ITTO20040050A1 - Dispositivo indicatore di un margine di potenza residua di motori a turbina di velivoli - Google Patents

Dispositivo indicatore di un margine di potenza residua di motori a turbina di velivoli

Info

Publication number: ITTO20040050A1
Authority: IT; Italy
Prior art keywords: indicator; turbine engines; power margin; residual power; aircraft turbine
Prior art date: 2004-02-03

Application number

IT000050A

Other languages

English (en)

Inventor

Maurizio Simoni

Original Assignee

Agusta Spa

Priority date (The priority date 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 date listed.)

2004-02-03

Filing date

2004-02-03

Publication date

2004-05-03

2004-02-03 Application filed by Agusta Spa filed Critical Agusta Spa

2004-02-03 Priority to IT000050A priority Critical patent/ITTO20040050A1/it

2004-05-03 Publication of ITTO20040050A1 publication Critical patent/ITTO20040050A1/it

2005-02-01 Priority to EP05100696A priority patent/EP1562022B1/en

2005-02-01 Priority to US11/046,900 priority patent/US7322178B2/en

2005-02-02 Priority to CA2495862A priority patent/CA2495862C/en

2005-02-03 Priority to JP2005027419A priority patent/JP4673076B2/ja

Links

RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1

Classifications

- 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
- G01—MEASURING; TESTING
- G01D—MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
- G01D7/00—Indicating measured values
- G01D7/02—Indicating value of two or more variables simultaneously
- G01D7/04—Indicating value of two or more variables simultaneously using a separate indicating element for each variable

Landscapes

Engineering & Computer Science (AREA)
Radar, Positioning & Navigation (AREA)
Remote Sensing (AREA)
Physics & Mathematics (AREA)
General Physics & Mathematics (AREA)
Aviation & Aerospace Engineering (AREA)
Control Of Turbines (AREA)
Combined Controls Of Internal Combustion Engines (AREA)

IT000050A 2004-02-03 2004-02-03 Dispositivo indicatore di un margine di potenza residua di motori a turbina di velivoli ITTO20040050A1 (it)

Priority Applications (5)

Application Number	Priority Date	Filing Date	Title
IT000050A ITTO20040050A1 (it)	2004-02-03	2004-02-03	Dispositivo indicatore di un margine di potenza residua di motori a turbina di velivoli
EP05100696A EP1562022B1 (en)	2004-02-03	2005-02-01	Device for indicating a residual power margin of aircraft turbine engines
US11/046,900 US7322178B2 (en)	2004-02-03	2005-02-01	Device for indicating a residual power margin of aircraft turbine engines
CA2495862A CA2495862C (en)	2004-02-03	2005-02-02	Device for indicating a residual power margin of aircraft turbine engines
JP2005027419A JP4673076B2 (ja)	2004-02-03	2005-02-03	航空機タービンエンジンの残存出力余裕を表示する装置

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
IT000050A ITTO20040050A1 (it)	2004-02-03	2004-02-03	Dispositivo indicatore di un margine di potenza residua di motori a turbina di velivoli

Publications (1)

Publication Number	Publication Date
ITTO20040050A1 true ITTO20040050A1 (it)	2004-05-03

Family

ID=34674590

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
IT000050A ITTO20040050A1 (it)	2004-02-03	2004-02-03	Dispositivo indicatore di un margine di potenza residua di motori a turbina di velivoli

Country Status (5)

Country	Link
US (1)	US7322178B2 (it)
EP (1)	EP1562022B1 (it)
JP (1)	JP4673076B2 (it)
CA (1)	CA2495862C (it)
IT (1)	ITTO20040050A1 (it)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
FR2888638B1 (fr) *	2005-07-18	2007-09-28	Airbus Sas	Indicateur de pilotage pour un aeronef, destine a fournir un parametre de puissance d'au moins un turbopropulseur dudit aeronef
FR2902408B1 (fr) *	2006-06-19	2008-08-08	Eurocopter France	Equilibrage en puissance de deux turbomoteurs d'un aeronef
US8417410B2 (en) *	2008-12-23	2013-04-09	Honeywell International Inc.	Operations support systems and methods with power management
US7801695B2 (en) *	2008-12-23	2010-09-21	Honeywell International Inc.	Operations support systems and methods with model-based torque estimates
US20100161196A1 (en) *	2008-12-23	2010-06-24	Honeywell International Inc.	Operations support systems and methods with engine diagnostics
US8321118B2 (en) *	2008-12-23	2012-11-27	Honeywell International Inc.	Operations support systems and methods with power assurance
FR2950324B1 (fr) *	2009-09-23	2011-08-26	Eurocopter France	Procede et dispositif d'aide au pilotage d'un aeronef en cas de pannes d'un indicateur de premiere limitation
US8467918B2 (en) *	2011-07-05	2013-06-18	Universal Avionics Systems Corporation	Heuristic method for computing performance of an aircraft
US20140257675A1 (en) *	2013-03-07	2014-09-11	Honda Motor Co., Ltd.	System and method for indicating engine power band information on a tachometer display
US9784508B2 (en) *	2013-04-16	2017-10-10	Hamilton Sundstrand Corporation	Method of monitoring a heat exchanger arrangement and ram air fan in an aircraft to prevent stall conditions
US10683099B2 (en)	2017-02-08	2020-06-16	Pratt & Whitney Canada Corp.	Methods and systems for controlling operation of aircraft engines
US11047309B2 (en)	2017-07-26	2021-06-29	Pratt & Whitney Canada Corp.	Method and system for detecting an abnormal engine start
FR3086274B1 (fr)	2018-09-26	2021-03-12	Airbus Helicopters	Procede et dispositif d'aide au pilotage d'un giravion hydride muni d'un rotor de sustentation et d'au moins un rotor propulsif generant une poussee
CN111204469B (zh) *	2019-12-04	2023-06-23	中国航空工业集团公司成都飞机设计研究所	一种飞行能量变化显示系统及显示位置确定方法
CN114013666B (zh) *	2021-11-19	2024-04-12	中国航发沈阳发动机研究所	一种航空发动机主动增稳控制方法及装置
FR3134564B1 (fr) *	2022-04-15	2024-07-19	Airbus Helicopters	Procédé et système d'aide au pilotage d'un aéronef, aéronef équipé d’un tel système.
US12208917B2 (en)	2022-06-28	2025-01-28	Beta Air, Llc	Transition gauge for electric aircraft

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US3181353A (en) *	1963-02-04	1965-05-04	United Aircraft Corp	Power remaining indicator
US3272004A (en) *	1963-09-03	1966-09-13	United Aircraft Corp	Horsepower remaining computer
US4736331A (en) *	1982-05-26	1988-04-05	United Technologies Corporation	Helicopter power available to hover indicator
FR2756256B1 (fr) *	1996-11-26	1999-01-22	Eurocopter France	Indicateur de marge de puissance pour un aeronef a voilure tournante, notamment un helicoptere
FR2772718B1 (fr) *	1997-12-22	2000-02-11	Eurocopter France	Indicateur de pilotage pour aeronef
FR2809082B1 (fr)	2000-05-17	2002-09-20	Eurocopter France	Indicateur de marge de puissance pour un aeronef a voilure tournante, notamment un helicoptere

2004
- 2004-02-03 IT IT000050A patent/ITTO20040050A1/it unknown
2005
- 2005-02-01 EP EP05100696A patent/EP1562022B1/en not_active Expired - Lifetime
- 2005-02-01 US US11/046,900 patent/US7322178B2/en not_active Expired - Lifetime
- 2005-02-02 CA CA2495862A patent/CA2495862C/en not_active Expired - Lifetime
- 2005-02-03 JP JP2005027419A patent/JP4673076B2/ja not_active Expired - Fee Related

Also Published As

Publication number	Publication date
CA2495862A1 (en)	2005-08-03
EP1562022B1 (en)	2013-01-02
US20060064959A1 (en)	2006-03-30
EP1562022A1 (en)	2005-08-10
JP2005248951A (ja)	2005-09-15
US7322178B2 (en)	2008-01-29
JP4673076B2 (ja)	2011-04-20
CA2495862C (en)	2012-08-21

Publication	Publication Date	Title
DE602005007391D1 (de)	2008-07-24	Gasturbinentriebwerk
DE602005027552D1 (de)	2011-06-01	Reparatur an gasturbinen-motorenbauteilen durch dynamisches kaltgasspritzen
GB2428748B (en)	2008-03-05	Method Of Operating A Wind Turbine
DK1772624T3 (da)	2014-06-16	Direkte drev vindmølle-elgenerator med aftagelig lejeindretning
SG123665A1 (en)	2006-07-26	Turbine engine guide vane and arrays thereof
GB2411437B (en)	2007-10-24	Aircraft gas turbine engines
DE602005003759D1 (de)	2008-01-24	Gegenläufiges Turbinentriebwerk
DE502005003989D1 (de)	2008-06-19	Windkraftanlage
DE602005025427D1 (de)	2011-02-03	Verstellbare Leitschaufelanordnung einer Gasturbine
FR2941492B1 (fr)	2011-09-09	Turbomachine a turbine de puissance equipee d'un generateur electronique de puissance centre sur l'axe de la turbomachine
EP1781944A4 (en)	2011-09-14	HYDROELECTRIC TURBINE WITH COLLAPSIVE DECKBAND
GB0401189D0 (en)	2004-02-25	Turbine engine arrangements
DE602005007297D1 (de)	2008-07-17	Turbine eines Gasturbinentriebwerks
FI20045289L (fi)	2006-02-12	Menetelmä tuulivoimalan yhteydessä
GB0817855D0 (en)	2008-11-05	Artificial bird projectiles for simulating bird strike events
EP1795714A4 (en)	2008-06-25	ENGINE TYPE <= GAS-VAPOR TURBINE> =
PL1820963T3 (pl)	2016-01-29	Sposób eksploatacji silnika wiatrowego
GB0403941D0 (en)	2004-03-24	A gas turbine engine blade containment assembly
DE602005001528D1 (de)	2007-08-16	Gasturbinentriebwerk
DK1577551T3 (da)	2012-09-17	Vindenergianlæg
DE602006020376D1 (de)	2011-04-14	ugehörige Gasturbine
NO20054322D0 (no)	2005-09-20	Rotorblad for forste trinn i en gassturbin
DE112004003013A5 (de)	2007-08-23	Gründung für eine Offshore-Windkraftanlage
NO20043558L (no)	2006-02-27	Anordning ved turbin
GB0413652D0 (en)	2004-07-21	Gas turbine engine structure