MX2019001504A - Metodos y sistemas para controlar el empuje producido por una pluralidad de motores en una aeronave para ayudar con ciertas condiciones de vuelo. - Google Patents

Metodos y sistemas para controlar el empuje producido por una pluralidad de motores en una aeronave para ayudar con ciertas condiciones de vuelo.

Info

Publication number
MX2019001504A
MX2019001504A MX2019001504A MX2019001504A MX2019001504A MX 2019001504 A MX2019001504 A MX 2019001504A MX 2019001504 A MX2019001504 A MX 2019001504A MX 2019001504 A MX2019001504 A MX 2019001504A MX 2019001504 A MX2019001504 A MX 2019001504A
Authority
MX
Mexico
Prior art keywords
aircraft
engines
assisting
thrust produced
systems
Prior art date
Application number
MX2019001504A
Other languages
English (en)
Inventor
Wilson Douglas
Mills Nikos
Eggold David
Haugeberg Heidi
Inderhees Leonard
Beland Steven
KAMOFSKI Kent
Hodges Christopher
Original Assignee
Boeing Co
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.)
Filing date
Publication date
Application filed by Boeing Co filed Critical Boeing Co
Publication of MX2019001504A publication Critical patent/MX2019001504A/es

Links

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
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • B64D31/02—Initiating means
    • B64D31/06—Initiating means actuated automatically
    • 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
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • 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
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • B64D31/14—Transmitting means between initiating means and power plants
    • 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
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B19/00—Programme-control systems
    • G05B19/02—Programme-control systems electric
    • G05B19/04—Programme control other than numerical control, i.e. in sequence controllers or logic controllers
    • 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
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
    • G05D1/0833—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability using limited authority control
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/50—On board measures aiming to increase energy efficiency

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Computer Security & Cryptography (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Traffic Control Systems (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Feedback Control In General (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)

Abstract

En un ejemplo se describe un método para controlar el empuje producido por una pluralidad de motores en una aeronave para ayudar con la recuperación de nariz hacia abajo de las aeronaves; el método incluye seleccionar un valor máximo de un parámetro de aeronave, medir un valor del parámetro de aeronave mientras que la aeronave está en vuelo, con base en una comparación del valor máximo y el valor medido determinando que el valor medido excede el valor máximo, y reducir un empuje producido por cada uno de los motores de la pluralidad de motores para llevar el valor medido del parámetro de aeronave por debajo del valor máximo del parámetro de aeronave.
MX2019001504A 2018-02-06 2019-02-05 Metodos y sistemas para controlar el empuje producido por una pluralidad de motores en una aeronave para ayudar con ciertas condiciones de vuelo. MX2019001504A (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US15/889,306 US10759544B2 (en) 2018-02-06 2018-02-06 Methods and systems for controlling thrust produced by a plurality of engines on an aircraft for assisting with certain flight conditions

Publications (1)

Publication Number Publication Date
MX2019001504A true MX2019001504A (es) 2019-11-28

Family

ID=65041597

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2019001504A MX2019001504A (es) 2018-02-06 2019-02-05 Metodos y sistemas para controlar el empuje producido por una pluralidad de motores en una aeronave para ayudar con ciertas condiciones de vuelo.

Country Status (7)

Country Link
US (1) US10759544B2 (es)
EP (1) EP3521175B1 (es)
JP (1) JP7246192B2 (es)
CN (1) CN110116815A (es)
BR (1) BR102019000604A2 (es)
CA (1) CA3028391C (es)
MX (1) MX2019001504A (es)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20190354644A1 (en) * 2018-05-18 2019-11-21 Honeywell International Inc. Apparatuses and methods for detecting anomalous aircraft behavior using machine learning applications
US11273903B2 (en) * 2019-01-07 2022-03-15 The Regents Of The University Of California Systems and methods for controlling an aircraft's flight control surface
CN111176310B (zh) * 2019-12-31 2020-09-08 北京星际荣耀空间科技有限公司 一种运载火箭姿态控制系统的测试方法、装置及系统
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

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005032849B4 (de) * 2005-07-14 2009-09-03 Eads Deutschland Gmbh Vorrichtung und Verfahren zum Überführen eines Flugzeugs von einem außerhalb eines zulässigen Flugzustandsbereichs in einen innerhalb des zulässigen Flugzustandsbereichs liegenden Flugzustand
FR2898584B1 (fr) * 2006-03-15 2008-12-19 Airbus France Sas Procede et dispositif de commande de la poussee d'un aeronef multimoteur
BR112012017154B1 (pt) 2009-12-21 2021-09-28 The Boeing Company Método de controlar a atitude de inclinação de uma aeronave multimotor experimentando assimetria de impulso e sistema para uma aeronave de multimotor
IL217501A (en) * 2012-01-12 2017-09-28 Israel Aerospace Ind Ltd A method and system for maneuvering aircraft
FR2986649B1 (fr) * 2012-02-06 2014-01-31 Eurocopter France Procede de simulation de panne sur un aeronef
US8653990B2 (en) 2012-06-18 2014-02-18 The Boeing Company Stall management system
IL222053A (en) * 2012-09-23 2016-11-30 Israel Aerospace Ind Ltd A device, method, and computerized product for aircraft management
FR3016158B1 (fr) * 2014-01-09 2017-09-01 Airbus Operations Sas Dispositif de protection d'energie pour un aeronef.
GB201405894D0 (en) * 2014-04-02 2014-05-14 Rolls Royce Plc Aircraft vapour trail control system
US20160041561A1 (en) * 2014-08-11 2016-02-11 Co-Pilot Engineering, LLC Aircraft Flying Aid
US10227933B2 (en) * 2015-02-12 2019-03-12 United Technologies Corporation Aircraft power setting trims for life extension
FR3033886B1 (fr) * 2015-03-18 2017-04-21 Dassault Aviat Dispositif d' affichage d'une variation d'energie et d'une borne de variation d'energie d'un aeronef
FR3044358B1 (fr) 2015-11-27 2017-11-24 Airbus Operations Sas Procede de controle de la poussee des reacteurs d'un avion pendant la phase de decollage, dispositif de controle et avion correspondant
US10273017B2 (en) 2016-03-15 2019-04-30 The Boeing Company System and method for protecting the structural integrity of an engine strut
US10005561B2 (en) * 2016-06-16 2018-06-26 Ge Aviation Systems Llc Controlling aircraft using thrust differential trim
US9969503B2 (en) * 2016-07-21 2018-05-15 Rockwell Collins, Inc. Head-up display (HUD) stall recovery symbology

Also Published As

Publication number Publication date
EP3521175A1 (en) 2019-08-07
CA3028391A1 (en) 2019-08-06
JP7246192B2 (ja) 2023-03-27
US10759544B2 (en) 2020-09-01
BR102019000604A2 (pt) 2019-08-27
EP3521175B1 (en) 2020-06-03
CN110116815A (zh) 2019-08-13
JP2019163028A (ja) 2019-09-26
CA3028391C (en) 2023-09-05
US20190241273A1 (en) 2019-08-08

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