Pressure sensor manifolds for high temperatures
A pressure sensing system includes a housing that houses one or more pressure transducers therein. A tube is sealed to the housing at a first end of the tube. One or more pressure transducers are in fluid communication with a second end of the tube through an inner passage of the tube for sensing pressure at the second end of the tube.
1 . A pressure sensing system comprising:
a housing that houses one or more pressure transducers therein;
a tube sealed to the housing at a first end of the tube; and
one or more pressure transducers in fluid communication with a second end of the tube through an inner passage of the tube for sensing pressure at the second end of the tube, wherein the tube defines a labyrinthine path through a heat exchanger.
2 . The system as recited in claim 1 , wherein the housing includes a manifold flange with one or more pressure transducers in fluid communication with respective ports in the manifold flange.
3 . The system as recited in claim 2 , wherein the tube is integral with the manifold flange.
4 . The system as recited in claim 3 , wherein the tube is welded to the manifold flange at a weld joint that fully seals the respective ports and the inner passage of the tube in fluid communication with one another.
5 . The system as recited in claim 3 , wherein the tube and the manifold flange are metallurgically monolithic.
6 . The system as recited in claim 5 , wherein the tube and the manifold flange are additively manufactured as one piece.
7 . The system as recited in claim 5 , wherein the tube and the manifold flange are machined as a single piece.
8 . The system as recited in claim 3 , wherein the respective ports in the manifold flange are each in fluid communication with the inner passage of the tube.
9 . The system as recited in claim 8 , further comprising a case flange configured to be mounted to a compressor case in fluid communication with an interior flow path of the compressor case, wherein the case flange is connected in fluid communication with the second end of the tube for fluid communication of pressure from the interior flow path of the compressor case, through the case flange, through the inner passage of the tube, and through the ports in the manifold flange, for pressure sensing pressure in the compressor case by the one or more pressure transducers.
10 . The system as recited in claim 3 , wherein the housing includes an enclosure case mounted to the manifold flange to enclose the one or more pressure transducers.
11 . The system as recited in claim 1 , wherein the heat exchanger includes fins radiating outward therefrom for heat exchange with nacelle air external from the tube and heat exchanger.
12 . The system as recited in claim 1 , wherein the housing includes a harness for electrical communication of signals from the one or more pressure transducers to engine control components through the housing.
13 . The system as recited in claim 1 , wherein the one or more pressure transducers comprises a plurality of pressure transducers and the housing includes a manifold flange comprising a plurality of ports, wherein each of the plurality of pressure transducers is in fluid communication with a respective one of the plurality of ports in the manifold flange, and wherein each the plurality of ports is in fluid communication with the inner passage of the tube.
14 . A gas turbine engine system comprising:
an engine case;
a housing that houses one or more pressure transducers therein, wherein the housing includes a manifold flange with the one or more pressure transducers in fluid communication with respective ports in the manifold flange;
a tube sealed to the manifold flange at a first end of the tube, the tube defining a labyrinthine path through a heat exchanger, wherein the respective ports in the manifold flange are each in fluid communication with an inner passage of the tube, wherein the one or more pressure transducers are in fluid communication with a second end of the tube through the inner passage of the tube for sensing pressure at the second end of the tube; and
a case flange configured to be mounted to the engine case in fluid communication with an interior flow path of the engine case, wherein the case flange is connected in fluid communication with the second end of the tube for fluid communication of pressure from the interior flow path of the engine case, through the case flange, through the inner passage of the tube, and through the ports in the manifold flange, for pressure sensing pressure in the engine case by the one or more pressure transducers.
15 . The system as recited in claim 14 , wherein the housing includes an enclosure case mounted to the manifold flange to enclose the one or more pressure transducers.
16 . The system as recited in claim 14 , wherein the heat exchanger includes fins radiating outward therefrom for heat exchange with nacelle air in a nacelle outboard of the engine case.
17 . The system as recited in claim 14 , wherein the engine case is a compressor case of a compressor section upstream of a combustor that is upstream of a turbine section.
18 . The system as recited in claim 14 , wherein the housing includes a harness for electrical communication of signals from the one or more pressure transducers to engine control components through the housing.
19 . The system as recited in claim 14 , wherein the case flange is connected in fluid communication with the engine case through a fitting joint.
20 . The system as recited in claim 14 , wherein the one or more pressure transducers comprises a plurality of pressure transducers, each of the plurality of pressure transducers in fluid communication with one of the respective ports in the manifold flange, wherein each of the respective ports are in fluid communication with the inner passage of the tube.