Sensor system having a sensor supported by a mast for use within fluid flows

Patent metadata

Field	Value
Publication number	US-10126208-B2
Application number	US-201615287459-A
Country	US
Kind code	B2
Filing date	Oct 6, 2016
Priority date	Oct 22, 2015
Publication date	Nov 13, 2018
Grant date	Nov 13, 2018

Abstract

A sensor system includes a sensor and a mast on which the sensor is mounted. The mast includes a core body and a shroud, wherein the shroud is provided about the core body, and the shroud is independently rotatable with respect to the core body under the influence, in use, of a fluid flow flowing past the shroud. The shroud is shaped so that, from at least one fluid flow direction, the shroud presents a different flow resistance in dependence upon the rotational orientation of the shroud. The rotational orientation of the shroud adjusts to reduce the flow resistance produced by the shroud to the fluid flow in response to the commencement of, or a change in the fluid flow direction to, one of the at least one fluid flow direction.

First claim

The invention claimed is:

1. A sensor system comprising:
a sensor; and
a mast on which the sensor is mounted, the mast including:
a core body, and
a plurality of shrouds, wherein:
each of the plurality of shrouds is provided about the core body and each of the plurality of shrouds is independently rotatable with respect to the core body under the influence, in use, of a fluid flow flowing past the plurality of shrouds, and
each of the plurality of shrouds is shaped so that, from at least one fluid flow direction, each of the plurality of shrouds presents a different flow resistance in dependence upon a rotational orientation of the respective shroud, such that the rotational orientation of the shroud adjusts to reduce the flow resistance produced by the respective shroud to the fluid flow in response to the commencement of, or a change in the fluid flow direction to, one of the at least one fluid flow direction.

2. The sensor system according to claim 1 , wherein each of the plurality of shrouds has an aerofoil shape.

3. The sensor system according to claim 1 , wherein a chord of each of the plurality of shrouds is substantially perpendicular to an axis of rotation of the respective shroud.

4. The sensor system according to claim 1 , wherein a bearing is provided between the core body and the plurality of shrouds.

5. The sensor system according to claim 1 , wherein the plurality of shrouds extend for substantially the full length of the mast.

6. The sensor system according to claim 1 , wherein the sensor is mounted on the core body.

7. The sensor system in accordance with claim 1 , wherein:
the core body has a proximal end and an opposite distal end that define a length of the mast,
the proximal end of the core body extends from a first one of the plurality of shrouds and the distal end of the core body extends from a second one of the plurality of shrouds that is furthest from the first one of the plurality of shrouds, and
the sensor is provided at a portion of the distal end that extends from the second one of the plurality of shrouds.

8. The sensor system in accordance with claim 1 , further comprising a duct in which the sensor is positioned and through which, in use, the fluid flow is passed.

9. The sensor system in accordance with claim 8 , wherein the largest dimension of the mast extends in a longitudinal direction between proximal and distal ends of the mast, the mast being adapted to be secured to the duct at or adjacent the proximal end.

10. The sensor system according to claim 9 , wherein the sensor is provided at or adjacent the distal end.

11. The sensor system according to claim 9 , wherein the distal end of the mast is a free end.

12. The sensor system according to claim 9 , wherein the axis of rotation of each of the plurality of shrouds is parallel to the longitudinal direction.

13. A gas turbine engine comprising a sensor system including:
a sensor; and
a mast on which the sensor is mounted, the mast including:
a core body, and
a plurality of shrouds, wherein:
each of the plurality of shrouds is provided about the core body and each of the plurality of shrouds is independently rotatable with respect to the core body under the influence, in use, of a fluid flow flowing past the plurality of shrouds, and
each of the plurality of shrouds is shaped so that, from at least one fluid flow direction, each of the plurality of shrouds presents a different flow resistance in dependence upon a rotational orientation of the respective shroud, such that the rotational orientation of the shroud adjusts to reduce the flow resistance produced by the respective shroud to the fluid flow in response to the commencement of, or a change in the fluid flow direction to, one of the at least one fluid flow direction.

14. A test rig comprising a sensor system including:
a sensor; and
a mast on which the sensor is mounted, the mast including:
a core body, and
a plurality of shrouds, wherein:
each of the plurality of shrouds is provided about the core body and each of the plurality of shrouds is independently rotatable with respect to the core body under the influence, in use, of a fluid flow flowing past the plurality of shrouds, and
each of the plurality of shrouds is shaped so that, from at least one fluid flow direction, each of the plurality of shrouds presents a different flow resistance in dependence upon a rotational orientation of the respective shroud, such that the rotational orientation of the shroud adjusts to reduce the flow resistance produced by the respective shroud to the fluid flow in response to the commencement of, or a change in the fluid flow direction to, one of the at least one fluid flow direction.

Assignees

• Rolls Royce Plc

Inventors

• Bianchi Stefano
• Namgoong Howoong

Classifications

• G01F15/18

  Supports or connecting means for meters · CPC title

• G01P5/10

  by measuring thermal variables · CPC title

• G01P5/12

  using variation of resistance of a heated conductor · CPC title

• G01F1/684

  Structural arrangements; Mounting of elements, e.g. in relation to fluid flow · CPC title

• G01M15/14 Primary

  Testing gas-turbine engines or jet-propulsion engines · CPC title