BE899646A - Dispositif pour avertir le pilote d'un avion durant l'atterrissage. - Google Patents
Dispositif pour avertir le pilote d'un avion durant l'atterrissage.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
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)
- Alarm Systems (AREA)
- Traffic Control Systems (AREA)
- Apparatus For Radiation Diagnosis (AREA)
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.
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 (fr) | 1984-11-12 |
Family
ID=23965111
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE0/212924A BE899646A (fr) | 1983-05-13 | 1984-05-11 | Dispositif pour avertir le pilote d'un avion durant l'atterrissage. |
Country Status (14)
| Country | Link |
|---|---|
| JP (1) | JPS59216792A (fr) |
| AU (2) | AU547843B2 (fr) |
| BE (1) | BE899646A (fr) |
| CH (1) | CH657819A5 (fr) |
| DE (1) | DE3417829A1 (fr) |
| ES (1) | ES532433A0 (fr) |
| FI (1) | FI74254C (fr) |
| FR (1) | FR2545929B1 (fr) |
| GB (1) | GB2140757B (fr) |
| GR (1) | GR82059B (fr) |
| IT (1) | IT1177720B (fr) |
| NL (1) | NL8401532A (fr) |
| NZ (1) | NZ207653A (fr) |
| SE (1) | SE8402470L (fr) |
Families Citing this family (3)
| 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 |
| US12525136B2 (en) | 2023-06-08 | 2026-01-13 | Honeywell International Inc. | Avionic system and method for selectively preventing and enhanced ground proximity warning system alert mode from generating an alert |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3988713A (en) * | 1974-06-19 | 1976-10-26 | Sundstrand Data Control, Inc. | Aircraft ground proximity warning instrument |
| US3946358A (en) * | 1974-06-19 | 1976-03-23 | 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 |
| CA1033828A (fr) * | 1976-06-14 | 1978-06-27 | Litton Industries | Systeme numerique permettant de reduire le nombre de fausses alarmes a l'approche du sol |
| GB1567553A (en) * | 1976-06-14 | 1980-05-14 | Litton Industries Inc | Digital ground proximity warning systems |
| FR2343223A1 (fr) * | 1976-07-01 | 1977-09-30 | Trt Telecom Radio Electr | Filtrage des alarmes dans un systeme de surveillance de la proximite du sol |
| 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 |
-
1984
- 1984-03-27 NZ NZ207653A patent/NZ207653A/en unknown
- 1984-04-10 AU AU26690/84A patent/AU547843B2/en not_active Ceased
- 1984-04-27 CH CH2080/84A patent/CH657819A5/fr not_active IP Right Cessation
- 1984-05-08 GR GR74647A patent/GR82059B/el unknown
- 1984-05-08 SE SE8402470A patent/SE8402470L/xx not_active Application Discontinuation
- 1984-05-09 GB GB08411771A patent/GB2140757B/en not_active Expired
- 1984-05-09 AU AU27820/84A patent/AU549796B2/en not_active Ceased
- 1984-05-10 JP JP59091972A patent/JPS59216792A/ja active Pending
- 1984-05-11 FR FR8407319A patent/FR2545929B1/fr not_active Expired
- 1984-05-11 NL NL8401532A patent/NL8401532A/nl not_active Application Discontinuation
- 1984-05-11 FI FI841913A patent/FI74254C/fi not_active IP Right Cessation
- 1984-05-11 ES ES532433A patent/ES532433A0/es active Granted
- 1984-05-11 BE BE0/212924A patent/BE899646A/fr not_active IP Right Cessation
- 1984-05-11 IT IT48180/84A patent/IT1177720B/it active
- 1984-05-14 DE DE3417829A patent/DE3417829A1/de active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| NL8401532A (nl) | 1984-12-03 |
| AU2669084A (en) | 1984-11-15 |
| DE3417829C2 (fr) | 1989-02-23 |
| IT1177720B (it) | 1987-08-26 |
| DE3417829A1 (de) | 1984-11-15 |
| IT8448180A0 (it) | 1984-05-11 |
| AU549796B2 (en) | 1986-02-13 |
| ES8502933A1 (es) | 1985-02-01 |
| CH657819A5 (fr) | 1986-09-30 |
| SE8402470L (sv) | 1984-11-14 |
| FI74254B (fi) | 1987-09-30 |
| GB2140757B (en) | 1986-12-03 |
| GR82059B (fr) | 1984-12-13 |
| FI841913A0 (fi) | 1984-05-11 |
| AU2782084A (en) | 1984-11-15 |
| FI841913L (fi) | 1984-11-14 |
| FI74254C (fi) | 1988-01-11 |
| ES532433A0 (es) | 1985-02-01 |
| JPS59216792A (ja) | 1984-12-06 |
| NZ207653A (en) | 1987-11-27 |
| FR2545929A1 (fr) | 1984-11-16 |
| SE8402470D0 (sv) | 1984-05-08 |
| GB8411771D0 (en) | 1984-06-13 |
| IT8448180A1 (it) | 1985-11-11 |
| FR2545929B1 (fr) | 1988-04-15 |
| GB2140757A (en) | 1984-12-05 |
| AU547843B2 (en) | 1985-11-07 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US4551723A (en) | Excessive descent rate warning system for rotary wing aircraft | |
| US5187478A (en) | Configuration responsive descent rate warning system for aircraft | |
| FR2416837A1 (fr) | Dispositif d'avertissement de vitesse de descente excessive pour un aeronef | |
| BE899879A (fr) | Dispositif avertisseur d'inclinaison excessive pour aeronef a aile rotative. | |
| BE899642A (fr) | Dispositif d'avertissement pour avion. | |
| US4818992A (en) | Excessive altitude loss after take-off warning system for rotary wing aircraft | |
| WO1986004983A1 (fr) | Systeme d'avertissement pour aeronefs sensible a leur configuration concernant la vitesse descensionnelle | |
| EP0217852A1 (fr) | Systeme d'avertissement d'approche du sol pour aeronefs a enveloppe modifiee sur la base de la vitesse descensionnelle. | |
| BE899646A (fr) | Dispositif pour avertir le pilote d'un avion durant l'atterrissage. | |
| US4639730A (en) | Excessive terrain closure warning system | |
| BE899643A (fr) | Dispositif d'avertissement de proximite du sol pour avion. | |
| BE899645A (fr) | Dispositif d'avertissement pour le pilote d'un avion en pique. | |
| BE899647A (fr) | Dispositif d'avertissement du pilote lors de l'atterrissage. | |
| AU567260B2 (en) | Excessive descent rate warning system for tactical aircraft | |
| NEWARK | AIRCRAFT ACCIDENT REPORT! | |
| KLINGNER | Problems pertaining to aeronautical technology in the case of rescue operations with helicopters in mountainous areas | |
| SPLETTSTOESSER et al. | Helicopter noise certification and sensitivity studies along the procedural lines of the new ICAO Annex 16/Chapter 8 regulations | |
| Phelan | Calculated landings | |
| MICCICHE et al. | HASEP- Survival from crashed Navy helicopters | |
| FRIEDERICY | Development, testing and evaluation of a night vision goggle compatible BO-105 for night low level operation | |
| Barwood | Principles and problems of high speed ejection | |
| GB433873A (en) | Aeroplane landing systems employing electromagnetic waves |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RE | Patent lapsed |
Owner name: SUNDSTRAND DATA CONTROL INC. Effective date: 19880531 |