BE899876A - Installation d'alarme pour avion tactique a aile tournante. - Google Patents
Installation d'alarme pour avion tactique a aile tournante.Info
- Publication number
- BE899876A BE899876A BE0/213110A BE213110A BE899876A BE 899876 A BE899876 A BE 899876A BE 0/213110 A BE0/213110 A BE 0/213110A BE 213110 A BE213110 A BE 213110A BE 899876 A BE899876 A BE 899876A
- Authority
- BE
- Belgium
- Prior art keywords
- aircraft
- alarm
- ground
- rotating wing
- alarm installation
- 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)
- Traffic Control Systems (AREA)
- Arrangements For Transmission Of Measured Signals (AREA)
Abstract
L'installation d'alarme pour aéronef à aile tournante surveille l'altitude au-dessus du sol de l'avion et donne une alarme lorsque l'avion vole à distance insuffisante au sol. Deux alarmes distinctes sont donnés. L'une indique la distance insuffisante du sol et l'autre avertit le pilote s'il essaie d'atterrir sans sortir le train d'atterrissage. Un circuit logique est prévu pour modifier les critères nécessaires pour produire l'alarme et pour bloquer certaines alarmes selon le mode d'opération de l'avion.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US50321683A | 1983-06-10 | 1983-06-10 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE899876A true BE899876A (fr) | 1984-12-10 |
Family
ID=24001189
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE0/213110A BE899876A (fr) | 1983-06-10 | 1984-06-08 | Installation d'alarme pour avion tactique a aile tournante. |
Country Status (14)
| Country | Link |
|---|---|
| JP (1) | JPS608196A (fr) |
| AU (1) | AU548266B2 (fr) |
| BE (1) | BE899876A (fr) |
| CA (1) | CA1240771A (fr) |
| CH (1) | CH660159A5 (fr) |
| DE (1) | DE3421517A1 (fr) |
| FI (1) | FI841931A7 (fr) |
| FR (1) | FR2553507B1 (fr) |
| GB (1) | GB2141683B (fr) |
| GR (1) | GR81645B (fr) |
| IT (1) | IT1179182B (fr) |
| NL (1) | NL8401856A (fr) |
| NZ (1) | NZ207888A (fr) |
| SE (1) | SE8403093L (fr) |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3944968A (en) * | 1974-11-01 | 1976-03-16 | Sundstrand Data Control, Inc. | Aircraft ground proximity warning system having speed versus altitude compensation |
| IL48315A (en) * | 1975-03-18 | 1978-08-31 | United Technologies Corp | Warning system for helicopters for avoiding tail contact during landing |
| US4030065A (en) * | 1976-07-19 | 1977-06-14 | Sundstrand Corporation | Terrain clearance warning system for aircraft |
| JPS53114981A (en) * | 1977-03-17 | 1978-10-06 | Santo Tekkosho Kk | Continuous fabric conveying apparatus |
| US4567483A (en) * | 1982-12-10 | 1986-01-28 | Sundstrand Data Control, Inc. | Position based ground proximity warning system for aircraft |
-
1984
- 1984-04-06 CA CA000451452A patent/CA1240771A/fr not_active Expired
- 1984-04-18 NZ NZ207888A patent/NZ207888A/en unknown
- 1984-05-14 FI FI841931A patent/FI841931A7/fi not_active Application Discontinuation
- 1984-05-14 FR FR8407408A patent/FR2553507B1/fr not_active Expired
- 1984-05-21 GB GB08412991A patent/GB2141683B/en not_active Expired
- 1984-05-30 AU AU28842/84A patent/AU548266B2/en not_active Ceased
- 1984-06-06 CH CH2762/84A patent/CH660159A5/fr not_active IP Right Cessation
- 1984-06-07 IT IT48342/84A patent/IT1179182B/it active
- 1984-06-07 GR GR74951A patent/GR81645B/el unknown
- 1984-06-08 BE BE0/213110A patent/BE899876A/fr not_active IP Right Cessation
- 1984-06-08 SE SE8403093A patent/SE8403093L/ not_active Application Discontinuation
- 1984-06-08 JP JP59116819A patent/JPS608196A/ja active Pending
- 1984-06-08 DE DE3421517A patent/DE3421517A1/de not_active Ceased
- 1984-06-12 NL NL8401856A patent/NL8401856A/nl not_active Application Discontinuation
Also Published As
| Publication number | Publication date |
|---|---|
| GB2141683B (en) | 1986-10-15 |
| IT8448342A0 (it) | 1984-06-07 |
| IT8448342A1 (it) | 1985-12-07 |
| NL8401856A (nl) | 1985-01-02 |
| SE8403093D0 (sv) | 1984-06-08 |
| DE3421517A1 (de) | 1984-12-13 |
| FI841931L (fi) | 1984-12-11 |
| CH660159A5 (fr) | 1987-03-31 |
| CA1240771A (fr) | 1988-08-16 |
| FR2553507A1 (fr) | 1985-04-19 |
| GR81645B (fr) | 1984-12-11 |
| GB2141683A (en) | 1985-01-03 |
| AU2884284A (en) | 1984-12-13 |
| FI841931A7 (fi) | 1984-12-11 |
| JPS608196A (ja) | 1985-01-17 |
| AU548266B2 (en) | 1985-12-05 |
| FI841931A0 (fi) | 1984-05-14 |
| IT1179182B (it) | 1987-09-16 |
| FR2553507B1 (fr) | 1988-11-10 |
| GB8412991D0 (en) | 1984-06-27 |
| NZ207888A (en) | 1987-11-27 |
| SE8403093L (sv) | 1984-12-11 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| BE899878A (fr) | Installation d'alarme d'une descente excessive pour avion a aile tournante. | |
| BE899879A (fr) | Dispositif avertisseur d'inclinaison excessive pour aeronef a aile rotative. | |
| BE899877A (fr) | Installation d'alarme d'une perte d'altitude excessive apres decollage d'un avion a aile tournante. | |
| BE899643A (fr) | Dispositif d'avertissement de proximite du sol pour avion. | |
| BE899876A (fr) | Installation d'alarme pour avion tactique a aile tournante. | |
| IT8448177A0 (it) | Sistema per avvisare il pilota di un aereo di eccessiva velocita' di avvicinamento al suolo | |
| IT8448179A0 (it) | Sistema per avvisare il pilota di un aereo di un atterraggio con il carrello sollevato | |
| NORITAKE | A METHOD TO ESTIMATE AIRPORT RUNWAY CAPACITY | |
| IT8448180A0 (it) | Sistema per avvisare il pilota di un aereo tattico di eccessiva velocita' discensionale | |
| VANTUIJL | Orienting description of air traffic control in the Netherlands | |
| COLLINS | Mastering the systems- Air traffic control and weather(Book) | |
| PARKS | Automated Pilot Advisory System[Final Report] | |
| SULLIVAN et al. | On the cost benefits of air cushion landing gear to civil aviation | |
| ANOLL et al. | Heliport VFR airspace design based on helicopter performance(Final Report) | |
| SARTER et al. | The Flight Management System-'Rumors and facts' | |
| SPRINGS | PILOT PROFICIENCY | |
| Hearne | All-weather Helicopter Operation | |
| MOMIYAMA | Project NAVTOLAND(Navy vertical takeoff and landing capability development) | |
| Hearne | Part I Engineering Aspects | |
| SCHRAGE et al. | The integration of knowledge-based expert system and rotorcraft simulation models | |
| Reid | Part II Piloting Aspects | |
| JONES | Math model study, runway 16 R instrument landing system localizer at Seattle-Tacoma Airport, Washington[Data Report, period ending Aug. 1980] | |
| Commissions | Radar | |
| MOKROWIECKI | VASI-S- A visual landing aid | |
| FR2548133B1 (fr) | Structure d'aile pour aeronefs ultralegers |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RE | Patent lapsed |
Owner name: SUNDSTRAND DATA CONTROL INC. Effective date: 19890630 |