FR2900385B1 - Procede et dispositif d'aide au pilotage d'un giravion au decollage. - Google Patents
Procede et dispositif d'aide au pilotage d'un giravion au decollage.Info
- Publication number
- FR2900385B1 FR2900385B1 FR0603828A FR0603828A FR2900385B1 FR 2900385 B1 FR2900385 B1 FR 2900385B1 FR 0603828 A FR0603828 A FR 0603828A FR 0603828 A FR0603828 A FR 0603828A FR 2900385 B1 FR2900385 B1 FR 2900385B1
- Authority
- FR
- France
- Prior art keywords
- giravion
- aiding
- steering
- take
- 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 - Fee Related
Links
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- 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
- G05D1/0669—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for take-off specially adapted for vertical take-off
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0603828A FR2900385B1 (fr) | 2006-04-28 | 2006-04-28 | Procede et dispositif d'aide au pilotage d'un giravion au decollage. |
US11/790,971 US7756612B2 (en) | 2006-04-28 | 2007-04-30 | Method and a device for providing assistance in piloting a rotorcraft at takeoff |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0603828A FR2900385B1 (fr) | 2006-04-28 | 2006-04-28 | Procede et dispositif d'aide au pilotage d'un giravion au decollage. |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2900385A1 FR2900385A1 (fr) | 2007-11-02 |
FR2900385B1 true FR2900385B1 (fr) | 2008-12-26 |
Family
ID=37663288
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0603828A Expired - Fee Related FR2900385B1 (fr) | 2006-04-28 | 2006-04-28 | Procede et dispositif d'aide au pilotage d'un giravion au decollage. |
Country Status (2)
Country | Link |
---|---|
US (1) | US7756612B2 (fr) |
FR (1) | FR2900385B1 (fr) |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2916421B1 (fr) * | 2007-05-22 | 2010-04-23 | Eurocopter France | Systeme de commande d'un giravion. |
US8275500B2 (en) * | 2008-03-11 | 2012-09-25 | Honeywell International Inc. | Gas turbine engine fixed collective takeoff compensation control system and method |
US9014944B2 (en) * | 2009-06-18 | 2015-04-21 | United Technologies Corporation | Turbine engine speed and vibration sensing system |
US8360369B2 (en) * | 2009-11-24 | 2013-01-29 | Merlin Technology, Inc. | Emergency collective actuator and method for a helicopter |
US8651425B2 (en) | 2009-11-24 | 2014-02-18 | Merlin Technology Inc. | Emergency collective actuator and method for a helicopter |
WO2011078847A1 (fr) * | 2009-12-21 | 2011-06-30 | The Boeing Company | Calcul et affichage de la vitesse limite pour un contrôle de la poussée asymétrique |
JP5832352B2 (ja) * | 2012-03-29 | 2015-12-16 | 三菱重工業株式会社 | 垂直離着陸機のトルク推定装置、垂直離着陸機、垂直離着陸機のトルク推定プログラム、及び垂直離着陸機のトルク推定方法 |
US20140336849A1 (en) * | 2013-05-08 | 2014-11-13 | Honeywell International Inc. | System and method for displaying rate-of-climb on an avionics vertical speed indicator |
US9567091B2 (en) | 2013-06-06 | 2017-02-14 | Bell Helicopter Textron Inc. | System and method for maximizing aircraft safe landing capability during one engine inoperative operation |
US9856017B2 (en) * | 2013-06-11 | 2018-01-02 | Bell Helicopter Textron Inc. | Torque based method of limiting vertical axis augmentation |
US9221535B2 (en) * | 2013-09-18 | 2015-12-29 | Honeywell International Inc. | Adaptive remaining useful life balancing control system and method for multi-engine systems |
FR3023261B1 (fr) * | 2014-07-03 | 2016-07-01 | Airbus Helicopters | Methode de regulation de la vitesses de rotation du rotor principal d'un giravion multi-moteur en cas de panne de l'un des moteurs |
FR3028839B1 (fr) | 2014-11-26 | 2016-11-18 | Airbus Helicopters | Methode d'assistance a la navigation d'un giravion multimoteur en cas de panne moteur, dans le cadre d'un entrainement a vitesse variable d'un rotor principal du giravion |
US9957041B2 (en) | 2015-05-21 | 2018-05-01 | Merlin Technology, Inc. | Advanced emergency collective actuator with friction pull-off and method for a helicopter |
US10035609B2 (en) | 2016-03-08 | 2018-07-31 | Harris Corporation | Wireless engine monitoring system for environmental emission control and aircraft networking |
CA2972498C (fr) | 2017-06-28 | 2024-01-23 | Bombardier Inc. | Systeme et methode d'orientation d'inclinaison au decollage |
US10816971B2 (en) * | 2018-02-12 | 2020-10-27 | Textron Innovations Inc. | Autopilot recoupling for rotorcraft |
US10747235B2 (en) * | 2018-04-25 | 2020-08-18 | The Boeing Company | Pitch trim prediction for aircraft |
US11092136B2 (en) * | 2018-05-04 | 2021-08-17 | Raytheon Technologies Corporation | Systems and methods for optimal speed protection for power turbine governing |
FR3081597B1 (fr) | 2018-05-24 | 2021-07-30 | Airbus Helicopters | Procede et dispositif de determination et d'affichage d'une distance de securite d'un giravion en prenant en compte la hauteur des vagues |
US11725597B2 (en) | 2019-02-08 | 2023-08-15 | Pratt & Whitney Canada Corp. | System and method for exiting an asymmetric engine operating regime |
FR3123315A1 (fr) | 2021-05-31 | 2022-12-02 | Airbus Helicopters | Procédé d’assistance au pilotage d’un giravion comportant au moins deux moteurs |
CN113942653B (zh) * | 2021-11-19 | 2023-04-25 | 中国直升机设计研究所 | 一种双发高速直升机变旋翼转速控制方法 |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1161408A (en) * | 1965-11-03 | 1969-08-13 | Sperry Rand Ltd | Take-Off Director |
US3927306A (en) * | 1974-03-29 | 1975-12-16 | Sperry Rand Corp | Helicopter flight path control |
US4628455A (en) * | 1983-05-06 | 1986-12-09 | Sperry Corporation | Cross axis torque limiter for helicopter autopilot |
US5727754A (en) * | 1995-08-31 | 1998-03-17 | Cartercopters, L.L.C. | Gyroplane |
WO1997020734A2 (fr) * | 1995-12-06 | 1997-06-12 | Mc Donnell Douglas Corporation | Systeme de commandes de vol pour aeronef de formule hybride triple propulse par reaction |
US5853152A (en) * | 1997-04-29 | 1998-12-29 | Sikorsky Aircraft Corporation | Collective detent system for vertical takeoff flight operations |
FR2772718B1 (fr) | 1997-12-22 | 2000-02-11 | Eurocopter France | Indicateur de pilotage pour aeronef |
US6584382B2 (en) * | 2000-05-17 | 2003-06-24 | Abraham E. Karem | Intuitive vehicle and machine control |
FR2830630B1 (fr) * | 2001-10-05 | 2004-07-30 | Eurocopter France | Dispositif de pilotage automatique d'un helicoptere et systeme de pilotage automatique comportant un tel dispositif |
US6527225B1 (en) * | 2002-04-30 | 2003-03-04 | Sikorsky Aircraft Corporation | Method for performing an automated category a takeoff |
US6885917B2 (en) * | 2002-11-07 | 2005-04-26 | The Boeing Company | Enhanced flight control systems and methods for a jet powered tri-mode aircraft |
US7463956B2 (en) * | 2003-07-03 | 2008-12-09 | The Boeing Company | Constant vertical state maintaining cueing system |
US6824097B1 (en) * | 2003-08-27 | 2004-11-30 | The Boeing Company | Vertical takeoff and landing aircraft |
US7604198B2 (en) * | 2003-09-25 | 2009-10-20 | Petersen Bruce L | Rotorcraft having coaxial counter-rotating rotors which produce both vertical and horizontal thrust and method of controlled flight in all six degrees of freedom |
-
2006
- 2006-04-28 FR FR0603828A patent/FR2900385B1/fr not_active Expired - Fee Related
-
2007
- 2007-04-30 US US11/790,971 patent/US7756612B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR2900385A1 (fr) | 2007-11-02 |
US20080161983A1 (en) | 2008-07-03 |
US7756612B2 (en) | 2010-07-13 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CD | Change of name or company name |
Owner name: AIRBUS HELICOPTERS, FR Effective date: 20140602 |
|
PLFP | Fee payment |
Year of fee payment: 11 |
|
PLFP | Fee payment |
Year of fee payment: 12 |
|
PLFP | Fee payment |
Year of fee payment: 13 |
|
PLFP | Fee payment |
Year of fee payment: 14 |
|
PLFP | Fee payment |
Year of fee payment: 15 |
|
PLFP | Fee payment |
Year of fee payment: 16 |
|
PLFP | Fee payment |
Year of fee payment: 17 |
|
ST | Notification of lapse |
Effective date: 20231205 |