SE8403093L - WARNING SYSTEM FOR A TACTICAL AIRPLANE WITH ROTATING WINGS - Google Patents
WARNING SYSTEM FOR A TACTICAL AIRPLANE WITH ROTATING WINGSInfo
- Publication number
- SE8403093L SE8403093L SE8403093A SE8403093A SE8403093L SE 8403093 L SE8403093 L SE 8403093L SE 8403093 A SE8403093 A SE 8403093A SE 8403093 A SE8403093 A SE 8403093A SE 8403093 L SE8403093 L SE 8403093L
- Authority
- SE
- Sweden
- Prior art keywords
- warning
- aircraft
- warning system
- tactical
- airplane
- 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
A warning system for rotary wing aircraft that monitors the altitude above ground of the aircraft and issues a warning when there is insufficient terrain clearance. The warning criteria are optimized for rotary wing aircraft and are altered as a function of landing gear position and airspeed. Two distinct warnings are given. One indicates insufficient terrain clearance and the other warns the pilot if he attempts to land with the landing gear up. Logic circuitry is provided to modify the criteria necessary to generate a warning, and to inhibit certain warnings, as required by the mode of operation of the aircraft. <IMAGE>
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US50321683A | 1983-06-10 | 1983-06-10 |
Publications (2)
Publication Number | Publication Date |
---|---|
SE8403093D0 SE8403093D0 (en) | 1984-06-08 |
SE8403093L true SE8403093L (en) | 1984-12-11 |
Family
ID=24001189
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE8403093A SE8403093L (en) | 1983-06-10 | 1984-06-08 | WARNING SYSTEM FOR A TACTICAL AIRPLANE WITH ROTATING WINGS |
Country Status (14)
Country | Link |
---|---|
JP (1) | JPS608196A (en) |
AU (1) | AU548266B2 (en) |
BE (1) | BE899876A (en) |
CA (1) | CA1240771A (en) |
CH (1) | CH660159A5 (en) |
DE (1) | DE3421517A1 (en) |
FI (1) | FI841931A (en) |
FR (1) | FR2553507B1 (en) |
GB (1) | GB2141683B (en) |
GR (1) | GR81645B (en) |
IT (1) | IT1179182B (en) |
NL (1) | NL8401856A (en) |
NZ (1) | NZ207888A (en) |
SE (1) | SE8403093L (en) |
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/en not_active Expired
- 1984-04-18 NZ NZ207888A patent/NZ207888A/en unknown
- 1984-05-14 FR FR8407408A patent/FR2553507B1/en not_active Expired
- 1984-05-14 FI FI841931A patent/FI841931A/en not_active Application Discontinuation
- 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/en not_active IP Right Cessation
- 1984-06-07 IT IT48342/84A patent/IT1179182B/en active
- 1984-06-07 GR GR74951A patent/GR81645B/el unknown
- 1984-06-08 BE BE0/213110A patent/BE899876A/en not_active IP Right Cessation
- 1984-06-08 DE DE3421517A patent/DE3421517A1/en not_active Ceased
- 1984-06-08 JP JP59116819A patent/JPS608196A/en active Pending
- 1984-06-08 SE SE8403093A patent/SE8403093L/en not_active Application Discontinuation
- 1984-06-12 NL NL8401856A patent/NL8401856A/en not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
GB2141683B (en) | 1986-10-15 |
FI841931A0 (en) | 1984-05-14 |
GB8412991D0 (en) | 1984-06-27 |
FI841931A (en) | 1984-12-11 |
SE8403093D0 (en) | 1984-06-08 |
BE899876A (en) | 1984-12-10 |
IT1179182B (en) | 1987-09-16 |
AU548266B2 (en) | 1985-12-05 |
AU2884284A (en) | 1984-12-13 |
CA1240771A (en) | 1988-08-16 |
NL8401856A (en) | 1985-01-02 |
IT8448342A0 (en) | 1984-06-07 |
DE3421517A1 (en) | 1984-12-13 |
FR2553507B1 (en) | 1988-11-10 |
JPS608196A (en) | 1985-01-17 |
FR2553507A1 (en) | 1985-04-19 |
NZ207888A (en) | 1987-11-27 |
GB2141683A (en) | 1985-01-03 |
CH660159A5 (en) | 1987-03-31 |
GR81645B (en) | 1984-12-11 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
NAV | Patent application has lapsed |
Ref document number: 8403093-1 Effective date: 19881028 |