27-01-2016 дата публикации
Номер: KR1020160010345A
Принадлежит:
The present invention relates to a ground support device for an aircraft. The ground support device for an aircraft includes a gas turbine engine part, an air cycle system part, and an integrated controller. The gas turbine engine part includes: a compressor and a gas turbine, combined with a rotation shaft; a generator combined with the rotation shaft; and a combustion chamber supplying combustion gas to the gas turbine, and provides compressed air, discharged from the compressor, and power of the generator to the outside. The air cycle system part includes: a cooling turbine rotated by the compressed air, provided from the compressor, and expanding and cooling compressed air; and a cooling turbine changing nozzle installed at the mouth of the cooling turbine to spray the compressed air to the cooling turbine, and providing conditioning air to the outside. The integrated controller controls the pressure and flux of the compressed air, discharged from the compressor, according to a load ...
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