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IT1177721B - DANGEROUS FLIGHT CONDITION WARNING SYSTEM OF AN AIRCRAFT AFTER NECK AND DURING LOW ALTITUDE MANEUVER - Google Patents

DANGEROUS FLIGHT CONDITION WARNING SYSTEM OF AN AIRCRAFT AFTER NECK AND DURING LOW ALTITUDE MANEUVER

Info

Publication number
IT1177721B
IT1177721B IT48181/84A IT4818184A IT1177721B IT 1177721 B IT1177721 B IT 1177721B IT 48181/84 A IT48181/84 A IT 48181/84A IT 4818184 A IT4818184 A IT 4818184A IT 1177721 B IT1177721 B IT 1177721B
Authority
IT
Italy
Prior art keywords
aircraft
neck
warning system
during low
flight condition
Prior art date
Application number
IT48181/84A
Other languages
Italian (it)
Other versions
IT8448181A0 (en
Inventor
Noel S Paterson
Everette E Vermilion
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 IT8448181A0 publication Critical patent/IT8448181A0/en
Application granted granted Critical
Publication of IT1177721B publication Critical patent/IT1177721B/en

Links

Classifications

    • 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
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P1/00Details of instruments
    • G01P1/07Indicating devices, e.g. for remote indication
    • G01P1/08Arrangements of scales, pointers, lamps or acoustic indicators, e.g. in automobile speedometers
    • G01P1/10Arrangements 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)
IT48181/84A 1983-05-13 1984-05-11 DANGEROUS FLIGHT CONDITION WARNING SYSTEM OF AN AIRCRAFT AFTER NECK AND DURING LOW ALTITUDE MANEUVER IT1177721B (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
IT8448181A0 IT8448181A0 (en) 1984-05-11
IT1177721B true IT1177721B (en) 1987-08-26

Family

ID=23965099

Family Applications (1)

Application Number Title Priority Date Filing Date
IT48181/84A IT1177721B (en) 1983-05-13 1984-05-11 DANGEROUS FLIGHT CONDITION WARNING SYSTEM OF AN AIRCRAFT AFTER NECK AND DURING LOW ALTITUDE MANEUVER

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
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
ES8607158A1 (en) 1986-05-16
NL8401531A (en) 1984-12-03

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