Methods of manufacturing turbomachines having decoupled collectors
Turbomachines such as air dynamometers are disclosed that include a radial outflow compressor and gas collector. In some examples, the gas collector is designed as a separate component that is coupled to the machine, such as coupled to a frame. In some examples, the collector and frame are intentionally spaced and coupled at discrete points to minimize the transfer of mechanical and thermal energy therebetween. Aspects of the present disclosure also include turbomachines that include at least one impeller bypass flow path for the direct transfer of air between ambient and a location in the collector downstream of the impeller blades. In some examples, such flowpath(s) may allow for the inflow of external ambient air into the collector. Methods of manufacturing turbomachines having decoupled collectors are also disclosed.
1. A method of manufacturing a turbomachine including a collector, a frame, and a compressor having an impeller and adjustable shrouds, the impeller having a plurality of impeller blades, the method comprising:
providing mechanical and thermal attenuation between the collector, compressor, and frame by independently supporting the collector and compressor by the frame, to minimize, during operation, the transfer of mechanical and thermal energy between the collector and compressor,
incorporating at least one impeller bypass flow path for the direct transfer of air between ambient and a location in the collector downstream of the impeller blades; and
providing the at least one impeller bypass flow path between the collector and the adjustable shrouds.
2. The method of claim 1 , wherein the adjustable shrouds include first and second shrouds located on opposed sides of the impeller blades, wherein the first and second shrouds are coupled to the frame, and further including moving the first and second shrouds to control a volume of air transferred from the impeller to the collector.
3. A method of manufacturing a turbomachine, the method comprising:
coupling a compressor to a frame so that, when the turbomachine is assembled, the frame supports the compressor, wherein the compressor comprises impeller blades and at least one shroud for the impeller blades;
locating a collector relative to the compressor so that, during operation of the turbomachine, the compressor outputs an energized working fluid to the collector;
coupling the collector to the frame so that, when the turbomachine is assembled, the frame supports the collector independently relative to the compressor;
incorporating at least one impeller bypass flow path for direct transfer of air between ambient and a location within the collector fluidly downstream of the impeller blades; and
providing the at least one impeller bypass flow path between the collector and the at least one shroud.
4. The method of claim 3 , wherein the compressor is a radial outflow compressor.
5. The method of claim 4 , wherein the turbomachine is an air dynamometer configured for testing rotational machinery.
6. The method of claim 3 , wherein the compressor comprises a cast iron housing, and the collector comprises sheet metal.
7. The method of claim 3 , wherein the at least one shroud is an adjustable shroud that allows a user to change operating characteristics of the turbomachine.
8. The method of claim 3 , wherein the compressor is a radial outflow compressor.
9. The method of claim 3 , wherein coupling the collector to the frame includes coupling the collector to the frame using a plurality of discrete brackets.
10. The method of claim 9 , wherein each of the discrete brackets is selected to inhibit transfer of vibration between the collector and the frame.
11. The method of claim 10 , wherein each of the discrete brackets comprises an isolation mount.
12. The method of claim 9 , wherein:
the frame is a U-shaped frame comprising a base, a pair of spaced-apart vertical supports integrated with the base, and a pair of cross braces extending between the pair of spaced-apart vertical supports proximate to opposite ends of the frame;
coupling the compressor to the frame includes coupling a pair of shaft bearings, respectively, to the pair of spaced-apart vertical supports; and
coupling the compressor to the frame includes coupling the collector to the pair of cross braces.
13. The method of claim 12 , wherein the compressor is a radial outflow compressor.
14. The method of claim 13 , wherein the collector includes:
spaced-apart first and second sidewalls;
first and second end walls located at opposite ends of the first and second sidewalls;
a first annular inlet formed in the first sidewall; and
a second annular inlet formed in the second sidewall and located in registration with the first annular inlet, wherein the radial outflow compressor extends through the first and second annular inlets;
wherein each of the first and second annular inlets is located closer to the first end wall than to the second end wall.
15. The method of claim 3 , wherein:
the compressor is a radial outflow compressor; and
the collector includes:
spaced-apart first and second sidewalls;
first and second end walls located at opposite ends of the first and second sidewalls;
a first annular inlet formed in the first sidewall; and
a second annular inlet formed in the second sidewall and located in registration with the first annular inlet, wherein the radial outflow compressor extends through the first and second annular inlets;
wherein each of the first and second annular inlets is located closer to the first end wall than to the second end wall.
16. The method of claim 3 , wherein:
the frame is a U-shaped frame comprising a base, a pair of spaced-apart vertical supports integrated with the base, and a pair of cross braces extending between the pair of spaced-apart vertical supports proximate to opposite ends of the frame;
coupling the compressor to the frame includes coupling a pair of shaft bearings, respectively, to the pair of vertical supports; and
coupling the compressor to the frame includes coupling the collector to the pair of cross braces.
17. The method of claim 12 , wherein the compressor is a radial outflow compressor.
18. The method of claim 17 , wherein the collector includes:
spaced-apart first and second sidewalls;
first and second end walls located at opposite ends of the first and second sidewalls;
a first annular inlet formed in the first sidewall; and
a second annular inlet formed in the second sidewall and located in registration with the first annular inlet, wherein the radial outflow compressor extends through the first and second annular inlets;
wherein each of the first and second annular inlets is located closer to the first end wall than to the second end wall.
19. The method of claim 3 , wherein coupling the collector to the frame is performed for the purpose of attenuating transfer of mechanical energy between the collector and the compressor.
20. The method of claim 19 , wherein coupling the collector to the frame is further performed for the purpose of attenuating transfer of thermal energy between the collector and the compressor.