Working fluid system for aircraft powerplant
An assembly includes a first powerplant component, a second powerplant component, a first inter-circuit heat exchanger, a first fluid circuit and a second fluid circuit. The first fluid circuit is configured to service the first powerplant component using a first working fluid in the first fluid circuit. The first fluid circuit includes a first circuit reservoir, a first circuit pump and a first circuit path extending through the first circuit reservoir, the first circuit pump and the first inter-circuit heat exchanger. The second fluid circuit is fluidly independent of the first fluid circuit. The second fluid circuit is configured to service the second powerplant component using a second working fluid in the second fluid circuit. The second fluid circuit includes a second circuit reservoir, a second circuit pump and a second circuit path extending through the second circuit reservoir, the second circuit pump and the first inter-circuit heat exchanger.
1 . An assembly for an aircraft powerplant, comprising:
a first electric machine comprising a first powerplant component;
a second electric machine comprising a second powerplant component;
a first inter-circuit heat exchanger;
a first fluid circuit configured to service the first powerplant component using a first working fluid in the first fluid circuit, the first fluid circuit including a first circuit reservoir, a first circuit pump and a first circuit path extending through the first circuit reservoir, the first circuit pump and the first inter-circuit heat exchanger; and
a second fluid circuit fluidly independent of the first fluid circuit, the second fluid circuit configured to service the second powerplant component using a second working fluid in the second fluid circuit, the second fluid circuit including a second circuit reservoir, a second circuit pump and a second circuit path extending through the second circuit reservoir, the second circuit pump and the first inter-circuit heat exchanger.
2 . The assembly of claim 1 , wherein the first inter-circuit heat exchanger is dedicated to transferring heat energy between the first working fluid in the first fluid circuit and the second working fluid in the second fluid circuit.
3 . The assembly of claim 1 , further comprising a lubricant circuit comprising a lubricant circuit path extending through the first inter-circuit heat exchanger.
4 . The assembly of claim 1 , further comprising a fuel circuit comprising a fuel circuit path extending through the first inter-circuit heat exchanger.
5 . The assembly of claim 4 , further comprising:
a second inter-circuit heat exchanger fluidly coupled inline along the first circuit path and the second circuit path; and
a lubricant circuit comprising a lubricant circuit path extending through the second inter-circuit heat exchanger.
6 . The assembly of claim 1 , wherein
the first fluid circuit further includes a first circuit heat exchanger, and the first circuit path further extending through the first circuit heat exchanger; and
the second fluid circuit further includes a second circuit heat exchanger, and the second circuit path further extending through the second circuit heat exchanger.
7 . The assembly of claim 1 , wherein at least one of
the first circuit path further extends through the first powerplant component; or
the second circuit path further extends through the second powerplant component.
8 . The assembly of claim 1 , further comprising at least one of
a first component heat exchanger thermally coupling the first powerplant component to the first working fluid in the first fluid circuit, the first circuit path further extending through the first component heat exchanger; or
a second component heat exchanger thermally coupling the second powerplant component to the second working fluid in the second fluid circuit, the second circuit path further extending through the second component heat exchanger.
9 . The assembly of claim 1 , wherein at least one of
the first circuit pump is configured with the first powerplant component in a first line replaceable unit; or
the second circuit pump is configured with the second powerplant component in a second line replaceable unit.
10 . The assembly of claim 1 , wherein at least one of
the first circuit reservoir is configured with the first powerplant component in a first line replaceable unit; or
the second circuit reservoir is configured with the second powerplant component in a second line replaceable unit.
11 . The assembly of claim 1 , wherein the first fluid circuit further includes an additional first circuit pump fluidly coupled inline along the first circuit path.
12 . An assembly for an aircraft powerplant, comprising:
a first electric machine controller comprising a first powerplant component;
a second electric machine controller comprising a second powerplant component;
a first inter-circuit heat exchanger;
a first fluid circuit configured to service the first powerplant component using a first working fluid in the first fluid circuit, the first fluid circuit including a first circuit reservoir, a first circuit pump and a first circuit path extending through the first circuit reservoir, the first circuit pump and the first inter-circuit heat exchanger; and
a second fluid circuit fluidly independent of the first fluid circuit, the second fluid circuit configured to service the second powerplant component using a second working fluid in the second fluid circuit, the second fluid circuit including a second circuit reservoir, a second circuit pump and a second circuit path extending through the second circuit reservoir, the second circuit pump and the first inter-circuit heat exchanger.
13 . An assembly for an aircraft powerplant, comprising:
an electric machine comprising a first powerplant component;
an electric machine controller comprising a second powerplant component;
a first inter-circuit heat exchanger;
a first fluid circuit configured to service the first powerplant component using a first working fluid in the first fluid circuit, the first fluid circuit including a first circuit reservoir, a first circuit pump and a first circuit path extending through the first circuit reservoir, the first circuit pump and the first inter-circuit heat exchanger; and
a second fluid circuit fluidly independent of the first fluid circuit, the second fluid circuit configured to service the second powerplant component using a second working fluid in the second fluid circuit, the second fluid circuit including a second circuit reservoir, a second circuit pump and a second circuit path extending through the second circuit reservoir, the second circuit pump and the first inter-circuit heat exchanger.
14 . The assembly of claim 13 , wherein the electric machine controller is configured to control operation of the electric machine.
15 . An assembly for an aircraft powerplant, comprising:
a rotating structure comprising a bladed rotor;
an electric machine operatively coupled to the rotating structure;
an electric machine controller configured to control operation of the electric machine; and
a fluid circuit configured to cool and/or lubricate at least one of the electric machine or the electric machine controller using a working fluid in the fluid circuit, the fluid circuit including a circuit path, a circuit reservoir, a circuit pump, a radiator, a fuel-to-working fluid heat exchanger and a lubricant-to-working fluid heat exchanger, the circuit path extending through the circuit reservoir, the circuit pump, the radiator, the fuel-to-working fluid heat exchanger and the lubricant-to-working fluid heat exchanger, the radiator configured to transfer first heat energy between the working fluid and air flowing through the radiator, the fuel-to-working fluid heat exchanger configured to transfer second heat energy between the working fluid and fuel flowing through the fuel-to-working fluid heat exchanger, and the lubricant-to-working fluid heat exchanger configured to transfer third heat energy between the working fluid and lubricant flowing through the lubricant-to-working fluid heat exchanger.