SE8100892L - Markvarnande anordning for flygplan - Google Patents

Markvarnande anordning for flygplan

Info

Publication number
SE8100892L
SE8100892L SE8100892A SE8100892A SE8100892L SE 8100892 L SE8100892 L SE 8100892L SE 8100892 A SE8100892 A SE 8100892A SE 8100892 A SE8100892 A SE 8100892A SE 8100892 L SE8100892 L SE 8100892L
Authority
SE
Sweden
Prior art keywords
signal
aircraft
warning
slide
condition
Prior art date
Application number
SE8100892A
Other languages
English (en)
Other versions
SE449599B (sv
Inventor
C D Bateman
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 SE8100892L publication Critical patent/SE8100892L/sv
Publication of SE449599B publication Critical patent/SE449599B/sv

Links

Classifications

    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0017—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information
    • G08G5/0021—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information located in the aircraft
    • 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
    • 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)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Traffic Control Systems (AREA)
  • Emergency Alarm Devices (AREA)
  • Navigation (AREA)
  • Alarm Systems (AREA)

Claims (1)

1. PATENTKRAV Varningsinstrument inrSttat att gbra piloten i en flygfarkost uppmarksam pa ett tillstand on ej bnskad Werhet till marken vid en flygplats, soon Or utrustad med en sUndare for glidbaneradiostrale; vilken strale innefattar giltig och synbarligen giltig stignings- och siunkningsinformation, varvid instrumentet innefattar en i flygfarkosten fbrefintlig mottagare (37), son Or pdverkbar i beroende an glidbaneradiostralen fbr alstring av en signal (G/S) soon representerar riktningen och storleken boo vinkelavvikelse for flygfarkostens ldge Over eller under den medelst glidbaneradiostrAlen bestUmda glidbanan, en i beroende an signalen fran mottagaren (37) paverkbar detektor (87) 'air detektering an en, en avvikelse Under glidbanan indikerande avvikelsesignal, som representerar ett tillstAnd under glidbanan overstigande ett faststallt Verde, varvid detektorn Or anordnad att alstra en, en yarning URI att flygfarkosten befinner sig under glidbanan initierande 3ignal, och on hbjdsignelkUlla (26) fbr alstring av en signal, son representerar flygfarkostens hdjd, en i beroende an hbjdsignalkUllan (26) naverkbar konditioneringskrets (88-91) inrSttad att son funktion av hbjden variera Oct faststUllda vardet for tillstAndet under glidbanan IjOr att konditionera detektorn (87) till att alstra den en yarning om att flygfarkosten befinner sig under glidbanan initierande signalen, en kretsanordning (86) inratted att, nUr flygrarkosten befinner sig under en fdrutbestSmi hajd, inhibera den en venni00 att flygfarkrbefinner sig under glidbanan initierande signalen, ochetsanordningon Sr kopplad for att aura pa- verkbar i beroende av den en yarning on att flygfarkosten befinner sig under glidbanan initierande signalen i och fbr att aktivera en pilotvarningsanordning (54), k Unnetecknat an att en varningsdetktor (61) Sr kopplad fbr att vara paverkbar i beroende an on funktion an hbjdsignalen ftir detektering av en hbjd under ett fbrutbestSmt verde fir flygfarkostens drift atom fbr forhallandena old landning i och for att alstra en signal for minsta markfrigang, att en minneskrets (58) Or kopplad fdr att vara paverkbar i beroende av flygfarkostens fysiska till-stand fkir att fastlUggaett signaltillstIndndr flygfarkosten Or iordningstalld fbr ladning, att en OU-grind (62) Sr kopplad on en ingAng paverkbar i beroende an flygfarkostens landningstillstandssignal och en annan ingAng pAverkbar i beroer an glidbanevarningssignalen I och fbr alstring an varningsinitieringsutsignalen War endera varningssignalen upptbder, och att pilotvarningsanordningen (54) '61- pAverkbar i beroende an varningsinitieringsutsignalen frin ELLER-grinden. 56 v.is —240 in/min 6. 64 Markte -7L- Negativ atigningehastighet FD 57
SE8100892A 1974-06-19 1981-02-09 Markvarnande instrument for flygplan SE449599B (sv)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/480,727 US3946358A (en) 1974-06-19 1974-06-19 Aircraft ground proximity warning instrument

Publications (2)

Publication Number Publication Date
SE8100892L true SE8100892L (sv) 1981-02-09
SE449599B SE449599B (sv) 1987-05-11

Family

ID=23909109

Family Applications (6)

Application Number Title Priority Date Filing Date
SE7506677A SE418720B (sv) 1974-06-19 1975-06-11 Varningsinstrument for flygfarkoster
SE7808631A SE424624B (sv) 1974-06-19 1978-08-15 Varningsinstrument i flygfarkost
SE8100891A SE449598B (sv) 1974-06-19 1981-02-09 Markvarnande instrument for flygplan
SE8100890A SE422671B (sv) 1974-06-19 1981-02-09 Varningsinstrument i flygfarkost
SE8100892A SE449599B (sv) 1974-06-19 1981-02-09 Markvarnande instrument for flygplan
SE8100889A SE422715B (sv) 1974-06-19 1981-02-09 Varningsinstrument i en flygfarkost

Family Applications Before (4)

Application Number Title Priority Date Filing Date
SE7506677A SE418720B (sv) 1974-06-19 1975-06-11 Varningsinstrument for flygfarkoster
SE7808631A SE424624B (sv) 1974-06-19 1978-08-15 Varningsinstrument i flygfarkost
SE8100891A SE449598B (sv) 1974-06-19 1981-02-09 Markvarnande instrument for flygplan
SE8100890A SE422671B (sv) 1974-06-19 1981-02-09 Varningsinstrument i flygfarkost

Family Applications After (1)

Application Number Title Priority Date Filing Date
SE8100889A SE422715B (sv) 1974-06-19 1981-02-09 Varningsinstrument i en flygfarkost

Country Status (9)

Country Link
US (1) US3946358A (sv)
JP (2) JPS5934560B2 (sv)
AU (2) AU499009B2 (sv)
CA (1) CA1043005A (sv)
DE (2) DE2559952C3 (sv)
FR (2) FR2309939A1 (sv)
GB (2) GB1488745A (sv)
IT (1) IT1040627B (sv)
SE (6) SE418720B (sv)

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US4071894A (en) * 1976-06-28 1978-01-31 Rockwell International Corporation Profile warning generator with anticipation of warning condition
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US4684948A (en) * 1983-07-08 1987-08-04 Sundstrand Data Control, Inc. Ground proximity warning system having modified terrain closure rate warning on glide slope approach
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US4951047A (en) * 1983-05-13 1990-08-21 Sunstrand Data Control, Inc. Negative climb after take-off warning system
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US4980684A (en) * 1983-06-10 1990-12-25 Sundstrand Data Controls, Inc. Warning system for tactical rotary wing aircraft
US4551723A (en) * 1983-06-10 1985-11-05 Sundstrand Data Control, Inc. Excessive descent rate warning system for rotary wing aircraft
US5220322A (en) * 1984-07-18 1993-06-15 Sundstrand Corporation Ground proximity warning system for use with aircraft having egraded performance
IL75701A0 (en) * 1984-07-18 1985-11-29 Sundstrand Data Control Ground proximity warning system for aircraft
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CA1243117A (en) * 1985-02-22 1988-10-11 Michael M. Grove Altitude loss after take-off warning system utilizing time and altitude
US5187478A (en) * 1985-02-22 1993-02-16 Sundstrand Corporation Configuration responsive descent rate warning system for aircraft
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US4947164A (en) * 1988-01-21 1990-08-07 Sundstrand Data Control, Inc. Flight path responsive aircraft wind shear alerting and warning system
US4916448A (en) * 1988-02-26 1990-04-10 The United States Of America As Represented By The Secretary Of The Air Force Low altitude warning system for aircraft
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US5260702A (en) * 1989-12-27 1993-11-09 Thompson Keith P Aircraft information system
US5166682A (en) * 1991-03-07 1992-11-24 Sundstrand Corporation Ground proximity warning instrument utilizing glideslope modulation of excessive descent rate envelope
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US5406487A (en) * 1991-10-11 1995-04-11 Tanis; Peter G. Aircraft altitude approach control device
US5666110A (en) * 1995-03-09 1997-09-09 Paterson; Noel S. Helicopter enhanced descent after take-off warning for GPWS
US5745053A (en) * 1995-12-08 1998-04-28 Fleming, Iii; Hoyt A. Landing gear warning apparatus and method for pilots approaching a runway with retracted landing gear
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JP4551562B2 (ja) 1998-10-16 2010-09-29 ユニバーサル エイビーアニクス システムズ コーポレイション 飛行計画目的警報システムおよび方法
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JP4025649B2 (ja) * 2001-01-23 2007-12-26 ハネウェル・インターナショナル・インコーポレーテッド ヘリコプター用ｅｇｐｗｓカットオフ高度
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US7274309B2 (en) * 2005-03-29 2007-09-25 Nance C Kirk Aircraft landing gear initial touch-down velocity monitor
US7274310B1 (en) 2005-03-29 2007-09-25 Nance C Kirk Aircraft landing gear kinetic energy monitor
US7209053B2 (en) * 2005-04-06 2007-04-24 Honeywell International Inc. System and method for displaying validity of airport visual approach slope indicators
US7633430B1 (en) * 2007-09-14 2009-12-15 Rockwell Collins, Inc. Terrain awareness system with false alert suppression
US8042765B1 (en) 2008-05-20 2011-10-25 Nance C Kirk Aircraft landing gear compression rate monitor
FR2938683B1 (fr) * 2008-11-14 2012-06-15 Airbus France Procede et systeme d'evitement de terrain pour un aeronef
RU2449923C1 (ru) * 2010-11-15 2012-05-10 Открытое акционерное общество Московский научно-производственный комплекс "Авионика" имени О.В. Успенского (ОАО МНПК "Авионика") Система автоматического управления самолетом при заходе на посадку
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Also Published As

Publication number Publication date
DE2527056C3 (de) 1979-10-11
DE2527056B2 (de) 1979-02-15
JPS5114699A (en) 1976-02-05
DE2559952C3 (de) 1981-07-02
SE8100890L (sv) 1981-02-09
AU511815B2 (en) 1980-09-04
SE422715B (sv) 1982-03-22
AU4266578A (en) 1979-04-05
SE8100891L (sv) 1981-02-09
FR2289980A1 (fr) 1976-05-28
FR2309939B1 (sv) 1980-07-25
JPS5934560B2 (ja) 1984-08-23
SE8100889L (sv) 1981-02-09
GB1488744A (en) 1977-10-12
CA1043005A (en) 1978-11-21
FR2289980B1 (sv) 1979-05-04
DE2559952B1 (de) 1980-11-20
DE2527056A1 (de) 1976-01-02
SE424624B (sv) 1982-08-02
AU8212875A (en) 1976-12-16
SE7506677L (sv) 1975-12-22
AU499009B2 (en) 1979-04-05
SE418720B (sv) 1981-06-22
SE449598B (sv) 1987-05-11
IT1040627B (it) 1979-12-20
SE449599B (sv) 1987-05-11
SE422671B (sv) 1982-03-22
GB1488745A (en) 1977-10-12
JPS5861100A (ja) 1983-04-11
FR2309939A1 (fr) 1976-11-26
SE7808631L (sv) 1978-08-15
US3946358A (en) 1976-03-23
JPS6253051B2 (sv) 1987-11-09

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