EP3066651A4 - Système d'avertissement de choc entre la queue d'un aéronef et le sol - Google Patents

Système d'avertissement de choc entre la queue d'un aéronef et le sol Download PDF

Info

Publication number
EP3066651A4
EP3066651A4 EP13897022.3A EP13897022A EP3066651A4 EP 3066651 A4 EP3066651 A4 EP 3066651A4 EP 13897022 A EP13897022 A EP 13897022A EP 3066651 A4 EP3066651 A4 EP 3066651A4
Authority
EP
European Patent Office
Prior art keywords
warning system
tailstrike
tailstrike warning
warning
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.)
Withdrawn
Application number
EP13897022.3A
Other languages
German (de)
English (en)
Other versions
EP3066651A1 (fr
Inventor
Randall A. Greene
Shawn BEYER
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.)
Safe Flight Instrument Co
Safe Flight Instrument Corp
Original Assignee
Safe Flight Instrument Co
Safe Flight Instrument Corp
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 Safe Flight Instrument Co, Safe Flight Instrument Corp filed Critical Safe Flight Instrument Co
Publication of EP3066651A1 publication Critical patent/EP3066651A1/fr
Publication of EP3066651A4 publication Critical patent/EP3066651A4/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D43/00—Arrangements or adaptations of instruments
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C23/00—Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
    • G01C23/005—Flight directors
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/02—Automatic approach or landing aids, i.e. systems in which flight data of incoming planes are processed to provide landing data
    • G08G5/025—Navigation or guidance aids
EP13897022.3A 2013-11-05 2013-11-05 Système d'avertissement de choc entre la queue d'un aéronef et le sol Withdrawn EP3066651A4 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US2013/068580 WO2015069228A1 (fr) 2013-11-05 2013-11-05 Système d'avertissement de choc entre la queue d'un aéronef et le sol

Publications (2)

Publication Number Publication Date
EP3066651A1 EP3066651A1 (fr) 2016-09-14
EP3066651A4 true EP3066651A4 (fr) 2017-07-19

Family

ID=53041846

Family Applications (1)

Application Number Title Priority Date Filing Date
EP13897022.3A Withdrawn EP3066651A4 (fr) 2013-11-05 2013-11-05 Système d'avertissement de choc entre la queue d'un aéronef et le sol

Country Status (2)

Country Link
EP (1) EP3066651A4 (fr)
WO (1) WO2015069228A1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10852747B2 (en) * 2018-02-21 2020-12-01 The Boeing Company Tailstrike awareness system

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2300167A (en) * 1995-04-28 1996-10-30 Smiths Industries Plc Aircraft instrument for indicating rate of change of pitch
US6121899A (en) * 1999-04-16 2000-09-19 Rockwell Collins, Inc. Impending aircraft tail strike warning display symbology

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6422517B1 (en) * 1999-12-02 2002-07-23 Boeing Company Aircraft tailstrike avoidance system
EP1317652B1 (fr) * 2000-09-14 2010-11-10 Honeywell International Inc. Procede, appareil et progiciel informatique d'alerte de collision de la poutre de queue
AU2002334708A1 (en) * 2001-10-01 2003-04-14 Kline And Walker, Llc Pfn/trac system faa upgrades for accountable remote and robotics control
US8532848B2 (en) * 2010-10-19 2013-09-10 Honeywell International Inc. Systems and methods for alerting potential tailstrike during landing

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2300167A (en) * 1995-04-28 1996-10-30 Smiths Industries Plc Aircraft instrument for indicating rate of change of pitch
US6121899A (en) * 1999-04-16 2000-09-19 Rockwell Collins, Inc. Impending aircraft tail strike warning display symbology

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
JOHN E CASHMAN ET AL: "Angle FLIGHT OPERATIONS 10 AERO FLIGHT CREW OPERATIONS INTEGRATION BOEING COMMERCIAL AIRPLANES GROUP ON MODERN COMMERCIAL JET AIRPLANES OPERATIONAL USE OF ANGLE OF ATTACK", 31 December 2012 (2012-12-31), XP055125765, Retrieved from the Internet <URL:http://www.boeing.com/commercial/aeromagazine/aero_12/aoa.pdf> [retrieved on 20140627] *
See also references of WO2015069228A1 *

Also Published As

Publication number Publication date
WO2015069228A1 (fr) 2015-05-14
EP3066651A1 (fr) 2016-09-14

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