ES2678748R1 - Sistema electrónico para estimación de carga y centrado de aeronaves - Google Patents

Sistema electrónico para estimación de carga y centrado de aeronaves Download PDF

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Publication number
ES2678748R1
ES2678748R1 ES201700137A ES201700137A ES2678748R1 ES 2678748 R1 ES2678748 R1 ES 2678748R1 ES 201700137 A ES201700137 A ES 201700137A ES 201700137 A ES201700137 A ES 201700137A ES 2678748 R1 ES2678748 R1 ES 2678748R1
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ES
Spain
Prior art keywords
aircraft
load
electronic system
data
gravity
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.)
Granted
Application number
ES201700137A
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English (en)
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ES2678748B2 (es
ES2678748A2 (es
Inventor
Saúl ROBAINA HERNÁNDEZ
Luis GÓMEZ DÉNIZ
Rafael SOCAS GUTIÉRREZ
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Universidad de las Palmas de Gran Canaria
Original Assignee
Universidad de las Palmas de Gran Canaria
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.)
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Publication date
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Priority to ES201700137A priority Critical patent/ES2678748B2/es
Publication of ES2678748A2 publication Critical patent/ES2678748A2/es
Publication of ES2678748R1 publication Critical patent/ES2678748R1/es
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Publication of ES2678748B2 publication Critical patent/ES2678748B2/es
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Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M1/00—Testing static or dynamic balance of machines or structures
    • G01M1/12—Static balancing; Determining position of centre of gravity
    • G01M1/122—Determining position of centre of gravity
    • G01M1/125—Determining position of centre of gravity of aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01G—WEIGHING
    • G01G19/00—Weighing apparatus or methods adapted for special purposes not provided for in the preceding groups
    • G01G19/02—Weighing apparatus or methods adapted for special purposes not provided for in the preceding groups for weighing wheeled or rolling bodies, e.g. vehicles
    • G01G19/07—Weighing apparatus or methods adapted for special purposes not provided for in the preceding groups for weighing wheeled or rolling bodies, e.g. vehicles for weighing aircraft

Abstract

En la actualidad, existen aeronaves en las que se tienen que calcular la carga y el centro de gravedad de la aeronave de forma manual y estimativa, por lo que estos datos de vital importancia en la estabilidad de todas las fases de vuelo de la aeronave pueden diferir de los verdaderos con las consecuencias en pilotaje que ello conlleva. La presente invención aporta un sistema electrónico para realizar el cálculo automático de dicha carga y centro de gravedad. Su aplicación es en el sector de la tecnología aeronáutica civil, cuyo objetivo es conocer si estos datos se encuentran entre los límites de seguridad impuestos por el fabricante para el pilotaje de la aeronave.#Este sistema electrónico comprende un sistema de adquisición de datos y un dispositivo visualizador en un terminal móvil (Tablet, laptop o teléfono móvil) de propósito general. El sistema de adquisición de datos consta de un conjunto de sensores (de carga y de presión) y una unidad de control implementada con una placa microcontroladora, que se encarga de capturar las lecturas de los sensores para enviarla al sistema de visualización mediante una comunicación inalámbrica basada en una red pública de comunicaciones móviles.
ES201700137A 2017-02-15 2017-02-15 Sistema electrónico para estimación de carga y centrado de aeronaves Active ES2678748B2 (es)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES201700137A ES2678748B2 (es) 2017-02-15 2017-02-15 Sistema electrónico para estimación de carga y centrado de aeronaves

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES201700137A ES2678748B2 (es) 2017-02-15 2017-02-15 Sistema electrónico para estimación de carga y centrado de aeronaves

Publications (3)

Publication Number Publication Date
ES2678748A2 ES2678748A2 (es) 2018-08-17
ES2678748R1 true ES2678748R1 (es) 2018-10-15
ES2678748B2 ES2678748B2 (es) 2019-02-18

Family

ID=63139215

Family Applications (1)

Application Number Title Priority Date Filing Date
ES201700137A Active ES2678748B2 (es) 2017-02-15 2017-02-15 Sistema electrónico para estimación de carga y centrado de aeronaves

Country Status (1)

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ES (1) ES2678748B2 (es)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3415979A (en) * 1964-06-05 1968-12-10 Elfenbein Analog trim computer
US3746844A (en) * 1970-10-22 1973-07-17 Aerospatiale Apparatus for determining the center of gravity of passengers in a vehicle, namely an aircraft
US4225926A (en) * 1978-01-18 1980-09-30 Messerschmitt-Bolkow-Blohm Gmbh Apparatus for loading and unloading an aircraft and ascertaining the weight of the load
DE10152958A1 (de) * 2001-10-26 2003-08-21 Hottinger Messtechnik Baldwin Vorrichtung und Verfahren zur sitzbelegungsabhängigen Ansteuerung von Sicherheitssystemen
US20090105874A1 (en) * 2005-01-13 2009-04-23 Rheinmetall Defence Electronics Gmbh Device and Method for Controlling the Loading and/or Unloading Process of an Airplane
US20160371899A1 (en) * 2015-06-19 2016-12-22 Aisin Seiki Kabushiki Kaisha Seat-occupancy state detection device

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3415979A (en) * 1964-06-05 1968-12-10 Elfenbein Analog trim computer
US3746844A (en) * 1970-10-22 1973-07-17 Aerospatiale Apparatus for determining the center of gravity of passengers in a vehicle, namely an aircraft
US4225926A (en) * 1978-01-18 1980-09-30 Messerschmitt-Bolkow-Blohm Gmbh Apparatus for loading and unloading an aircraft and ascertaining the weight of the load
DE10152958A1 (de) * 2001-10-26 2003-08-21 Hottinger Messtechnik Baldwin Vorrichtung und Verfahren zur sitzbelegungsabhängigen Ansteuerung von Sicherheitssystemen
US20090105874A1 (en) * 2005-01-13 2009-04-23 Rheinmetall Defence Electronics Gmbh Device and Method for Controlling the Loading and/or Unloading Process of an Airplane
US20160371899A1 (en) * 2015-06-19 2016-12-22 Aisin Seiki Kabushiki Kaisha Seat-occupancy state detection device

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
PURA CIENCIA CON SÁUL ROBAINA, INGENIERO DE LA ULPGC. 20/07/2016, [en línea][recuperado el 02/10/2018]. Recuperado de Internet (URL:play.cadenaser.com/audio/000WB1009120160720111029/), Entrevista radiofónica *
Universidad de Las Palmas de Gran Canaria: OTRI. SISTEMA ELECTRÓNICO PARA ESTIMACIÓN DE CARGA Y CENTRADO DE AERONAVES LIGERAS Y MEDIANAS CON PASAJEROS Y EQUIPAJE.. 02/08/2016, Recuperado de Internet (URL:https://web.archive.org/web/20160802205038/http:/otri.ulpgc.es:80/sistema-electronico-para-estimacion-de-carga-y-centrado-de-aeronaves-ligeras-y-medianas-electronic-system-for-estimating-weight-and-balance-of-light-and-medium-aircraft/), *

Also Published As

Publication number Publication date
ES2678748B2 (es) 2019-02-18
ES2678748A2 (es) 2018-08-17

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