FIELD: aviation.
SUBSTANCE: invention relates to aircraft fueling. Flow amplifier (107) contains setting mechanism (115) of a receiving device, starting device (116) and flow regulator (118). Setting mechanism (115) of the receiving device is connected to connecting device (110) of the receiving device, and starting device (116) is jointly connected between setting mechanism (115) of the receiving device and flow regulator (118). Flow regulator (118) is connected to aircraft (102), fuel chain (108), setting mechanism (115) of the receiving device and/or starting device (116) to control and/or manage their operation. Setting mechanism (115) of the receiving device can be connected to receiving device (110) to apply some force to it. Starting device (116) can be used to change the force of setting mechanism (115) of the receiving device; and, in response to changed parameters, such as fuel pressure, the flow regulator can be used to activate starting device (116).
EFFECT: increase in the safety and refueling efficiency is achieved.
15 cl, 24 dwg
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Authors
Dates
2022-06-29—Published
2019-01-08—Filed