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
Authority: EP; European Patent Office
Prior art keywords: warning system; tailstrike; tailstrike warning; warning
Prior art date: 2013-11-05
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 Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.): Withdrawn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.)

2013-11-05

Filing date

2013-11-05

Publication date

2017-07-19

2013-11-05 Application filed by Safe Flight Instrument Co, Safe Flight Instrument Corp filed Critical Safe Flight Instrument Co

2016-09-14 Publication of EP3066651A1 publication Critical patent/EP3066651A1/fr

2017-07-19 Publication of EP3066651A4 publication Critical patent/EP3066651A4/fr

Status Withdrawn legal-status Critical Current

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
- 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

Landscapes

Engineering & Computer Science (AREA)
Aviation & Aerospace Engineering (AREA)
Radar, Positioning & Navigation (AREA)
Remote Sensing (AREA)
Physics & Mathematics (AREA)
General Physics & Mathematics (AREA)
Traffic Control Systems (AREA)

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
WO2003029922A2 (fr) *	2001-10-01	2003-04-10	Kline & Walker, Llc	Perfectionnements faa au systeme pfn/tracmd pour le controle responsable a distance et robotique pour l'elimination de l'utilisation non autorisee d'aeronefs et pour l'amelioration de la gestion d'equipement et de la securite publique dans le domaine du transport
US8532848B2 (en) *	2010-10-19	2013-09-10	Honeywell International Inc.	Systems and methods for alerting potential tailstrike during landing

2013
- 2013-11-05 WO PCT/US2013/068580 patent/WO2015069228A1/fr active Application Filing
- 2013-11-05 EP EP13897022.3A patent/EP3066651A4/fr not_active Withdrawn

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
EP3066651A1 (fr)	2016-09-14
WO2015069228A1 (fr)	2015-05-14

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Legal Events

Date	Code	Title	Description
2016-08-12	PUAI	Public reference made under article 153(3) epc to a published international application that has entered the european phase	Free format text: ORIGINAL CODE: 0009012
2016-09-14	17P	Request for examination filed	Effective date: 20160217
2016-09-14	AK	Designated contracting states	Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR
2016-09-14	AX	Request for extension of the european patent	Extension state: BA ME
2017-02-08	DAX	Request for extension of the european patent (deleted)
2017-07-19	A4	Supplementary search report drawn up and despatched	Effective date: 20170621
2017-07-19	RIC1	Information provided on ipc code assigned before grant	Ipc: G08G 5/02 20060101AFI20170614BHEP Ipc: G01C 23/00 20060101ALI20170614BHEP Ipc: B64D 45/04 20060101ALI20170614BHEP Ipc: B64D 43/00 20060101ALI20170614BHEP
2018-02-27	STAA	Information on the status of an ep patent application or granted ep patent	Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE
2018-06-15	STAA	Information on the status of an ep patent application or granted ep patent	Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN
2018-07-18	18D	Application deemed to be withdrawn	Effective date: 20180118