RU97112580A - METHOD FOR OPERATING AN OPERATING CHAIR - Google Patents

METHOD FOR OPERATING AN OPERATING CHAIR

Info

Publication number
RU97112580A
RU97112580A RU97112580/28A RU97112580A RU97112580A RU 97112580 A RU97112580 A RU 97112580A RU 97112580/28 A RU97112580/28 A RU 97112580/28A RU 97112580 A RU97112580 A RU 97112580A RU 97112580 A RU97112580 A RU 97112580A
Authority
RU
Russia
Prior art keywords
speed
vertical
systems
operating
ejection
Prior art date
Application number
RU97112580/28A
Other languages
Russian (ru)
Other versions
RU2116939C1 (en
Inventor
Г.И. Северин
А.Н. Лившиц
С.И. Артамонов
В.С. Беловинцев
В.П. Сарычев
Н.Н. Яковлев
Original Assignee
Открытое акционерное общество "Научно-производственное предприятие "Звезда"
Filing date
Publication date
Application filed by Открытое акционерное общество "Научно-производственное предприятие "Звезда" filed Critical Открытое акционерное общество "Научно-производственное предприятие "Звезда"
Priority to RU97112580A priority Critical patent/RU2116939C1/en
Priority claimed from RU97112580A external-priority patent/RU2116939C1/en
Application granted granted Critical
Publication of RU2116939C1 publication Critical patent/RU2116939C1/en
Publication of RU97112580A publication Critical patent/RU97112580A/en

Links

Claims (1)

Способ управления режимом работы катапультного кресла, заключающийся в получении с борта самолета в момент катапультирования скорости и высоты полета и задании в зависимости от них с помощью системы автоматики функциональной конфигурации катапультного кресла и временной последовательности работы его систем, отличающийся тем, что одновременно с использованием значения скорости и высоты полета в момент катапультирования дополнительно используют угол крена и угловую скорость по крену, вертикальную скорость, вертикальное ускорение и наличие признаков пикирования, кабрирования и обжатия шасси самолета, затем измеряют ускорение торможения и барометрическую высоту кресла и включают полученные данные в задание функциональной конфигурации катапультного кресла и временной последовательности работы его систем, причем скорость, высоту полета, угол крена и угловую скорость по крену, вертикальную скорость и вертикальное ускорение берут от бортовых систем самолета в цифровом последовательном коде.The method of controlling the operation mode of the ejection seat, which consists in receiving from the aircraft at the moment of ejection the speed and altitude and setting depending on them using the automation system the functional configuration of the ejection seat and the time sequence of its systems, characterized in that at the same time using the speed value and the flight altitude at the moment of bailout additionally use the roll angle and roll angular velocity, vertical speed, vertical acceleration and The signs of diving, cabling and crimping the airplane landing gear are then measured, then the braking acceleration and the barometric height of the seat are measured and the obtained data is included in the task of the functional configuration of the ejection seat and the time sequence of its systems, with the vertical speed, flight altitude, roll angle and roll angular velocity, vertical speed and vertical acceleration are taken from the aircraft's onboard systems in a digital serial code.
RU97112580A 1997-07-22 1997-07-22 Method of control of ejection seat operation RU2116939C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU97112580A RU2116939C1 (en) 1997-07-22 1997-07-22 Method of control of ejection seat operation

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU97112580A RU2116939C1 (en) 1997-07-22 1997-07-22 Method of control of ejection seat operation

Publications (2)

Publication Number Publication Date
RU2116939C1 RU2116939C1 (en) 1998-08-10
RU97112580A true RU97112580A (en) 1999-01-20

Family

ID=20195577

Family Applications (1)

Application Number Title Priority Date Filing Date
RU97112580A RU2116939C1 (en) 1997-07-22 1997-07-22 Method of control of ejection seat operation

Country Status (1)

Country Link
RU (1) RU2116939C1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2527603C1 (en) * 2013-06-25 2014-09-10 Открытое акционерное общество "Научно-производственное предприятие "Звезда" имени академика Г.И. Северина" Astronaut seat
RU2527615C1 (en) * 2013-06-25 2014-09-10 Открытое акционерное общество "Научно-производственное предприятие "Звезда" имени академика Г.И. Северина" Provision of operating and emergent g-tolerance in spacecraft
CN110803301A (en) * 2019-12-12 2020-02-18 沈阳航空航天大学 Novel ejection speed measuring method for ejection of ejection seat out of cabin

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