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BE899879A - Dispositif avertisseur d'inclinaison excessive pour aeronef a aile rotative. - Google Patents

Dispositif avertisseur d'inclinaison excessive pour aeronef a aile rotative.

Info

Publication number
BE899879A
BE899879A BE0/213113A BE213113A BE899879A BE 899879 A BE899879 A BE 899879A BE 0/213113 A BE0/213113 A BE 0/213113A BE 213113 A BE213113 A BE 213113A BE 899879 A BE899879 A BE 899879A
Authority
BE
Belgium
Prior art keywords
wing aircraft
warning device
rotating wing
excessive tilt
tilt warning
Prior art date
Application number
BE0/213113A
Other languages
English (en)
Inventor
N S Paterson
Original Assignee
Sundstrand Data Control
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 Sundstrand Data Control filed Critical Sundstrand Data Control
Publication of BE899879A publication Critical patent/BE899879A/fr

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

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Traffic Control Systems (AREA)
  • Emergency Alarm Devices (AREA)
  • Alarm Systems (AREA)
  • Jib Cranes (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

Un dispositif pour avertir le pilote d'un aéronef à aile rotative, par exemple un hélicoptère des conditions de vol qui, si on les laisse sans correction, provoquent un choc de la queue de l'avion contre le sol, surveille l'altitude au-dessus du sol, la vitesse de descente, l'inclinaison et le changement d'inclinaison de l'avion, et fournit un avertissement si la relation entre les paramètres mentionnés est telle que le heurt de la queue est imminent.
BE0/213113A 1983-06-10 1984-06-08 Dispositif avertisseur d'inclinaison excessive pour aeronef a aile rotative. BE899879A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/503,219 US4769645A (en) 1983-06-10 1983-06-10 Excessive pitch attitude warning system for rotary wing aircraft

Publications (1)

Publication Number Publication Date
BE899879A true BE899879A (fr) 1984-12-10

Family

ID=24001200

Family Applications (1)

Application Number Title Priority Date Filing Date
BE0/213113A BE899879A (fr) 1983-06-10 1984-06-08 Dispositif avertisseur d'inclinaison excessive pour aeronef a aile rotative.

Country Status (16)

Country Link
US (1) US4769645A (fr)
JP (1) JPS608197A (fr)
AU (1) AU544110B2 (fr)
BE (1) BE899879A (fr)
CA (1) CA1242255A (fr)
CH (1) CH660160A5 (fr)
DE (1) DE3421441A1 (fr)
FI (1) FI841932L (fr)
FR (1) FR2547275B1 (fr)
GB (2) GB2141394B (fr)
GR (1) GR82152B (fr)
IL (1) IL71607A (fr)
IT (1) IT1178397B (fr)
NL (1) NL8401853A (fr)
NZ (1) NZ207889A (fr)
SE (1) SE460283B (fr)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2963912B2 (ja) * 1992-04-18 1999-10-18 株式会社光電製作所 Ｇｐｓ航法装置
GB9508659D0 (en) * 1995-04-28 1995-06-14 Smiths Industries Plc Aircraft instruments
US5781126A (en) * 1996-07-29 1998-07-14 Alliedsignal Inc. Ground proximity warning system and methods for rotary wing aircraft
US6121899A (en) * 1999-04-16 2000-09-19 Rockwell Collins, Inc. Impending aircraft tail strike warning display symbology
US6422517B1 (en) * 1999-12-02 2002-07-23 Boeing Company Aircraft tailstrike avoidance system
EP1727012B1 (fr) * 1999-12-02 2007-11-07 The Boeing Company Système pour éviter un toucher de queue pour un avion
DE60143440D1 (de) 2000-09-14 2010-12-23 Honeywell Int Inc Verfahren, vorrichtung und computerprogrammprodukt zur warnung vor einer hubschrauberheckbodenberührung
FR2816704B1 (fr) 2000-11-14 2003-02-21 Eads Airbus Sa Procede et dispositif pour la detection de l'envol d'un avion en cours de decollage
EP1407226A1 (fr) * 2001-07-17 2004-04-14 Honeywell International Inc. Dispositif d'avertissement d'angle de tangage pour systeme avertisseur ameliore de proximite du sol (egwps)
WO2003066433A1 (fr) * 2002-02-06 2003-08-14 Honeywell International, Inc. Appareil pour guidage d'un avion en detresse
US7239266B2 (en) * 2004-08-26 2007-07-03 Honeywell International Inc. Radar altimeter
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
US8866667B2 (en) 2012-02-22 2014-10-21 Honeywell International Inc. High sensitivity single antenna FMCW radar
US9297885B2 (en) 2012-07-27 2016-03-29 Honeywell International Inc. Method of system compensation to reduce the effects of self interference in frequency modulated continuous wave altimeter systems
US9660605B2 (en) 2014-06-12 2017-05-23 Honeywell International Inc. Variable delay line using variable capacitors in a maximally flat time delay filter
US10018716B2 (en) 2014-06-26 2018-07-10 Honeywell International Inc. Systems and methods for calibration and optimization of frequency modulated continuous wave radar altimeters using adjustable self-interference cancellation
US9989972B2 (en) * 2016-02-22 2018-06-05 The Boeing Company Systems and methods to prevent an aircraft from tail contact with the ground
US10860038B2 (en) * 2018-02-26 2020-12-08 Textron Innovations Inc. System and method for automatic rotorcraft tail strike protection
CN113928575A (zh) * 2021-10-20 2022-01-14 成都国营锦江机器厂 一种预防直升机尾部着地的告警方法和装置

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3979717A (en) * 1974-06-03 1976-09-07 United Technologies Corporation Helicopter warning system
IL48315A (en) * 1975-03-18 1978-08-31 United Technologies Corp Warning system for helicopters for avoiding tail contact during landing
US4027838A (en) * 1975-03-18 1977-06-07 United Technologies Corporation Helicopter warning system
US4060793A (en) * 1976-07-19 1977-11-29 Sundstrand Data Control, Inc. Excessive sink rate warning system for aircraft
DE3228557A1 (de) * 1982-07-30 1984-02-09 Ulrich 8000 München Trampnau Warnvorrichtung fuer hubschrauber
US4551723A (en) * 1983-06-10 1985-11-05 Sundstrand Data Control, Inc. Excessive descent rate warning system for rotary wing aircraft

Also Published As

Publication number Publication date
FR2547275B1 (fr) 1988-04-15
SE8403096D0 (sv) 1984-06-08
JPS608197A (ja) 1985-01-17
GB2149373A (en) 1985-06-12
IT1178397B (it) 1987-09-09
IT8448339A0 (it) 1984-06-07
SE460283B (sv) 1989-09-25
GB2141394A (en) 1984-12-19
GB8412949D0 (en) 1984-06-27
GB8428728D0 (en) 1984-12-27
DE3421441C2 (fr) 1989-07-27
NL8401853A (nl) 1985-01-02
FI841932A0 (fi) 1984-05-14
AU544110B2 (en) 1985-05-16
DE3421441A1 (de) 1984-12-13
CA1242255A (fr) 1988-09-20
US4769645A (en) 1988-09-06
SE8403096L (sv) 1984-12-11
GR82152B (fr) 1984-12-13
GB2149373B (en) 1986-10-15
FI841932L (fi) 1984-12-11
FR2547275A1 (fr) 1984-12-14
GB2141394B (en) 1986-10-15
IL71607A (en) 1990-08-31
NZ207889A (en) 1987-07-31
CH660160A5 (fr) 1987-03-31
AU2884384A (en) 1984-12-13

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Legal Events

Date Code Title Description
RE Patent lapsed

Owner name: SUNDSTRAND DATA CONTROL INC.

Effective date: 19880630