Turbine engine cooling system with an open loop circuit
Номер патента: EP2920444A2
Опубликовано: 23-09-2015
Автор(ы): Mark F. Zelesky, Michael F. Blair, Tracy A. Propheter-Hinckley
Принадлежит: United Technologies Corp
Опубликовано: 23-09-2015
Автор(ы): Mark F. Zelesky, Michael F. Blair, Tracy A. Propheter-Hinckley
Принадлежит: United Technologies Corp
Реферат: A turbine engine system includes a heat source, a heat exchanger, a cooling medium inlet and a cooling medium outlet. The heat source includes a first passage. The heat exchanger includes a second passage and a third passage. The first and the second passages are configured in a closed loop circuit. The third passage is configured between the inlet and the outlet in an open loop circuit.
Turbine engine cooling system with an open loop circuit
Номер патента: US09739171B2. Автор: Mark F. Zelesky,Michael F. Blair,Tracy A. Propheter-Hinckley. Владелец: United Technologies Corp. Дата публикации: 2017-08-22.