ES8502932A1 - Una instalacion avisadora para dar aviso al piloto de un avion tactico si el avion tiene una tasa excesiva de acercamiento con respecto al terreno - Google Patents
Una instalacion avisadora para dar aviso al piloto de un avion tactico si el avion tiene una tasa excesiva de acercamiento con respecto al terrenoInfo
- Publication number
- ES8502932A1 ES8502932A1 ES532432A ES532432A ES8502932A1 ES 8502932 A1 ES8502932 A1 ES 8502932A1 ES 532432 A ES532432 A ES 532432A ES 532432 A ES532432 A ES 532432A ES 8502932 A1 ES8502932 A1 ES 8502932A1
- Authority
- ES
- Spain
- Prior art keywords
- terrain
- aircraft
- warning
- flying
- warning system
- 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
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
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Emergency Alarm Devices (AREA)
- Radar Systems Or Details Thereof (AREA)
- Braking Arrangements (AREA)
- Navigation (AREA)
- Traffic Control Systems (AREA)
Abstract
INSTALACION AVISADORA PARA DAR AVISO AL PILOTO DE UN AVION TACTICO SI EL AVION TIENE UNA TASA EXCESIVA DE ACERCAMIENTO CON RESPECTO AL TERRENO.EL CIRCUITO CONSTA DE: UN RADIOALTIMETRO (12), CIRCUITO DE TASA DE VARIACION DE LA ALTURA (14), FUENTE DE SEN/ALES (18) DE VELOCIDAD AERODINAMICA, CONTROL DE ARMAS MONTADAS (20), Y UN ELEMENTO DISCRETO DE SI HAY PESO EN RUEDAS. LA PUERTA (22) DA UNA SEN/AL HABILITADORA A LA PUERTA (24), SI LAS ARMAS NO ESTAN MONTADAS (20) VELOCIDAD ES SUPERIOR A 200 NUDOS (18, 26) Y EL RADIOALTIMETRO NO ESTA INHIBIDO. ADEMAS A LA PUERTA (24) LLEGAN SEN/ALES DEL COMPARADOR DE MODALIDAD (28) Y DE UNO DE ALTITUD (30) QUE COMPARA LA ALTURA DEL RADIOALTIMETRO CON 30 M HABILITANDO LA PUERTA SI ES MAYOR. EL COMPARADOR (28) INICIA EL AVISO QUE GENERA EN DOS FASES EL GENERADOR (32).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/494,591 US4639730A (en) | 1983-05-13 | 1983-05-13 | Excessive terrain closure warning system |
Publications (2)
Publication Number | Publication Date |
---|---|
ES8502932A1 true ES8502932A1 (es) | 1985-02-01 |
ES532432A0 ES532432A0 (es) | 1985-02-01 |
Family
ID=23965104
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES532432A Granted ES532432A0 (es) | 1983-05-13 | 1984-05-11 | Una instalacion avisadora para dar aviso al piloto de un avion tactico si el avion tiene una tasa excesiva de acercamiento con respecto al terreno |
Country Status (17)
Country | Link |
---|---|
US (1) | US4639730A (es) |
JP (1) | JPS59216796A (es) |
AU (1) | AU547722B2 (es) |
BE (1) | BE899644A (es) |
CA (1) | CA1241081A (es) |
CH (1) | CH657820A5 (es) |
DE (1) | DE3417830A1 (es) |
ES (1) | ES532432A0 (es) |
FI (1) | FI74252C (es) |
FR (1) | FR2545928B1 (es) |
GB (2) | GB2140368B (es) |
GR (1) | GR82060B (es) |
IL (1) | IL71349A (es) |
IT (1) | IT1177717B (es) |
NL (1) | NL8401533A (es) |
NZ (1) | NZ207651A (es) |
SE (1) | SE8402468L (es) |
Families Citing this family (11)
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 |
CA1243118A (en) * | 1985-02-22 | 1988-10-11 | Michael M. Grove | Aircraft terrain closure warning system with descent rate based envelope modification |
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 |
JP3251489B2 (ja) * | 1996-02-16 | 2002-01-28 | シャープ株式会社 | 座標入力装置 |
US6469660B1 (en) | 2000-04-13 | 2002-10-22 | United Parcel Service Inc | Method and system for displaying target icons correlated to target data integrity |
EP1299742A2 (en) | 2000-07-10 | 2003-04-09 | United Parcel Service Of America, Inc. | Method for determining conflicting paths between mobile airbone vehicles and associated system |
CN1476593A (zh) * | 2000-10-25 | 2004-02-18 | 美国联合包装服务有限公司 | 用于座舱交通显示的飞行员可编程高度范围过滤器 |
US7386373B1 (en) * | 2003-01-07 | 2008-06-10 | Garmin International, Inc. | System, method and apparatus for searching geographic area using prioritized spatial order |
US6745115B1 (en) | 2003-01-07 | 2004-06-01 | Garmin Ltd. | System, method and apparatus for searching geographic area using prioritized spacial order |
US7382287B1 (en) | 2003-06-03 | 2008-06-03 | Garmin International, Inc | Avionics system, method and apparatus for selecting a runway |
US6980892B1 (en) | 2003-11-18 | 2005-12-27 | Garmin International, Inc. | Avionics system and method for providing altitude alerts during final landing approach |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3703844A (en) * | 1970-12-02 | 1972-11-28 | Us Air Force | Arming unit |
US3934211A (en) * | 1973-03-09 | 1976-01-20 | Westinghouse Electric Corporation | Metal halide vapor laser |
US3946358A (en) * | 1974-06-19 | 1976-03-23 | Sundstrand Data Control, Inc. | Aircraft ground proximity warning instrument |
US3958218A (en) * | 1974-10-03 | 1976-05-18 | Sundstrand Data Control, Inc. | Aircraft ground proximity warning system with speed compensation |
US3944968A (en) * | 1974-11-01 | 1976-03-16 | Sundstrand Data Control, Inc. | Aircraft ground proximity warning system having speed versus altitude compensation |
US3958219A (en) * | 1975-03-06 | 1976-05-18 | Sundstrand Data Control, Inc. | Terrain closure warning system with altitude rate signal conditioning |
US3934221A (en) * | 1975-03-06 | 1976-01-20 | Sundstrand Data Control, Inc. | Terrain closure warning system with altitude rate signal conditioning |
US3934222A (en) * | 1975-04-02 | 1976-01-20 | Sundstrand Data Control, Inc. | Terrain closure warning system with climb inhibit and altitude gain measurement |
US4030065A (en) * | 1976-07-19 | 1977-06-14 | Sundstrand Corporation | Terrain clearance warning system for aircraft |
US4215334A (en) * | 1978-02-09 | 1980-07-29 | Sundstrand Data Control, Inc. | Aircraft excessive descent rate warning system |
US4319218A (en) * | 1980-01-04 | 1982-03-09 | Sundstrand Corporation | Negative climb after take-off warning system with configuration warning means |
US4551723A (en) * | 1983-06-10 | 1985-11-05 | Sundstrand Data Control, Inc. | Excessive descent rate warning system for rotary wing aircraft |
-
1983
- 1983-05-13 US US06/494,591 patent/US4639730A/en not_active Expired - Lifetime
-
1984
- 1984-03-14 CA CA000449620A patent/CA1241081A/en not_active Expired
- 1984-03-26 IL IL71349A patent/IL71349A/xx unknown
- 1984-03-27 NZ NZ207651A patent/NZ207651A/en unknown
- 1984-04-10 AU AU26686/84A patent/AU547722B2/en not_active Ceased
- 1984-04-27 CH CH2082/84A patent/CH657820A5/fr not_active IP Right Cessation
- 1984-05-08 GR GR74648A patent/GR82060B/el unknown
- 1984-05-08 SE SE8402468A patent/SE8402468L/ not_active Application Discontinuation
- 1984-05-09 GB GB08411769A patent/GB2140368B/en not_active Expired
- 1984-05-10 JP JP59091970A patent/JPS59216796A/ja active Pending
- 1984-05-11 NL NL8401533A patent/NL8401533A/nl not_active Application Discontinuation
- 1984-05-11 ES ES532432A patent/ES532432A0/es active Granted
- 1984-05-11 BE BE0/212922A patent/BE899644A/fr not_active IP Right Cessation
- 1984-05-11 FI FI841911A patent/FI74252C/fi not_active IP Right Cessation
- 1984-05-11 IT IT48177/84A patent/IT1177717B/it active
- 1984-05-11 FR FR8407318A patent/FR2545928B1/fr not_active Expired
- 1984-05-14 DE DE19843417830 patent/DE3417830A1/de active Granted
- 1984-11-14 GB GB08428727A patent/GB2148224B/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
SE8402468L (sv) | 1984-11-14 |
FI841911A (fi) | 1984-11-14 |
AU2668684A (en) | 1984-11-15 |
US4639730A (en) | 1987-01-27 |
GB2140368A (en) | 1984-11-28 |
SE8402468D0 (sv) | 1984-05-08 |
DE3417830C2 (es) | 1989-02-23 |
CA1241081A (en) | 1988-08-23 |
ES532432A0 (es) | 1985-02-01 |
FI74252C (fi) | 1988-01-11 |
FR2545928A1 (fr) | 1984-11-16 |
FI74252B (fi) | 1987-09-30 |
GB2148224B (en) | 1986-04-09 |
JPS59216796A (ja) | 1984-12-06 |
BE899644A (fr) | 1984-11-12 |
GB2148224A (en) | 1985-05-30 |
NZ207651A (en) | 1988-02-12 |
CH657820A5 (fr) | 1986-09-30 |
GB2140368B (en) | 1986-04-09 |
GB8411769D0 (en) | 1984-06-13 |
IT8448177A0 (it) | 1984-05-11 |
FI841911A0 (fi) | 1984-05-11 |
AU547722B2 (en) | 1985-10-31 |
DE3417830A1 (de) | 1984-11-15 |
FR2545928B1 (fr) | 1987-09-11 |
GB8428727D0 (en) | 1984-12-27 |
IL71349A (en) | 1989-10-31 |
NL8401533A (nl) | 1984-12-03 |
IT1177717B (it) | 1987-08-26 |
GR82060B (es) | 1984-12-13 |
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