BE899646A - DEVICE FOR ADVISING THE PILOT OF AN AIRPLANE DURING LANDING. - Google Patents

DEVICE FOR ADVISING THE PILOT OF AN AIRPLANE DURING LANDING.

Info

Publication number
BE899646A
BE899646A BE0/212924A BE212924A BE899646A BE 899646 A BE899646 A BE 899646A BE 0/212924 A BE0/212924 A BE 0/212924A BE 212924 A BE212924 A BE 212924A BE 899646 A BE899646 A BE 899646A
Authority
BE
Belgium
Prior art keywords
pilot
aircraft
during landing
advising
speed
Prior art date
Application number
BE0/212924A
Other languages
French (fr)
Inventor
S Paterson N
E Vermilion E
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 BE899646A publication Critical patent/BE899646A/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

Abstract

Le dispositif est agencé pour transmettre au pilote d'un avion de combat un avertissement acoustique si lors de l'atterissage la vitesse de descente de l'avion est excessive pour l'altitude à laquelle il se trouve. Ce dispositif surveille la vitesse de descente lorsque le train d'atterrissage est abaissé, que la vitesse relative est inférieure à 540 km/h et que les armes ne sont pas armées, et émet un signal d'avertissement acoustique lorsque la vitesse de descente barométrique excède une limite de sécurité prédéterminée dépendant de l'altitude radio de l'avion.The device is arranged to transmit to the pilot of a combat aircraft an acoustic warning if during landing the speed of descent of the aircraft is excessive for the altitude at which it is located. This device monitors the descent speed when the landing gear is lowered, the relative speed is less than 540 km / h and the weapons are not armed, and emits an acoustic warning signal when the barometric descent speed exceeds a predetermined safety limit depending on the radio altitude of the aircraft.

BE0/212924A 1983-05-13 1984-05-11 DEVICE FOR ADVISING THE PILOT OF AN AIRPLANE DURING LANDING. BE899646A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US49459383A 1983-05-13 1983-05-13

Publications (1)

Publication Number Publication Date
BE899646A true BE899646A (en) 1984-11-12

Family

ID=23965111

Family Applications (1)

Application Number Title Priority Date Filing Date
BE0/212924A BE899646A (en) 1983-05-13 1984-05-11 DEVICE FOR ADVISING THE PILOT OF AN AIRPLANE DURING LANDING.

Country Status (14)

Country Link
JP (1) JPS59216792A (en)
AU (2) AU547843B2 (en)
BE (1) BE899646A (en)
CH (1) CH657819A5 (en)
DE (1) DE3417829A1 (en)
ES (1) ES8502933A1 (en)
FI (1) FI74254C (en)
FR (1) FR2545929B1 (en)
GB (1) GB2140757B (en)
GR (1) GR82059B (en)
IT (1) IT1177720B (en)
NL (1) NL8401532A (en)
NZ (1) NZ207653A (en)
SE (1) SE8402470L (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IL76204A0 (en) * 1984-09-06 1985-12-31 Sundstrand Data Control Excessive descent rate warning system for tactical aircraft
US4999262A (en) * 1990-04-20 1991-03-12 Hughes Aircraft Company Multilayer cathode current collector/container for a battery

Family Cites Families (8)

* 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
US3988713A (en) * 1974-06-19 1976-10-26 Sundstrand Data Control, Inc. Aircraft ground proximity warning instrument
US3936796A (en) * 1974-06-19 1976-02-03 Sundstrand Data Control, Inc. Aircraft ground proximity warning instrument
GB1567553A (en) * 1976-06-14 1980-05-14 Litton Industries Inc Digital ground proximity warning systems
CA1033828A (en) * 1976-06-14 1978-06-27 Litton Industries Digital ground proximity system for reducing false warnings
FR2343223A1 (en) * 1976-07-01 1977-09-30 Trt Telecom Radio Electr FILTERING OF ALARMS IN A SOIL PROXIMITY MONITORING 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

Also Published As

Publication number Publication date
DE3417829A1 (en) 1984-11-15
IT8448180A0 (en) 1984-05-11
AU2782084A (en) 1984-11-15
FI74254C (en) 1988-01-11
AU549796B2 (en) 1986-02-13
FI841913A (en) 1984-11-14
FR2545929A1 (en) 1984-11-16
AU547843B2 (en) 1985-11-07
JPS59216792A (en) 1984-12-06
GB8411771D0 (en) 1984-06-13
CH657819A5 (en) 1986-09-30
GR82059B (en) 1984-12-13
NZ207653A (en) 1987-11-27
AU2669084A (en) 1984-11-15
FR2545929B1 (en) 1988-04-15
SE8402470L (en) 1984-11-14
IT1177720B (en) 1987-08-26
FI74254B (en) 1987-09-30
ES532433A0 (en) 1985-02-01
GB2140757B (en) 1986-12-03
SE8402470D0 (en) 1984-05-08
NL8401532A (en) 1984-12-03
FI841913A0 (en) 1984-05-11
GB2140757A (en) 1984-12-05
ES8502933A1 (en) 1985-02-01
DE3417829C2 (en) 1989-02-23

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Legal Events

Date Code Title Description
RE Patent lapsed

Owner name: SUNDSTRAND DATA CONTROL INC.

Effective date: 19880531