Motorless mass flowmeter

• US 8,205,508 B2
• Filed: 01/12/2010
• Issued: 06/26/2012
• Est. Priority Date: 01/12/2010
• Status: Active Grant

• Current Assignee: Meggitt New Hampshire Inc (Parker-Hannifin Corporation)
• Original Assignee: Meggitt New Hampshire Inc (Parker-Hannifin Corporation)
• Inventors: Healey, Christopher J
• Primary Examiner(s): PATEL, HARSHAD R
• Application Number:
  US12/686,004
• Publication Number:
  US 20110167927A1
• Time in Patent Office: 896 Days
• Field of Search: None
• US Class Current: 73/861.352
• CPC Class Codes: F03B 13/00 Adaptations of machines or engines for special use; Combinations of machines or engines with driving or driven apparatus if the apparatus aspects are predominant, see the relevant subclasses for such apparatus, e.g. H02K7/18; Power stations or aggregates incorporating only machines or engines of positive-displacement type F03C; hydraulic engineering aspects E02B; combinations with wind energy converters F03D9/008
• CPC Class Codes: G01F 1/82 using a driven wheel as impeller and one or more other wheels or moving elements which are angularly restrained by a resilient member, e.g. spring member as the measuring device
• CPC Class Codes: G01F 15/00 Details of, or accessories for, apparatus of groups G01F1/00 - G01F13/00 insofar as such details or appliances are not adapted to particular types of such apparatus
• CPC Class Codes: Y10T 137/87249 Multiple inlet with multiple outlet

Abstract

A motorless mass flowmeter in accordance with one embodiment of the invention comprises a turbine subassembly, a drum, and an impeller. The drum is rigidly connected to the turbine subassembly such that the drum rotates in accompaniment to rotation of the turbine subassembly. The impeller is rotationally coupled to the drum by way of a spring that allows relative rotation against the bias of the spring. The turbine subassembly has jets and bypass valves. The turbine subassembly may be implemented in the form of a laminated bypass valve structure. The laminated bypass valve structure may include an entrance layer having entrance port(s), a closure layer having closure member(s), an exit layer defining exit passage(s), and an intermediary layer forming conduit(s) for guiding fluid from entrance port(s) to exit passage(s).

Claims

1. A motorless mass flowmeter having an inlet and an outlet for flow of fluid therethrough, the mass flowmeter comprising:

a turbine subassembly;

a drum rigidly connected to the turbine subassembly such that the drum rotates in accompaniment to rotation of the turbine subassembly; and

an impeller rotationally coupled to the drum by way of a spring that allows relative rotation against the bias of the spring;

wherein the turbine subassembly has a first set of jets causing a first torque to be applied about a rotational axis of the turbine subassembly as fluid flows therethrough, the first torque tending to cause the turbine subassembly to rotate in a first direction;

the turbine subassembly has a second set of jets causing a second torque to be applied about the rotational axis of the turbine subassembly as fluid flows therethrough; and

a first set of one or more bypass valves causing an increasing amount of fluid to be diverted from the first set of jets to the second set of jets with increasing flow of fluid through the mass flowmeter.

2. A motorless mass flowmeter according to claim 1 wherein the second torque tends to cause the turbine subassembly to rotate in the same direction as the first torque.

3. A motorless mass flowmeter according to claim 1 wherein the second torque tends to cause the turbine subassembly to rotate in a second direction that is opposite the first direction.

4. A motorless mass flowmeter according to claim 1 wherein the diversion of fluid from the first set of jets to the second set of jets and the application of the second torque about the rotational axis of the turbine subassembly by the first set of bypass valves only occurs when flow of fluid through the mass flowmeter is above a first threshold value.

5. A motorless mass flowmeter according to claim 1 wherein the turbine subassembly furthermore has

a third set of jets causing a third torque to be applied about the rotational axis of the turbine subassembly as fluid flows therethrough;

and

a second set of one or more bypass valves causing an increasing amount of fluid to be diverted from the first set of jets to the third set of jets with increasing flow of fluid through the mass flowmeter.

6. A motorless mass flowmeter according to claim 5 wherein the third torque tends to cause the turbine subassembly to rotate in the same direction as the first torque.

7. A motorless mass flowmeter according to claim 5 wherein the third torque tends to cause the turbine subassembly to rotate in a second direction that is opposite the first direction.

8. A motorless mass flowmeter according to claim 5 wherein the diversion of fluid from the first set of jets to the third set of jets and the application of the third torque about the rotational axis of the turbine subassembly by the second set of bypass valves only occurs when flow of fluid through the mass flowmeter is above a second threshold value.

9. A motorless mass flowmeter according to claim 5 wherein the turbine subassembly furthermore has

a third set of one or more bypass valves causing an increasing amount of fluid to be diverted away from the first set of jets with increasing flow of fluid through the mass flowmeter, this diversion of fluid away from the first set of jets by the third set of bypass valves causing application of substantially no torque about the rotational axis of the turbine subassembly.

10. A motorless mass flowmeter according to claim 9 wherein the diversion of fluid away from the first set of jets with application of substantially no torque about the rotational axis of the turbine subassembly by the third set of bypass valves only occurs when flow of fluid through the mass flowmeter is above a third threshold value.

11. A motorless mass flowmeter according to claim 1 wherein the mass flowmeter furthermore comprises:

an internal flow straightener disposed downstream from the turbine subassembly and upstream from the impeller, the internal flow straightener reducing angular momentum of fluid as it passes from the turbine subassembly to the impeller; and

a viscous decoupler disposed at the upstream side of the impeller, the viscous decoupler substantially preventing viscous drag of fluid from adversely affecting rotation of the impeller.