DE60143440D1 - Verfahren, vorrichtung und computerprogrammprodukt zur warnung vor einer hubschrauberheckbodenberührung - Google Patents

Verfahren, vorrichtung und computerprogrammprodukt zur warnung vor einer hubschrauberheckbodenberührung

Info

Publication number
DE60143440D1
DE60143440D1 DE60143440T DE60143440T DE60143440D1 DE 60143440 D1 DE60143440 D1 DE 60143440D1 DE 60143440 T DE60143440 T DE 60143440T DE 60143440 T DE60143440 T DE 60143440T DE 60143440 D1 DE60143440 D1 DE 60143440D1
Authority
DE
Germany
Prior art keywords
computer program
program product
procedure
warning before
bottom tread
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Lifetime
Application number
DE60143440T
Other languages
English (en)
Inventor
Kevin Conner
Noel Paterson
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Honeywell International Inc
Original Assignee
Honeywell International Inc
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 Honeywell International Inc filed Critical Honeywell International Inc
Application granted granted Critical
Publication of DE60143440D1 publication Critical patent/DE60143440D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C5/00—Measuring height; Measuring distances transverse to line of sight; Levelling between separated points; Surveyors' levels
    • G01C5/005—Measuring height; Measuring distances transverse to line of sight; Levelling between separated points; Surveyors' levels altimeters for aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Mechanical Engineering (AREA)
  • Emergency Alarm Devices (AREA)
  • Traffic Control Systems (AREA)
  • Alarm Systems (AREA)
  • Navigation (AREA)
  • Audible And Visible Signals (AREA)
DE60143440T 2000-09-14 2001-05-25 Verfahren, vorrichtung und computerprogrammprodukt zur warnung vor einer hubschrauberheckbodenberührung Expired - Lifetime DE60143440D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US23296700P 2000-09-14 2000-09-14
PCT/US2001/017227 WO2002023125A1 (en) 2000-09-14 2001-05-25 Method, apparatus and computer program product for helicopter tail strike warning

Publications (1)

Publication Number Publication Date
DE60143440D1 true DE60143440D1 (de) 2010-12-23

Family

ID=22875305

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60143440T Expired - Lifetime DE60143440D1 (de) 2000-09-14 2001-05-25 Verfahren, vorrichtung und computerprogrammprodukt zur warnung vor einer hubschrauberheckbodenberührung

Country Status (5)

Country Link
US (1) US6737987B2 (de)
EP (1) EP1317652B1 (de)
AT (1) ATE487923T1 (de)
DE (1) DE60143440D1 (de)
WO (1) WO2002023125A1 (de)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6906641B2 (en) * 2000-05-26 2005-06-14 Honeywell International Inc. Apparatus, method and computer program product for helicopter enhanced ground proximity warning system
FR2848662B1 (fr) * 2002-12-17 2005-03-04 Thales Sa Dispositif d'affichage pour equipement anticollision terrain embarque a bord d'aeronef
US20050113985A1 (en) * 2003-11-26 2005-05-26 Safe Flight Instrument Corporation Obstacle avoidance system for rotary wing aircraft
US6980153B2 (en) * 2004-05-17 2005-12-27 Honeywell International Inc. Radar altimeter for helicopter load carrying operations
US7126496B2 (en) * 2004-09-30 2006-10-24 Safe Flight Instrument Corporation Tactile cueing system and method for aiding a helicopter pilot in making landings
US20060089759A1 (en) * 2004-10-22 2006-04-27 Honeywell International Inc. Systems and methods for performing high accurate distance measuring for radar altimeters
US7145501B1 (en) 2005-09-26 2006-12-05 Honeywell International Inc. Methods and systems for measuring terrain height
FR2893158B1 (fr) * 2005-11-10 2007-12-28 Thales Sa Procede de generation d'une base de donnees comportant des informations topographiques sur des obstacles, et base de donnees d'obstacles.
FR2908218B1 (fr) * 2006-11-07 2014-08-15 Thales Sa Dispositif d'aide a la navigation d'un aeronef dans une zone aeroportuaire
US7598888B2 (en) * 2006-12-08 2009-10-06 Sikorsky Aircraft Corporation Rotary wing aircraft proximity warning system with a geographically based avoidance system
US20080173753A1 (en) * 2007-01-22 2008-07-24 Honeywell International Inc. Methods and systems for monitoring approach of rotary wing aircraft
WO2009002645A2 (en) * 2007-05-24 2008-12-31 Aviation Communication & Surveillance Systems Llc Systems and methods for aircraft winshear detection
EP2226766A3 (de) * 2009-03-02 2014-06-11 Sikorsky Aircraft Corporation Rotorsystem-Gesundheitsüberwachung mit Schaftbelastungsmessungen und virtuelle Überwachung von Lasten
US9196168B2 (en) * 2009-05-20 2015-11-24 Textron Innovations Inc. Collision avoidance and warning system
FR2956512B1 (fr) * 2010-02-16 2012-03-09 Airbus Operations Sas Procede et dispositif de protection automatique d'un aeronef contre un taux de descente excessif.
US9261883B2 (en) * 2010-05-07 2016-02-16 Honeywell International Inc. Systems and methods for performing excessive negative pitch alert and for biasing a sink rate alert
US9828113B2 (en) 2013-11-05 2017-11-28 Safe Flight Instrument Corporation Tailstrike warning system
WO2015069228A1 (en) * 2013-11-05 2015-05-14 Safe Flight Instrument Corporation Tailstrike warning system
US9546003B2 (en) * 2014-03-14 2017-01-17 Safe Flight Instrument Corporation Deflare pitch command
US20170008639A1 (en) 2015-07-08 2017-01-12 Safe Flight Instrument Corporation Aircraft turbulence detection
US9989972B2 (en) * 2016-02-22 2018-06-05 The Boeing Company Systems and methods to prevent an aircraft from tail contact with the ground
US10040574B1 (en) * 2016-04-26 2018-08-07 James William Laske, Jr. Airplane anti-hijacking system
FR3063715B1 (fr) * 2017-03-09 2019-04-12 Dassault Aviation Systeme d'avertissement de proximite au sol d'un aeronef, avionique et procede associe
EP3613032A1 (de) * 2017-04-18 2020-02-26 Aviation Communication & Surveillance Systems LLC Systeme und verfahren zur aktivierung einer funkbake für globale flugzeugverfolgung
US10852747B2 (en) * 2018-02-21 2020-12-01 The Boeing Company Tailstrike awareness system
CN110069070B (zh) * 2019-05-08 2022-01-18 成都高威节能科技有限公司 一种提高大型飞机起飞过程安全性的方法
US11827376B2 (en) * 2022-04-19 2023-11-28 Honeywell International Inc. Enhanced ground proximity warning system that selectively operates in both a helicopter mode and a fixed-wing mode

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US3715718A (en) 1970-08-11 1973-02-06 Sundstrand Data Control Ground proximity warning system utilizing radio and barometric altimeter combination
US3979717A (en) * 1974-06-03 1976-09-07 United Technologies Corporation Helicopter warning system
US3936796A (en) 1974-06-19 1976-02-03 Sundstrand Data Control, Inc. Aircraft ground proximity warning instrument
US3958218A (en) 1974-10-03 1976-05-18 Sundstrand Data Control, Inc. Aircraft ground proximity warning system with speed compensation
US3944968A (en) 1974-11-01 1976-03-16 Sundstrand Data Control, Inc. Aircraft ground proximity warning system having speed versus altitude compensation
US3947808A (en) 1975-01-13 1976-03-30 Sundstrand Data Control, Inc. Excessive descent rate warning system for aircraft
US3947810A (en) 1975-01-13 1976-03-30 Sundstrand Data Control, Inc. Negative climb rate after take-off warning system with predetermined loss of altitude inhibit
US3934221A (en) 1975-03-06 1976-01-20 Sundstrand Data Control, Inc. Terrain closure warning system with altitude rate signal conditioning
US3958219A (en) 1975-03-06 1976-05-18 Sundstrand Data Control, Inc. Terrain closure warning system with altitude rate signal conditioning
US4027838A (en) * 1975-03-18 1977-06-07 United Technologies Corporation Helicopter warning system
US3925751A (en) 1975-04-02 1975-12-09 Sundstrand Data Control Glide slope warning system with a variable warning rate
US3934222A (en) 1975-04-02 1976-01-20 Sundstrand Data Control, Inc. Terrain closure warning system with climb inhibit and altitude gain measurement
US4060793A (en) 1976-07-19 1977-11-29 Sundstrand Data Control, Inc. Excessive sink rate warning system for aircraft
US4030065A (en) 1976-07-19 1977-06-14 Sundstrand Corporation Terrain clearance warning system for aircraft
US4224669A (en) 1977-12-22 1980-09-23 The Boeing Company Minimum safe altitude monitoring, indication and warning system
US4215334A (en) 1978-02-09 1980-07-29 Sundstrand Data Control, Inc. Aircraft excessive descent rate warning system
US4319218A (en) 1980-01-04 1982-03-09 Sundstrand Corporation Negative climb after take-off warning system with configuration warning means
US4818992A (en) 1983-06-10 1989-04-04 Sundstrand Data Control, Inc. Excessive altitude loss after take-off warning system for rotary wing aircraft
US4551723A (en) 1983-06-10 1985-11-05 Sundstrand Data Control, Inc. Excessive descent rate warning system for rotary wing aircraft
US4769645A (en) 1983-06-10 1988-09-06 Sundstrand Data Control, Inc. Excessive pitch attitude warning system for rotary wing aircraft
US4675823A (en) 1983-12-09 1987-06-23 Sundstrand Data Control, Inc. Ground proximity warning system geographic area determination
US4646244A (en) 1984-02-02 1987-02-24 Sundstrand Data Control, Inc. Terrain advisory system
US4914436A (en) 1987-04-06 1990-04-03 Sundstrand Data Control, Inc. Ground proximity approach warning system without landing flap input
FR2697796B1 (fr) 1992-11-10 1994-12-09 Sextant Avionique Dispositif d'évitement de collisions pour aéronef notamment avec le sol.
JPH0774718A (ja) 1993-09-02 1995-03-17 Mitsubishi Electric Corp 時分割通信制御方法
FR2718875B1 (fr) 1994-04-15 1996-05-15 Sextant Avionique Dispositif d'aide à l'atterrissage.
US5666110A (en) 1995-03-09 1997-09-09 Paterson; Noel S. Helicopter enhanced descent after take-off warning for GPWS
US6138060A (en) 1995-07-31 2000-10-24 Alliedsignal Inc. Terrain awareness system
US6092009A (en) 1995-07-31 2000-07-18 Alliedsignal Aircraft terrain information system
US5839080B1 (en) 1995-07-31 2000-10-17 Allied Signal Inc Terrain awareness system
US5781126A (en) 1996-07-29 1998-07-14 Alliedsignal Inc. Ground proximity warning system and methods for rotary wing aircraft
US6043759A (en) 1996-07-29 2000-03-28 Alliedsignal Air-ground logic system and method for rotary wing aircraft

Also Published As

Publication number Publication date
US6737987B2 (en) 2004-05-18
EP1317652B1 (de) 2010-11-10
EP1317652A1 (de) 2003-06-11
ATE487923T1 (de) 2010-11-15
WO2002023125A1 (en) 2002-03-21
US20020030607A1 (en) 2002-03-14

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