CA2253899A1 - Systeme indicateur d'acceleration au decollage pour aeronef - Google Patents
Systeme indicateur d'acceleration au decollage pour aeronef Download PDFInfo
- Publication number
- CA2253899A1 CA2253899A1 CA002253899A CA2253899A CA2253899A1 CA 2253899 A1 CA2253899 A1 CA 2253899A1 CA 002253899 A CA002253899 A CA 002253899A CA 2253899 A CA2253899 A CA 2253899A CA 2253899 A1 CA2253899 A1 CA 2253899A1
- Authority
- CA
- Canada
- Prior art keywords
- aircraft
- takeoff
- airspeed
- acceleration
- needle
- 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.)
- Abandoned
Links
- 230000001133 acceleration Effects 0.000 title claims abstract description 39
- 230000003466 anti-cipated effect Effects 0.000 claims description 3
- 230000000750 progressive effect Effects 0.000 claims 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- XDXHAEQXIBQUEZ-UHFFFAOYSA-N Ropinirole hydrochloride Chemical compound Cl.CCCN(CCC)CCC1=CC=CC2=C1CC(=O)N2 XDXHAEQXIBQUEZ-UHFFFAOYSA-N 0.000 description 1
- VPNMENGBDCZKOE-LNYNQXPHSA-N [(1R,5S)-8-methyl-8-azabicyclo[3.2.1]octan-3-yl] 3-hydroxy-2-phenylpropanoate [(1S,2S,4R,5R)-9-methyl-3-oxa-9-azatricyclo[3.3.1.02,4]nonan-7-yl] (2S)-3-hydroxy-2-phenylpropanoate (1R,3S)-1,2,2-trimethylcyclopentane-1,3-dicarboxylic acid Chemical compound CC1(C)[C@H](CC[C@@]1(C)C(O)=O)C(O)=O.CC1(C)[C@H](CC[C@@]1(C)C(O)=O)C(O)=O.CN1[C@H]2CC[C@@H]1CC(C2)OC(=O)C(CO)c1ccccc1.CN1[C@H]2CC(C[C@@H]1[C@H]1O[C@@H]21)OC(=O)[C@H](CO)c1ccccc1 VPNMENGBDCZKOE-LNYNQXPHSA-N 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 244000045947 parasite Species 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D43/00—Arrangements or adaptations of instruments
- B64D43/02—Arrangements or adaptations of instruments for indicating aircraft speed or stalling conditions
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C23/00—Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/04—Control of altitude or depth
- G05D1/06—Rate of change of altitude or depth
- G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
- G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
- G05D1/0661—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for take-off
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Traffic Control Systems (AREA)
Abstract
L'invention concerne un système d'instrument aéronautique informant le pilote si la vitesse d'accélération de l'aéronef durant le roulement au décollage est suffisante pour atteindre la vitesse V1 au moment voulu (et donc sur la distance voulue), et si tel n'est pas le cas, de la distance correspondant au retard de l'aéronef sur le programme d'accélération requis.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA002253899A CA2253899A1 (fr) | 1997-04-11 | 1997-10-22 | Systeme indicateur d'acceleration au decollage pour aeronef |
Applications Claiming Priority (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA2,202,409 | 1997-04-11 | ||
| CA002202409A CA2202409C (fr) | 1997-04-11 | 1997-04-11 | Circuit anemometrique howgozit |
| CA002253899A CA2253899A1 (fr) | 1997-04-11 | 1997-10-22 | Systeme indicateur d'acceleration au decollage pour aeronef |
| PCT/CA1997/000785 WO1998047056A1 (fr) | 1997-04-11 | 1997-10-22 | Systeme indicateur d'acceleration au decollage pour aeronef |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA2253899A1 true CA2253899A1 (fr) | 1998-10-22 |
Family
ID=29550702
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002253899A Abandoned CA2253899A1 (fr) | 1997-04-11 | 1997-10-22 | Systeme indicateur d'acceleration au decollage pour aeronef |
Country Status (1)
| Country | Link |
|---|---|
| CA (1) | CA2253899A1 (fr) |
-
1997
- 1997-10-22 CA CA002253899A patent/CA2253899A1/fr not_active Abandoned
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request | ||
| FZDE | Discontinued |