ES8506523A1 - 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 maneuveringInfo
- Publication number
- ES8506523A1 ES8506523A1 ES532430A ES532430A ES8506523A1 ES 8506523 A1 ES8506523 A1 ES 8506523A1 ES 532430 A ES532430 A ES 532430A ES 532430 A ES532430 A ES 532430A ES 8506523 A1 ES8506523 A1 ES 8506523A1
- Authority
- ES
- Spain
- Prior art keywords
- pilot
- alerting
- low level
- during low
- profile during
- 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
Links
- 230000007704 transition Effects 0.000 abstract 1
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
DISPOSITIVO PARA DAR UN AVISO AL PILOTO DE UN AVION QUE MANIOBRA CERCA DEL SUELO.COMPRENDE UNA PUERTA (20), QUE DA SEN/AL INICIAL A OTRAS DOS (22, 24), JUNTAMENTE CON LAS SEN/ALES PROCEDENTES DEL ALTIMETRO BAROMETRICO (12), EL CIRCUITO (14) DE TASA DE VARIACION BAROMETRICA Y EL RADICALTIMETRO (16). LA CONDICION DE QUE EL AVION SE HALLA EN FASE DE APROXIMACION, VIENE DADA POR TRES PUERTAS (26, 28, 30) Y UN BIESTABLE (32). EXISTE UN DETECTOR DE TRANSICION (36) QUE ACTIVA UN BIESTABLE (34), EL CUAL ACTUA SOBRE UN CONMUTADOR (389, ASI COMO UN COMPARADOR (40), UN CIRCUITO GRADUADOR (42) Y UN ACUMULADOR (44) DE ALTURA RADIOALTIMETRICA.DEVICE FOR GIVING A WARNING TO THE PILOT OF AN AIRCRAFT MANEUVERING NEAR THE GROUND. IT INCLUDES A DOOR (20), WHICH GIVES INITIAL SIGNAL TO TWO OTHERS (22, 24), TOGETHER WITH THE SIGNALS FROM THE BAROMETRIC ALTIMETER (12 ), THE CIRCUIT (14) OF BAROMETRIC VARIATION RATE AND THE RADICALTIMETER (16). THE CONDITION THAT THE PLANE IS IN THE APPROACH PHASE IS GIVEN BY THREE DOORS (26, 28, 30) AND A FLIP-UP (32). THERE IS A TRANSITION DETECTOR (36) THAT ACTIVATES A FLIP-OFF (34), WHICH ACTS ON A SWITCH (389, AS WELL AS A COMPARATOR (40), A GRADING CIRCUIT (42) AND A RADIOALTIMETRICAL HEIGHT ACCUMULATOR (44).
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US49459083A | 1983-05-13 | 1983-05-13 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| ES532430A0 ES532430A0 (en) | 1985-08-01 |
| ES8506523A1 true ES8506523A1 (en) | 1985-08-01 |
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 After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES541246A Expired ES8607158A1 (en) | 1983-05-13 | 1985-03-14 | 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)
| 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)
| 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 |
-
1984
- 1984-03-14 CA CA000449619A patent/CA1234417A/en not_active Expired
- 1984-03-26 IL IL71348A patent/IL71348A/en unknown
- 1984-04-10 AU AU26687/84A patent/AU548709B2/en not_active Ceased
- 1984-04-27 CH CH2085/84A patent/CH660156A5/en not_active IP Right Cessation
- 1984-05-08 GR GR74651A patent/GR82062B/el unknown
- 1984-05-08 SE SE8402467A patent/SE8402467L/en not_active Application Discontinuation
- 1984-05-09 GB GB08411768A patent/GB2139588B/en not_active Expired
- 1984-05-10 JP JP59091969A patent/JPS59216795A/en active Pending
- 1984-05-11 NL NL8401531A patent/NL8401531A/en not_active Application Discontinuation
- 1984-05-11 FI FI841910A patent/FI74251C/en not_active IP Right Cessation
- 1984-05-11 IT IT48181/84A patent/IT1177721B/en active
- 1984-05-11 BE BE0/212921A patent/BE899643A/en not_active IP Right Cessation
- 1984-05-11 FR FR8407322A patent/FR2550334B1/en not_active Expired
- 1984-05-11 ES ES532430A patent/ES8506523A1/en not_active Expired
- 1984-05-14 DE DE3417884A patent/DE3417884A1/en active Granted
-
1985
- 1985-03-14 ES ES541246A patent/ES8607158A1/en not_active Expired
-
1986
- 1986-03-24 AU AU55067/86A patent/AU5506786A/en not_active Abandoned
- 1986-05-06 GB GB08611002A patent/GB2175264B/en not_active Expired
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 |
| 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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