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ES8607158A1 - System for alerting a pilot of a dangerous flight profile during low level maneuvering - Google Patents

System for alerting a pilot of a dangerous flight profile during low level maneuvering

Info

Publication number
ES8607158A1
ES8607158A1 ES541246A ES541246A ES8607158A1 ES 8607158 A1 ES8607158 A1 ES 8607158A1 ES 541246 A ES541246 A ES 541246A ES 541246 A ES541246 A ES 541246A ES 8607158 A1 ES8607158 A1 ES 8607158A1
Authority
ES
Spain
Prior art keywords
pilot
ground
alerting
low level
during low
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.)
Expired
Application number
ES541246A
Other languages
Spanish (es)
Other versions
ES541246A0 (en
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.)
Sundstrand Data Control Inc
Original Assignee
Sundstrand Data Control Inc
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 Inc filed Critical Sundstrand Data Control Inc
Publication of ES541246A0 publication Critical patent/ES541246A0/en
Publication of ES8607158A1 publication Critical patent/ES8607158A1/en
Expired legal-status Critical Current

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
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P1/00—Details of instruments
    • G01P1/07—Indicating devices, e.g. for remote indication
    • G01P1/08—Arrangements of scales, pointers, lamps or acoustic indicators, e.g. in automobile speedometers
    • G01P1/10—Arrangements of scales, pointers, lamps or acoustic indicators, e.g. in automobile speedometers for indicating predetermined speeds

Landscapes

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

Abstract

INSTALACION AVISADORA PARA PONER EN ALERTA AL PILOTO DE UN AVION CERCA DE UNA CONDICION DE VUELO PELIGROSA TRAS EL DESPEGUE Y DURANTE MANIOBRAS A POCA ALTURA SOBRE EL SUELO. CONSTA DE UN ALTIMETRO BAROMETRICO (12) QUE SUMINISTRA UNA SEÑAL REPRESENTATIVA DE LA ALTURA DEL AVION SOBRE EL SUELO; DE UN DISPOSITIVO DE ALMACENAJE SENSIBLE AL ALTIMETRO SUMINISTRADOR DE LA SEÑAL DE ALTURA SOBRE EL SUELO, PARA ALMACENAR UNA INDICACION DE LA MAXIMA ALTURA SOBRE EL SUELO ALCANZADA DESPUES DEL DESPEGUE; DE UN CIRCUITO INDICADOR (14) DE LA VARIACION DE LA ALTITUD BAROMETRICA; DE UN RADIOALTIMETRO (16); DE UNA PLATAFORMA GIROSCOPICA (18).WARNING INSTALLATION TO ALERT THE PILOT OF AN AIRCRAFT NEAR A DANGEROUS FLIGHT CONDITION AFTER TAKEOFF AND DURING MANEUVERS AT LOW HEIGHT ABOVE THE GROUND. IT CONSISTS OF A BAROMETRIC ALTIMETER (12) WHICH PROVIDES A SIGNAL REPRESENTATIVE OF THE HEIGHT OF THE AIRPLANE ABOVE THE GROUND; OF A STORAGE DEVICE SENSITIVE TO THE ALTIMETER SUPPLYING THE HEIGHT ABOVE THE GROUND SIGNAL, TO STORE AN INDICATION OF THE MAXIMUM HEIGHT ABOVE THE GROUND REACHED AFTER TAKEOFF; OF AN INDICATOR CIRCUIT (14) OF THE VARIATION OF THE BAROMETRIC ALTITUDE; OF A RADIO ALTIMETER (16); OF A GYROSCOPIC PLATFORM (18).

ES541246A 1983-05-13 1985-03-14 System for alerting a pilot of a dangerous flight profile during low level maneuvering Expired ES8607158A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US49459083A 1983-05-13 1983-05-13

Publications (2)

Publication Number Publication Date
ES541246A0 ES541246A0 (en) 1986-05-16
ES8607158A1 true ES8607158A1 (en) 1986-05-16

Family

ID=23965099

Family Applications (2)

Application Number Title Priority Date Filing Date
ES532430A Expired ES8506523A1 (en) 1983-05-13 1984-05-11 System for alerting a pilot of a dangerous flight profile during low level maneuvering
ES541246A Expired ES8607158A1 (en) 1983-05-13 1985-03-14 System for alerting a pilot of a dangerous flight profile during low level maneuvering

Family Applications Before (1)

Application Number Title Priority Date Filing Date
ES532430A Expired ES8506523A1 (en) 1983-05-13 1984-05-11 System for alerting a pilot of a dangerous flight profile during low level maneuvering

Country Status (15)

Country Link
JP (1) JPS59216795A (en)
AU (2) AU548709B2 (en)
BE (1) BE899643A (en)
CA (1) CA1234417A (en)
CH (1) CH660156A5 (en)
DE (1) DE3417884A1 (en)
ES (2) ES8506523A1 (en)
FI (1) FI74251C (en)
FR (1) FR2550334B1 (en)
GB (2) GB2139588B (en)
GR (1) GR82062B (en)
IL (1) IL71348A (en)
IT (1) IT1177721B (en)
NL (1) NL8401531A (en)
SE (1) SE8402467L (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5001476A (en) * 1983-05-13 1991-03-19 Sundstrand Data Control, Inc. Warning system for tactical 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
DE3621052A1 (en) * 1986-06-24 1988-01-07 Aerodata Flugmesstechnik Gmbh Device for the automatic flight path guidance of aircraft along a guidance beam
CH671555A5 (en) * 1986-09-10 1989-09-15 Zermatt Air Ag
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
US5864307A (en) * 1996-02-19 1999-01-26 Gec Marconi Limited Aircraft terrain advisory system
FR2749676B1 (en) * 1996-06-11 1998-09-11 Sextant Avionique ALTITUDE MANAGEMENT METHOD AND SYSTEM FOR AERODYNE
US8155804B2 (en) 2007-10-12 2012-04-10 Airbus Operations Gmbh Device and method for providing a flight status signal
DE102007048956B4 (en) * 2007-10-12 2019-02-14 Airbus Operations Gmbh Apparatus and method for providing a flight status signal
US8086361B2 (en) * 2007-12-12 2011-12-27 Honeywell International Inc. Advisory system to aid pilot recovery from spatial disorientation during an excessive roll
EP2592381A1 (en) 2011-11-08 2013-05-15 EADS Construcciones Aeronauticas, S.A. Discrete signal consolidation device and method and aircraft with said device

Family Cites Families (5)

* 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
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
US3947808A (en) * 1975-01-13 1976-03-30 Sundstrand Data Control, Inc. Excessive descent rate warning system for aircraft
GB1567553A (en) * 1976-06-14 1980-05-14 Litton Industries Inc Digital ground proximity warning systems
US4319218A (en) * 1980-01-04 1982-03-09 Sundstrand Corporation Negative climb after take-off warning system with configuration warning means

Also Published As

Publication number Publication date
GB2139588B (en) 1987-04-15
FR2550334A1 (en) 1985-02-08
FI841910L (en) 1984-11-14
AU548709B2 (en) 1986-01-02
FR2550334B1 (en) 1988-04-15
GB2175264A (en) 1986-11-26
GB2139588A (en) 1984-11-14
ES541246A0 (en) 1986-05-16
GB8411768D0 (en) 1984-06-13
CA1234417A (en) 1988-03-22
BE899643A (en) 1984-11-12
JPS59216795A (en) 1984-12-06
GB8611002D0 (en) 1986-06-11
SE8402467D0 (en) 1984-05-08
SE8402467L (en) 1984-11-14
IT1177721B (en) 1987-08-26
GR82062B (en) 1984-12-13
DE3417884C2 (en) 1990-04-19
ES532430A0 (en) 1985-08-01
FI74251B (en) 1987-09-30
ES8506523A1 (en) 1985-08-01
GB2175264B (en) 1987-04-15
FI841910A0 (en) 1984-05-11
AU5506786A (en) 1986-08-14
FI74251C (en) 1988-01-11
DE3417884A1 (en) 1984-12-13
IT8448181A0 (en) 1984-05-11
AU2668784A (en) 1984-11-15
CH660156A5 (en) 1987-03-31
IL71348A (en) 1989-09-10
NL8401531A (en) 1984-12-03

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Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 19971201