[go: up one dir, main page]

SG11201606267PA - Short landing warning - Google Patents

Short landing warning

Info

Publication number
SG11201606267PA
SG11201606267PA SG11201606267PA SG11201606267PA SG11201606267PA SG 11201606267P A SG11201606267P A SG 11201606267PA SG 11201606267P A SG11201606267P A SG 11201606267PA SG 11201606267P A SG11201606267P A SG 11201606267PA SG 11201606267P A SG11201606267P A SG 11201606267PA
Authority
SG
Singapore
Prior art keywords
short landing
landing warning
warning
short
landing
Prior art date
Application number
SG11201606267PA
Inventor
Mark H Henderson
Original Assignee
Boeing Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Boeing Co filed Critical Boeing Co
Publication of SG11201606267PA publication Critical patent/SG11201606267PA/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
    • B64D45/08—Landing aids; Safety measures to prevent collision with earth's surface optical
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
    • G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft
    • G08G5/80—Anti-collision systems
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft
    • G08G5/50—Navigation or guidance aids
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft
    • G08G5/50—Navigation or guidance aids
    • G08G5/55—Navigation or guidance aids for a single aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Traffic Control Systems (AREA)
SG11201606267PA 2014-03-18 2015-02-23 Short landing warning SG11201606267PA (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US14/218,672 US9522742B2 (en) 2014-03-18 2014-03-18 Short landing warning
PCT/US2015/017145 WO2015142481A1 (en) 2014-03-18 2015-02-23 Short landing warning

Publications (1)

Publication Number Publication Date
SG11201606267PA true SG11201606267PA (en) 2016-08-30

Family

ID=52669660

Family Applications (1)

Application Number Title Priority Date Filing Date
SG11201606267PA SG11201606267PA (en) 2014-03-18 2015-02-23 Short landing warning

Country Status (6)

Country Link
US (1) US9522742B2 (en)
EP (1) EP3094561B1 (en)
JP (1) JP6573902B2 (en)
CN (1) CN106061842B (en)
SG (1) SG11201606267PA (en)
WO (1) WO2015142481A1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016095096A1 (en) 2014-12-15 2016-06-23 深圳市大疆创新科技有限公司 Aircraft and take-off control method and system and landing control method and system thereof
FR3044809B1 (en) * 2015-12-03 2017-11-24 Airbus Operations Sas METHOD AND SYSTEM FOR AIDING THE LANDING OF AN AIRCRAFT.
RU2620587C1 (en) * 2016-04-27 2017-05-29 Акционерное общество "Лётно-исследовательский институт имени М.М. Громова" Method of determining the coordinates of an aircraft relative to the flight strip
US10228692B2 (en) 2017-03-27 2019-03-12 Gulfstream Aerospace Corporation Aircraft flight envelope protection and recovery autopilot
FR3072948B1 (en) * 2017-10-30 2019-11-15 Airbus Operations SYSTEM FOR ASSISTING THE LANDING OF AN AIRCRAFT IN THE APPROACH PHASE OF A LANDING TRACK
CN110949659A (en) * 2019-12-06 2020-04-03 江西洪都航空工业集团有限责任公司 Trailing edge flap control method

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IL76204A0 (en) * 1984-09-06 1985-12-31 Sundstrand Data Control Excessive descent rate warning system for tactical aircraft
US5196847A (en) * 1991-09-18 1993-03-23 Sundstrand Corporation Ground proximity warning instrument using flight path modulation of glide slope alerting function
US5343395A (en) * 1992-08-26 1994-08-30 Watts Alan B Aircraft landing guidance system and method
CA2136570A1 (en) * 1994-02-04 1995-08-05 Gary L. Viviani Hybrid synthetic aircraft landing system
FR2717934B1 (en) * 1994-03-22 1996-04-26 Sextant Avionique Collision avoidance device for aircraft in particular with the ground by approach slope control.
FR2725691B1 (en) * 1994-10-18 1997-01-03 Sextant Avionique PILOT AID DEVICE, DURING LANDING, OF AN AIRCRAFT
WO2000047948A1 (en) 1999-02-01 2000-08-17 Honeywell International Inc. Apparatus, method, and computer program product for generating terrain clearance floor envelopes about a selected runway
US6785594B1 (en) 1999-03-25 2004-08-31 Honeywell International Inc. Ground proximity warning system and method having a reduced set of input parameters
EP1309837B1 (en) 2000-08-18 2006-12-13 Honeywell International Inc. Glideslope monitor for aircraft
JP2002092799A (en) * 2000-09-19 2002-03-29 Toshiba Corp Landing guidance diagnostic system
US6980892B1 (en) * 2003-11-18 2005-12-27 Garmin International, Inc. Avionics system and method for providing altitude alerts during final landing approach
FR2897593B1 (en) * 2006-02-17 2012-09-14 Airbus France METHOD AND SYSTEM FOR PREDICTING THE POSSIBILITY OF COMPLETELY STOPPING AN AIRCRAFT ON A LANDING TRAIL.
FR2913503B1 (en) * 2007-03-06 2009-07-17 Thales Sa FLIGHT MANAGEMENT CALCULATOR TAKING INTO ACCOUNT OF APPROACH SPEED CONSTRAINTS
US20100036550A1 (en) * 2008-08-05 2010-02-11 Honeywell International Inc. Systems and methods for improving pilot situational awareness during landing
FR2936079B1 (en) * 2008-09-16 2010-09-17 Thales Sa METHOD FOR MONITORING THE LANDING PHASE OF AN AIRCRAFT
KR20130020889A (en) * 2010-04-09 2013-03-04 샌델 에이비아닉스 인코포레이티드 Taws with alert suppression
US8560150B1 (en) * 2010-07-07 2013-10-15 The Boeing Company Methods and systems for landing decision point
US8532848B2 (en) * 2010-10-19 2013-09-10 Honeywell International Inc. Systems and methods for alerting potential tailstrike during landing
US8630756B2 (en) * 2011-04-12 2014-01-14 The Boeing Company Airplane position assurance monitor
US8653990B2 (en) * 2012-06-18 2014-02-18 The Boeing Company Stall management system
US9129521B2 (en) * 2013-05-29 2015-09-08 Honeywell International Inc. System and method for displaying a runway position indicator

Also Published As

Publication number Publication date
EP3094561A1 (en) 2016-11-23
CN106061842A (en) 2016-10-26
EP3094561B1 (en) 2018-02-21
US20150266590A1 (en) 2015-09-24
WO2015142481A1 (en) 2015-09-24
CN106061842B (en) 2018-08-31
JP6573902B2 (en) 2019-09-11
US9522742B2 (en) 2016-12-20
JP2017509532A (en) 2017-04-06

Similar Documents

Publication Publication Date Title
IL279836B (en) Aircraft system
GB201416842D0 (en) Aircraft
GB201405553D0 (en) Rotor-Lift Aircraft
PL3177817T3 (en) Aircraft
GB201508138D0 (en) Aircraft
SG11201609232YA (en) Aircraft collision warning
GB201616518D0 (en) Aircraft
GB2526680B (en) Runway arrangement
PL3140189T3 (en) Helicopter
EP3061629A4 (en) Tire
SG11201606267PA (en) Short landing warning
GB201415491D0 (en) Propeller
GB2549885B (en) Landing system
AU355715S (en) Travelator
GB2532752B (en) Truck
TWM489236U (en) Warning apparatus
AU365494S (en) Warning triangle
GB201409437D0 (en) Warning system
TWM489091U (en) Warning pen
GB201414917D0 (en) Hydroplane
GB201414790D0 (en) Hydroplanes
PH32014000854S1 (en) Car
PH32014000814S1 (en) Car
PH32014000813S1 (en) Car
PH32014000812S1 (en) Car