2002-09-03 |
WO2002006115A1 (en) | 2002-01-24 |
JP2004506561A (en) | 2004-03-04 |
ATE287822T1 (en) | 2005-02-15 |
DE60108637T2 (en) | 2006-05-11 |
EP1301393B1 (en) | 2005-01-26 |
EP1301393A1 (en) | 2003-04-16 |
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