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2 483 397

(13)

(51)

IPC

H01M8/04(2006-01-01)

H01M8/14(2006-01-01)

H01M8/16(2006-01-01)

(21) (22)

Application

2012107520/07, 2012-02-28

(24)

Start date

2012-02-28

(22)

Actual filing date

2012-02-28

(45)

Published

2013-05-27

(72)

Inventor

Vinokurov Vladislav DmitrievichVinokurov Stanislav DmitrievichKazakov Evgenij BorisovichShuklin Igor' KlavdievichVolkov Vitalij Vital'Evich

(73)

Holder

Federal'Noe Gosudarstvennoe Voennoe Obrazovatel'Noe Uchrezhdenie Vysshego Professional'Nogo Obrazovanija Aviatsionnyj Inzhenernyj Universitet" Voronezh) Ministerstva Oborony Rossijskoj Federatsii

AIRCRAFT ENGINE STARTING SYSTEM Russian patent published in 2013 - IPC H01M8/04 H01M8/14 H01M8/16

Abstract RU 2483397 C1

FIELD: power industry.

SUBSTANCE: starting system of aircraft engines includes N units of sensors and a commutator, which are connected to a control, monitoring and protection unit.

EFFECT: conversion of energy of fuel elements to electric energy of improved quality with specified output parameters for reliable supply to onboard consumers of an airborne vehicle with all kinds of electric current, which excludes voltage supply in emergency situations.

1 dwg

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RU 2 483 397 C1

Authors

Vinokurov Vladislav Dmitrievich

Vinokurov Stanislav Dmitrievich

Kazakov Evgenij Borisovich

Shuklin Igor' Klavdievich

Volkov Vitalij Vital'Evich

Dates

2013-05-27—Published

2012-02-28—Filed