SE8100890L - Markvarnande anordning for flygplan - Google Patents

Markvarnande anordning for flygplan

Info

Publication number
SE8100890L
SE8100890L SE8100890A SE8100890A SE8100890L SE 8100890 L SE8100890 L SE 8100890L SE 8100890 A SE8100890 A SE 8100890A SE 8100890 A SE8100890 A SE 8100890A SE 8100890 L SE8100890 L SE 8100890L
Authority
SE
Sweden
Prior art keywords
aircraft
warning
signal
slide
glide
Prior art date
Application number
SE8100890A
Other languages
English (en)
Other versions
SE422671B (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 SE8100890L publication Critical patent/SE8100890L/sv
Publication of SE422671B publication Critical patent/SE422671B/sv

Links

Classifications

    • GPHYSICS
    • G08SIGNALLING
    • G08GTRAFFIC CONTROL SYSTEMS
    • G08G5/00Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0017Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information
    • G08G5/0021Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information located in the aircraft
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C5/00Measuring height; Measuring distances transverse to line of sight; Levelling between separated points; Surveyors' levels
    • G01C5/005Measuring height; Measuring distances transverse to line of sight; Levelling between separated points; Surveyors' levels altimeters for aircraft
    • GPHYSICS
    • G08SIGNALLING
    • G08GTRAFFIC CONTROL SYSTEMS
    • G08G5/00Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/02Automatic approach or landing aids, i.e. systems in which flight data of incoming planes are processed to provide landing data
    • G08G5/025Navigation or guidance aids

Landscapes

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

Claims (1)

1. PATENT KRAV Varningsinstrument inrattat att Ora piloten i en flygfarkost uppmarksam pA ett tillstAnd as ej onskad narhet till marken vid en flygplats, som Sr utrustad med en sanclare for glidbaneradiostralesilken strAle innefattar giltig och syn- barligen giltig stignings- och sjunkningsinformation, varvid instrumentet innefattar en i flygfarkosten forefintlig mottagare (37), som hr pAverkbar i beroende as glidbaneradiostrAlen far alstring as en signal (G/S) son representerar riktningen och storleken has vinkelavvikelse fOr flygfarkostens loge over eller under den medelst glidbaneradiostrAlen bestgmda glidbanan, en i beroende as signalen frAn mottagaren (37) pAverkbar detektor (87) far detektering as en, en avvikelse under glidbanan indikerande avvikelsesignal, som representerar ett tillstAnd under glidbanan averstigande ett faststgllt vgrde, varvid detektorn ar anordnad att alstra en, en yarning am att flygfarkosten befinner sig under glidbanan initierande signal, och en hajdsignalkalla (26) far alstring av en signal, som representerar flygfarkostens hajd, en i beroende as hajdsignalkallan (26) pAverkbar konditioneringskrets (88-91) inrgttad att som.funktion as Widen variera dot faststallda vgrdet far tillstAndet under glidbanan far att konditionera detektorn (87) till att alstra den en yarning om att flygfarkosten befinner sig under glidbanan initierande signalen, en kretsanOrdning (86) inrgttad att, ngr flygfarkosten befinner sig under en farutbestamd hajd, inhibera den en yarning am att flygfarkosten befinner sig under glidbanan initierande signalen, och en kretsanordning (52), som or kopplad far att vara pAverkbar i k ---ende as den en v--,ing on att flygfarkosten befinner sig under glidbanan mittle signalen i o.r att aktivera en pilotvarningsanord- ning (54),kannetecknat as att en summeringsanordning (73) or kopplad Giver, fOr flygplane- tillstAnd Varnings-tillstAnds-detektorer FIG. I Barometerhojdmatare Negativ etigning after start Hojdmatare Sakerhets Glidbanemottagare Alit fOr h8g ejunkningshaetighet Varning I Vingklaffar Alit for hog haetighet mot marken Landningsstall m emn 0 74 — Test i luften Varningeenhet 54 Under G/S atm arrIonmrr. Markteet.Seek FD Markt. 240 m/min RS 64 4X 6 /GX * 204.0„in -145 m 72 1:1 I Negativ stigningehaatighet 07FS hRf2ln m
SE8100890A 1974-06-19 1981-02-09 Varningsinstrument i flygfarkost SE422671B (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
SE8100890L true SE8100890L (sv) 1981-02-09
SE422671B SE422671B (sv) 1982-03-22

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
SE8100890A SE422671B (sv) 1974-06-19 1981-02-09 Varningsinstrument i flygfarkost
SE8100891A SE449598B (sv) 1974-06-19 1981-02-09 Markvarnande instrument for flygplan
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 (2)

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

Family Applications After (3)

Application Number Title Priority Date Filing Date
SE8100891A SE449598B (sv) 1974-06-19 1981-02-09 Markvarnande instrument for flygplan
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

Country Status (9)

Country Link
US (1) US3946358A (sv)
JP (2) JPS5934560B2 (sv)
AU (2) AU499009B2 (sv)
CA (1) CA1043005A (sv)
DE (2) DE2527056C3 (sv)
FR (2) FR2309939A1 (sv)
GB (2) GB1488744A (sv)
IT (1) IT1040627B (sv)
SE (6) SE418720B (sv)

Families Citing this family (63)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3946358A (en) 1974-06-19 1976-03-23 Sundstrand Data Control, Inc. Aircraft ground proximity warning instrument
JPS5174333A (en) * 1974-12-23 1976-06-28 Honda Motor Co Ltd Sharyoni okeru keihosochi
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
US4016565A (en) * 1975-09-15 1977-04-05 Rockwell International Corporation Aircraft ground closure rate filtering method and means
US4071894A (en) * 1976-06-28 1978-01-31 Rockwell International Corporation Profile warning generator with anticipation of warning condition
FR2343223A1 (fr) * 1976-07-01 1977-09-30 Trt Telecom Radio Electr Filtrage des alarmes dans un systeme de surveillance de la proximite du sol
US4030065A (en) * 1976-07-19 1977-06-14 Sundstrand Corporation Terrain clearance warning system for aircraft
US4060793A (en) * 1976-07-19 1977-11-29 Sundstrand Data Control, Inc. Excessive sink rate warning system for aircraft
JPS544172U (sv) * 1977-06-11 1979-01-11
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
US4189777A (en) * 1978-05-01 1980-02-19 The Bendix Corporation Ground proximity warning system with means for altering warning threshold in accordance with wind shear
US4319218A (en) * 1980-01-04 1982-03-09 Sundstrand Corporation Negative climb after take-off warning system with configuration warning means
US4495483A (en) * 1981-04-30 1985-01-22 Sundstrand Corporation Ground proximity warning system with time based mode switching
US4433323A (en) * 1982-02-04 1984-02-21 Sundstrand Data Control, Inc. Ground proximity warning system with time and altitude based mode switching
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
US4567483A (en) * 1982-12-10 1986-01-28 Sundstrand Data Control, Inc. Position based ground proximity warning system for aircraft
CA1234417A (en) * 1983-05-13 1988-03-22 Noel S. Paterson System for alerting a pilot of a dangerous flight profile during low level maneuvering
US4639730A (en) * 1983-05-13 1987-01-27 Sundstrand Data Control, Inc. Excessive terrain closure warning system
NZ207653A (en) * 1983-05-13 1987-11-27 Sundstrand Data Control Excessive descent rate warning system for aircraft
US5001476A (en) * 1983-05-13 1991-03-19 Sundstrand Data Control, Inc. Warning system for tactical aircraft
US4939513A (en) * 1983-05-13 1990-07-03 Sundstrand Data Control, Inc. System for alerting a pilot of a dangerous flight profile during low level maneuvering
US4951047A (en) * 1983-05-13 1990-08-21 Sunstrand Data Control, Inc. Negative climb after take-off warning system
US4551723A (en) * 1983-06-10 1985-11-05 Sundstrand Data Control, Inc. Excessive descent rate warning system for rotary wing aircraft
US4980684A (en) * 1983-06-10 1990-12-25 Sundstrand Data Controls, Inc. Warning system for tactical rotary wing aircraft
US4818992A (en) * 1983-06-10 1989-04-04 Sundstrand Data Control, Inc. Excessive altitude loss after take-off 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
CA1243405A (en) * 1985-02-22 1988-10-18 Michael M. Grove Configuration responsive descent rate warning system for aircraft
IL77860A0 (en) * 1985-02-22 1986-09-30 Sundstrand Data Control Ground proximity warning system for aircraft
US5187478A (en) * 1985-02-22 1993-02-16 Sundstrand Corporation Configuration responsive descent rate warning system for aircraft
CA1243117A (en) * 1985-02-22 1988-10-11 Michael M. Grove Altitude loss after take-off warning system utilizing time and altitude
CA1243118A (en) * 1985-02-22 1988-10-11 Michael M. Grove Aircraft terrain closure warning system with descent rate based envelope modification
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
US5136512A (en) * 1988-06-26 1992-08-04 Cubic Defense Systems, Inc. Ground collision avoidance system
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
US5225829A (en) * 1991-05-09 1993-07-06 Sundstrand Corporation Independent low airspeed alert
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
US6043758A (en) * 1996-02-12 2000-03-28 Alliedsignal Inc. Terrain warning system
US6008742A (en) * 1997-05-21 1999-12-28 Groves; Duane Aircraft landing gear warning system
ATE269572T1 (de) 1998-10-16 2004-07-15 Universal Avionics Sys Corp Warnungsverfahren und -system für flugpläne
US6421603B1 (en) 1999-08-11 2002-07-16 Honeywell International Inc. Hazard detection for a travel plan
US6622066B2 (en) * 2001-01-23 2003-09-16 Yasuo Ishihara EGPWS cutoff altitude for helicopters
EP1407226A1 (en) * 2001-07-17 2004-04-14 Honeywell International Inc. Pitch angle alerting device for ground proximity warning systems (gpws)
GB2387912A (en) * 2002-04-26 2003-10-29 Messier Dowty Inc Monitoring parameters in structural components
US7633410B2 (en) * 2004-02-19 2009-12-15 Honeywell International Inc. Wireless assisted recovery systems and methods
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
RU2449922C1 (ru) * 2010-11-15 2012-05-10 Открытое акционерное общество Московский научно-производственный комплекс "Авионика" имени О.В. Успенского (ОАО МНПК "Авионика") Способ автоматического управления самолетом при заходе на посадку
US8554396B2 (en) * 2012-01-03 2013-10-08 Honeywell International Inc. Systems and methods for issuing a hard landing warning and providing maintenance advisories for hard landing incidents
US9284047B2 (en) * 2013-08-02 2016-03-15 Goodrich Corporation Routings for articulated landing gear
US10089634B2 (en) 2015-10-27 2018-10-02 C Kirk Nance Method to recover non-recognized errors in aircraft weight determinations to increase weight and center of gravity limitations for regulated aircraft
US9751636B2 (en) 2015-12-15 2017-09-05 International Business Machines Corporation Dynamic detection of landing gear deployment
FR3072490B1 (fr) * 2017-10-17 2019-11-08 Airbus Operations (S.A.S.) Systeme et procede d'aide a l'atterrissage d'un aeronef

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB866125A (en) 1958-07-16 1961-04-26 Secr Aviation Improvements in or relating to warning devices for aircraft
US3052427A (en) * 1960-07-08 1962-09-04 Sperry Rand Corp Flare-out system for aircraft
US3169730A (en) * 1962-11-01 1965-02-16 Sperry Rand Corp Flight control system
US3355733A (en) * 1964-10-19 1967-11-28 Bell Aerospace Corp Designated area instrument landing system
US3327973A (en) * 1965-06-14 1967-06-27 Lear Siegler Inc Automatic landing pitch axis control system for aircraft
GB1178842A (en) * 1966-01-29 1970-01-21 Elliott Brothers London Ltd Improvements in and relating to the Control of Aircraft
US3743221A (en) * 1970-04-09 1973-07-03 Lear Siegler Inc Aircraft flight control apparatus
US3652835A (en) * 1970-05-14 1972-03-28 Sperry Rand Corp Aircraft glide slope coupler system
US3715718A (en) 1970-08-11 1973-02-06 Sundstrand Data Control Ground proximity warning system utilizing radio and barometric altimeter combination
US3658280A (en) * 1970-10-29 1972-04-25 Mc Donnell Douglas Corp Altitude and glide slope track controller
US3757338A (en) * 1971-02-05 1973-09-04 Bendix Corp Glide slope lock-out network
US3847328A (en) * 1972-01-31 1974-11-12 Boeing Co Automatic go-around control system for aircraft
US3801049A (en) * 1972-01-31 1974-04-02 Boeing Co Automatic approach landing and go-around pitch axis control system for aircraft
US3860800A (en) * 1972-06-19 1975-01-14 Boeing Co Automatic pitch axis control system for aircraft
US3946358A (en) 1974-06-19 1976-03-23 Sundstrand Data Control, Inc. Aircraft ground proximity warning instrument

Also Published As

Publication number Publication date
AU499009B2 (en) 1979-04-05
GB1488744A (en) 1977-10-12
SE422671B (sv) 1982-03-22
JPS5934560B2 (ja) 1984-08-23
DE2527056C3 (de) 1979-10-11
JPS5114699A (en) 1976-02-05
FR2289980B1 (sv) 1979-05-04
FR2309939A1 (fr) 1976-11-26
DE2527056A1 (de) 1976-01-02
DE2527056B2 (de) 1979-02-15
JPS6253051B2 (sv) 1987-11-09
SE449598B (sv) 1987-05-11
SE8100892L (sv) 1981-02-09
JPS5861100A (ja) 1983-04-11
AU511815B2 (en) 1980-09-04
SE8100889L (sv) 1981-02-09
DE2559952C3 (de) 1981-07-02
FR2289980A1 (fr) 1976-05-28
SE449599B (sv) 1987-05-11
SE8100891L (sv) 1981-02-09
AU4266578A (en) 1979-04-05
SE418720B (sv) 1981-06-22
SE7808631L (sv) 1978-08-15
DE2559952B1 (de) 1980-11-20
AU8212875A (en) 1976-12-16
FR2309939B1 (sv) 1980-07-25
GB1488745A (en) 1977-10-12
US3946358A (en) 1976-03-23
SE7506677L (sv) 1975-12-22
SE422715B (sv) 1982-03-22
IT1040627B (it) 1979-12-20
SE424624B (sv) 1982-08-02
CA1043005A (en) 1978-11-21

Similar Documents

Publication Publication Date Title
SE8100890L (sv) Markvarnande anordning for flygplan
US5666110A (en) Helicopter enhanced descent after take-off warning for GPWS
SE427825B (sv) Anordning for varning vid alltfor hog sjunkhastighet for flygfarkost
CA1205167A (en) Ground proximity warning system with time and altitude based mode switching
CA1255794A (en) Vertical windshear detection for aircraft
RU2302359C2 (ru) Способ и устройство для обнаружения ухудшения характеристик летательного аппарата
US5781126A (en) Ground proximity warning system and methods for rotary wing aircraft
US5187478A (en) Configuration responsive descent rate warning system for aircraft
US10358232B2 (en) Detecting that a rotorcraft is approaching a vortex domain, and signaling that detection
RU2730814C2 (ru) Способ интеллектуальной информационной поддержки экипажа вертолета по высотно-скоростным параметрам и параметрам воздушной среды, окружающей вертолет, и устройство для его осуществления
US5038141A (en) Configuration responsive descent rate warning system for aircraft
FI74250B (fi) Varningssystem foer negativ stigning efter start.
US4769645A (en) Excessive pitch attitude warning system for rotary wing aircraft
GB2141087A (en) Excessive altitude loss after take-off warning system for rotary wing aircraft
GB921216A (en) Aircraft take-off safety indicating device
FI74252C (sv) Varningssystem för för nära belägen terräng.
US20040193333A1 (en) Low airspeed assist algorithm for air data computer applications
FI74247C (sv) Varningssystem för flygplan, som landar med landningsstället uppfällt .
AU567260B2 (en) Excessive descent rate warning system for tactical aircraft
US3348412A (en) Altitude measurement
FI74254C (sv) Varningssystem för för hög sjunkhastighet för ett taktiskt flygplan.
Rade Requirements for operation of light helicopters at night and in poor visibility
CA1241083A (en) System for alerting a pilot of a dangerous flight profile during low level maneuvering
Garfield IV—Radio Altimetry
Funk Measurements of Atmospheric Turbulence on Seattle-Alaska Airways

Legal Events

Date Code Title Description
NUG Patent has lapsed

Ref document number: 8100890-6

Effective date: 19890725

Format of ref document f/p: F