WO2001003583A1 - Procede de controle de l'etat fonctionnel d'un pilote en vol et dispositif correspondant - Google Patents

Procede de controle de l'etat fonctionnel d'un pilote en vol et dispositif correspondant Download PDF

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Publication number
WO2001003583A1
WO2001003583A1 PCT/RU2000/000051 RU0000051W WO0103583A1 WO 2001003583 A1 WO2001003583 A1 WO 2001003583A1 RU 0000051 W RU0000051 W RU 0000051W WO 0103583 A1 WO0103583 A1 WO 0103583A1
Authority
WO
WIPO (PCT)
Prior art keywords
pilot
leτchiκa
uπρavleniya
daτchiκa
pressure
Prior art date
Application number
PCT/RU2000/000051
Other languages
English (en)
Russian (ru)
Inventor
Valentin Afanasievich Sukholitko
Original Assignee
Sukholitko Valentin Afanasievi
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 Sukholitko Valentin Afanasievi filed Critical Sukholitko Valentin Afanasievi
Priority to AU31999/00A priority Critical patent/AU3199900A/en
Publication of WO2001003583A1 publication Critical patent/WO2001003583A1/fr

Links

Classifications

    • G—PHYSICS
    • G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
    • G09B9/00—Simulators for teaching or training purposes
    • G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
    • G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
    • A—HUMAN NECESSITIES
    • A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61B—DIAGNOSIS; SURGERY; IDENTIFICATION
    • A61B5/00—Measuring for diagnostic purposes; Identification of persons
    • A61B5/16—Devices for psychotechnics; Testing reaction times ; Devices for evaluating the psychological state
    • A61B5/18—Devices for psychotechnics; Testing reaction times ; Devices for evaluating the psychological state for vehicle drivers or machine operators
    • G—PHYSICS
    • G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
    • G09B9/00—Simulators for teaching or training purposes
    • G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
    • G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
    • G09B9/28—Simulation of stick forces or the like

Definitions

  • the invention is subject to medical equipment, and specifically to the systems of control and management of the functional state of the device.
  • the physiological state of the machine is at the same time as the flight, and compared to the current
  • the data are mediocre, which may be used to change the mode
  • the crashes of the system are the absence of the automatic partitions of the machine and the crashes of the crashes
  • vyb ⁇ anny in ⁇ aches ⁇ ve blizhaysheg ⁇ anal ⁇ ga s ⁇ s ⁇ b ⁇ n ⁇ lya and u ⁇ avleniya ⁇ un ⁇ ii ⁇ nalnym s ⁇ s ⁇ yaniem ⁇ e ⁇ a ⁇ a, s ⁇ avnenii ⁇ luchenny ⁇ values e ⁇ al ⁇ nnymi data us ⁇ anenii ⁇ ass ⁇ glas ⁇ vaniya therebetween and v ⁇ zdeys ⁇ vii on s ⁇ s ⁇ yanie ⁇ e ⁇ a ⁇ a ( ⁇ a ⁇ . SSS ⁇ - ⁇ ⁇ l 1,708,303. ⁇ 61 ⁇ 5 / 16, 1992).
  • the objective of the invention is to expand the functional capabilities of the system, to increase the accessibility of the processor to the conditions of the condition
  • the task posed is achieved in that by means of a console and control
  • ⁇ ed ⁇ s ⁇ a ⁇ ami izves ⁇ n ⁇ g ⁇ us ⁇ ys ⁇ va yavlyayu ⁇ sya is ⁇ lz ⁇ vanie ⁇ g ⁇ anichenn ⁇ g ⁇ ⁇ liches ⁇ va da ⁇ chi ⁇ v for izme ⁇ eniya ⁇ a ⁇ ame ⁇ v ⁇ un ⁇ tsi ⁇ naln ⁇ g ⁇ s ⁇ s ⁇ yaniya ⁇ e ⁇ a ⁇ a and ⁇ g ⁇ anichenn ⁇ g ⁇ ⁇ liches ⁇ va s ⁇ eds ⁇ v v ⁇ zdeys ⁇ viya on s ⁇ s ⁇ yanie ⁇ e ⁇ a ⁇ a, is ⁇ lyuchayushee v ⁇ zdeys ⁇ vie if ⁇ e ⁇ i ⁇ e ⁇ a ⁇ m s ⁇ znaniya and ⁇ su ⁇ s ⁇ vie s ⁇ eds ⁇ v, ⁇ ed ⁇ v ⁇ aschayuschi ⁇ ava ⁇ iyu ⁇ ans ⁇ n ⁇ g ⁇
  • the task of the invention in part of the device is to expand the functional options, to increase the cost of the connection to the treatment unit.
  • the task posed is achieved in that, in the case of the device of the console and the operation of the functional state of the laptop, the connected connected measurement units are included in the plug-in.
  • da ⁇ izme ⁇ i ⁇ eley vy ⁇ lnen as da ⁇ chi ⁇ a ⁇ bzha ⁇ iya le ⁇ chi ⁇ m ⁇ uch ⁇ i u ⁇ avleniya sam ⁇ le ⁇ m, da ⁇ chi ⁇ a efforts ⁇ bzha ⁇ iya le ⁇ chi ⁇ m ⁇ uch ⁇ i u ⁇ avleniya, m ⁇ n ⁇ i ⁇ uemy ⁇ on ⁇ uch ⁇ e u ⁇ avleniya, da ⁇ chi ⁇ a ⁇ i ⁇ satsii ⁇ ae ⁇ ii movement ⁇ uch ⁇ i u ⁇ avleniya and da ⁇ chi ⁇ a ⁇ l ⁇ zheniya g ⁇ l ⁇ vy, ⁇ azmeschenny ⁇ in ⁇ abine sam ⁇ le ⁇ a, da ⁇ chi ⁇ a ⁇ i ⁇ sat
  • a pilot in the form of oxygen, electrics, noise and sound stimulators an automatic system for controlling a voltage and a self-defense system, a wiring system for an external wiring
  • the “a” measuring unit includes the following sensors:
  • Provider 1 of the summer flight control by the aircraft is mounted on the control panel;
  • the cottage 4 head position is mounted in the cockpit of the aircraft and signals to turn off the head position were turned off;
  • the 6th light ventilation unit is mounted in an acidic mask of the pilot and registers a dusty process and the proper use of acidic equipment;
  • the oxygen pressure sensor 7 is mounted in the oxygen system
  • the sensor 8 of the mixture quality is mounted in the oxygen system of the aircraft and signaling the oxygen-containing mixture of the industrial flue gas;
  • thermo-sensor 9 is mounted in an oxygen-based aircraft and
  • Pneumatic sensor 10 is mounted in the air blower
  • the 11 light ventilation unit is mounted in the air by blowing the air mixture in the compressor and bypassing it is free of charge;
  • Radiomotive height 12 is mounted on an airplane for the determination of a safe altitude
  • the sensor 15 is mounted on an airplane and signals a removed landing gear when take-off and landing landing gear; • Datch 16 of registration of the response of the pilot is mounted on an airplane and registers the response of the pilot to the system.
  • the analysis and control unit “b” consists of:
  • the electrical elements of the distributed input are the signal processing circuits of the sensors.
  • the final elements of the distributed output are transistor or other switches with relays, the contact points of the circuits control the load circuits.
  • Processing and processing of the commands is ensured by it in accordance with the processing and control system.
  • the device handles the following: • to turn on the automatic system 19 of the control panel;
  • the invention has the advantage of allowing the user to opt out of the environment
  • this invention allows you to bring the plane and the flyer to the ground. - -
  • the signals from sensors 1-14 are received in the analysis block “b”.
  • transmitted signals are analyzed by comparison.
  • the analysis block “b” replaces the command issued to the sound synthesizer 25, and the pilot continues to fly in the usual mode. ⁇ if the transmitter does not react to the signal of the sound synthesizer 25 in the installed mode, the “b” analysis unit will transmit and transmit the signal to the command:

Abstract

L'invention relève du domaine de la technique médicale et concerne un procédé pour contrôler l'état fonctionnel d'un pilote dans des conditions de vol. Selon ce procédé, on enregistre la pression et l'effort exercés par le pilote sur le manche à balai, les changements de trajectoire du manche à balai, l'effort appliqué par le pilote au palonnier, la position de la tête du piloet, le processus respiratoire, la pression de l'oxygène et la qualité du mélange dans la conduite du système d'oxygène, la pression dans la combinaison anti-g, l'altitude critique et l'altitude actuelle ainsi que la valeur du G. En cas de déviation des paramètres enregistrés par rapport qux valeurs de référence, une unité d'analyse et de commade génère des informations sur l'apparition d'une contingence et les transmet au pilote. En cas d'élimination de cette contignence par le pilote, l'unité d'analys annule la commande envoyée au synthétiseur vocal; en cas d'absence de réaction du pilote aux susdites informations, un signal est généné pour enclencher les systèmes de stimulation, remettre l'avion en vol horizontal et enclencher les systèmes de pilotage et d'atterrissage automatiques. Le dispositif de l'invention comprend une unité de capteurs, une unité d'analyse et de commande et une unité de sortie.
PCT/RU2000/000051 1999-07-08 2000-02-15 Procede de controle de l'etat fonctionnel d'un pilote en vol et dispositif correspondant WO2001003583A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU31999/00A AU3199900A (en) 1999-07-08 2000-02-15 Method for monitoring the functional status of a pilot during flight and device therefor

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
RU99114971 1999-07-08
RU99114971/28A RU2150886C1 (ru) 1999-07-08 1999-07-08 Способ контроля и управления функциональным состоянием летчика в полете и устройство для осуществления способа

Publications (1)

Publication Number Publication Date
WO2001003583A1 true WO2001003583A1 (fr) 2001-01-18

Family

ID=20222492

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/RU2000/000051 WO2001003583A1 (fr) 1999-07-08 2000-02-15 Procede de controle de l'etat fonctionnel d'un pilote en vol et dispositif correspondant

Country Status (3)

Country Link
AU (1) AU3199900A (fr)
RU (1) RU2150886C1 (fr)
WO (1) WO2001003583A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2868274A1 (fr) * 2013-11-04 2015-05-06 Airbus Operations (S.A.S) Systèmes et procédés de détection de focalisation sur pilote

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005008315A1 (fr) * 2003-07-18 2005-01-27 Oleg Leonidovich Golovkov Casque virtuel a grand angle
RU2655186C2 (ru) * 2016-05-13 2018-05-24 Акционерное общество "Ассоциация разработчиков и производителей систем мониторинга" Способ контроля функционального состояния человека в экстремальных условиях деятельности
CN112530259A (zh) * 2021-01-15 2021-03-19 岳阳职业技术学院 一种基础护理教学用输氧管固定设备

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4634384A (en) * 1984-02-02 1987-01-06 General Electric Company Head and/or eye tracked optically blended display system
EP0468554A2 (fr) * 1990-07-26 1992-01-29 Galeazzo Azzi Appareil pour constater et mesurer la capacité physique des utilisateurs de véhicules à moteur ainsi que leurs aptitudes pour la conduite avec ou sans l'aide d'adaptateurs et/ou de prothèses
SU1708303A1 (ru) * 1989-12-25 1992-01-30 Рижское Высшее Военно-Политическое Краснознаменное Училище Им.Маршала Советского Союза Бирюзова С.С. Устройство дл контрол и управлени функциональным состо нием оператора
SU1259860A1 (ru) * 1984-12-26 1994-10-30 Н.Н. Панов Имитатор бортового кислородного оборудования для авиационного тренажера
RU2072948C1 (ru) * 1992-12-28 1997-02-10 Акционерное общество открытого типа "Звезда" Способ установления факта потери сознания летчиком в результате воздействия перегрузок
RU2111698C1 (ru) * 1996-06-21 1998-05-27 Государственный научно-исследовательский испытательный институт МО РФ (авиационной и космической медицины) Способ автоматизированной оценки состояния летчика в условиях воздействия пилотажных перегрузок и устройство для его осуществления

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4634384A (en) * 1984-02-02 1987-01-06 General Electric Company Head and/or eye tracked optically blended display system
SU1259860A1 (ru) * 1984-12-26 1994-10-30 Н.Н. Панов Имитатор бортового кислородного оборудования для авиационного тренажера
SU1708303A1 (ru) * 1989-12-25 1992-01-30 Рижское Высшее Военно-Политическое Краснознаменное Училище Им.Маршала Советского Союза Бирюзова С.С. Устройство дл контрол и управлени функциональным состо нием оператора
EP0468554A2 (fr) * 1990-07-26 1992-01-29 Galeazzo Azzi Appareil pour constater et mesurer la capacité physique des utilisateurs de véhicules à moteur ainsi que leurs aptitudes pour la conduite avec ou sans l'aide d'adaptateurs et/ou de prothèses
RU2072948C1 (ru) * 1992-12-28 1997-02-10 Акционерное общество открытого типа "Звезда" Способ установления факта потери сознания летчиком в результате воздействия перегрузок
RU2111698C1 (ru) * 1996-06-21 1998-05-27 Государственный научно-исследовательский испытательный институт МО РФ (авиационной и космической медицины) Способ автоматизированной оценки состояния летчика в условиях воздействия пилотажных перегрузок и устройство для его осуществления

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2868274A1 (fr) * 2013-11-04 2015-05-06 Airbus Operations (S.A.S) Systèmes et procédés de détection de focalisation sur pilote

Also Published As

Publication number Publication date
AU3199900A (en) 2001-01-30
RU2150886C1 (ru) 2000-06-20

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