RU2018139226A - DYNAMIC HELICOPTER MASS CONTROL METHOD - Google Patents

DYNAMIC HELICOPTER MASS CONTROL METHOD Download PDF

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Publication number
RU2018139226A
RU2018139226A RU2018139226A RU2018139226A RU2018139226A RU 2018139226 A RU2018139226 A RU 2018139226A RU 2018139226 A RU2018139226 A RU 2018139226A RU 2018139226 A RU2018139226 A RU 2018139226A RU 2018139226 A RU2018139226 A RU 2018139226A
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RU
Russia
Prior art keywords
helicopter
mass
control method
mass control
board
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RU2018139226A
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Russian (ru)
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RU2018139226A3 (en
Inventor
Алексей Васильевич Егоров
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Алексей Васильевич Егоров
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Priority to RU2018139226A priority Critical patent/RU2018139226A/en
Publication of RU2018139226A3 publication Critical patent/RU2018139226A3/ru
Publication of RU2018139226A publication Critical patent/RU2018139226A/en

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Claims (1)

Метод контроля массы вертолета, отличающийся тем, что масса вертолета определяется как произведение массы вертолета с известной размещенной на его борту массой на отношение суммы вертикального ускорения вертолета с известной размещенной на его борту массой в заданном интервале высот на конкретном режиме работы двигательно-винтового комплекса вертолета и ускорения свободного падения к сумме вертикального ускорения вертолета с неизвестной размещенной на его борту массой в том же заданном интервале высот на том же конкретном режиме работы двигательно-винтового комплекса вертолета и ускорения свободного падения.The method of controlling the mass of the helicopter, characterized in that the mass of the helicopter is defined as the product of the mass of the helicopter with the known mass placed on its board by the ratio of the sum of the vertical acceleration of the helicopter with the known mass placed on its board in a given altitude range for a particular operating mode of the helicopter propeller complex of the helicopter and free fall acceleration to the sum of the vertical acceleration of the helicopter with an unknown mass placed on its board in the same given height range at the same specific operating mode of the helicopter propeller-screw complex and free fall acceleration.
RU2018139226A 2018-11-06 2018-11-06 DYNAMIC HELICOPTER MASS CONTROL METHOD RU2018139226A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2018139226A RU2018139226A (en) 2018-11-06 2018-11-06 DYNAMIC HELICOPTER MASS CONTROL METHOD

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2018139226A RU2018139226A (en) 2018-11-06 2018-11-06 DYNAMIC HELICOPTER MASS CONTROL METHOD

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RU2018139226A3 RU2018139226A3 (en) 2020-05-12
RU2018139226A true RU2018139226A (en) 2020-05-12

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RU2018139226A RU2018139226A (en) 2018-11-06 2018-11-06 DYNAMIC HELICOPTER MASS CONTROL METHOD

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2780976C1 (en) * 2021-11-24 2022-10-04 Федеральное государственное автономное образовательное учреждение высшего образования "Сибирский федеральный университет" Dynamic method for monitoring the mass of the load of a hoisting machine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2780976C1 (en) * 2021-11-24 2022-10-04 Федеральное государственное автономное образовательное учреждение высшего образования "Сибирский федеральный университет" Dynamic method for monitoring the mass of the load of a hoisting machine

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Publication number Publication date
RU2018139226A3 (en) 2020-05-12

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