Flow through cylindrical bores

Patent metadata

Field	Value
Publication number	US-10317073-B2
Application number	US-201213714270-A
Country	US
Kind code	B2
Filing date	Dec 13, 2012
Priority date	Dec 13, 2012
Publication date	Jun 11, 2019
Grant date	Jun 11, 2019

Abstract

A flow directing apparatus for directing fluid flow includes a flow body defining a bore therethrough configured and adapted to direct fluid flowing therethrough. The bore includes an outlet and an opposed inlet with an enlargement, formed as a countersink and/or a chamfer using a suitable boring device. The enlargement is configured and adapted to reduce sensitivity to entrance-edge conditions for the bore.

First claim

What is claimed is:

1. A flow directing apparatus for a gas turbine engine for directing fluid flowing therethrough, comprising:
a flow body defining a bore therethrough configured and adapted to direct fluid flowing therethrough, wherein the bore includes an outlet and an opposed inlet with an enlargement configured and adapted to reduce sensitivity to entrance-edge conditions for the bore, wherein the enlargement of the inlet includes
a countersink with a larger cross-sectional area than that of the bore downstream of the countersink, wherein the countersink has a depth of about 15% of the diameter of the bore where the bore angle is about 0° relative to the inlet surface.

2. The flow directing apparatus as recited in claim 1 , wherein the flow body includes an inlet surface in which the inlet of the bore is defined, and an opposed outlet surface in which the outlet of the bore is defined, wherein the bore defines a longitudinal axis that is angled relative to at least one of the inlet and outlet surfaces for imparting swirl onto a fluid flow through the flow directing apparatus.

3. The flow directing apparatus as recited in claim 1 , wherein the flow body includes an inlet surface in which the inlet of the bore is defined, and an opposed outlet surface in which the outlet of the bore is defined, wherein the bore defines a longitudinal axis that is angled relative to at least one of the inlet and outlet surfaces for imparting swirl onto a flow through the flow directing apparatus, and wherein the inlet of the bore includes a chamfer defined along a chamfer axis which extends traverse relative to the inlet surface and the longitudinal axis of the bore.

4. The flow directing apparatus of claim 1 , wherein the enlargement of the inlet includes a countersink with a larger cross-sectional area than that of the bore downstream of the countersink.

5. The flow directing apparatus of claim 4 , wherein the countersink has a diameter between about 30% and about 75% greater than that of the bore downstream of the countersink.

6. A flow directing apparatus for a gas turbine engine for directing fluid flowing therethrough, comprising:
a flow body defining an inlet surface and an opposed outlet surface with a plurality of bores defined through the flow body from the inlet surface to the outlet surface, wherein each bore is configured and adapted to direct fluid flowing therethrough and includes an outlet and an opposed inlet with an enlargement configured and adapted to reduce sensitivity to entrance-edge conditions for the bore, wherein the enlargement of the inlet includes
a countersink with a larger cross-sectional area than that of the bore downstream of the countersink, wherein the countersink depth varies depending upon the an angle of the bore relative to the inlet surface,

wherein at least one of the plurality of bores include a countersink having a depth of about 15% of the diameter of the bore where the bore angle is about 0° relative to the inlet surface.

7. The flow directing apparatus as recited in claim 6 , wherein the enlargement of each inlet includes a chamfer that has a depth larger than about 15% of a diameter of the bore downstream of the chamfer.

8. The flow directing apparatus as recited in claim 6 , wherein the flow body includes an inlet surface in which the inlet of each bore is defined, and an opposed outlet surface in which the outlet of each bore is defined, wherein each bore defines a longitudinal axis that is angled relative to at least one of the inlet and outlet surfaces for imparting swirl onto a fluid flow through the flow directing apparatus.

9. The flow directing apparatus as recited in claim 6 , wherein the flow body includes an inlet surface in which the inlet of each bore is defined, and an opposed outlet surface in which the outlet of each bore is defined, wherein each bore defines a longitudinal axis that is angled relative to at least one of the inlet and outlet surfaces for imparting swirl to a fluid flow through the flow directing apparatus, and wherein the inlet of each bore includes a chamfer that is defined along a chamfer axis extending traverse relative to the inlet surface and the longitudinal axis of the bore.

10. The flow directing apparatus as recited in claim 6 , wherein the enlargement of each inlet includes a countersink with a larger cross-sectional area than that of the bore downstream of the countersink, and wherein the countersink has a diameter between about 30% and about 75% greater than that of the bore downstream of the countersink.

11. The flow directing apparatus as recited in claim 6 , wherein the enlargement of the each inlet includes a countersink with a larger cross-sectional area than that of the bore downstream of the countersink.

12. A flow directing apparatus for a gas turbine engine for directing fluid flowing therethrough, comprising:
a flow body defining a bore therethrough configured and adapted to direct fluid flowing therethrough, wherein the bore includes an outlet and an opposed inlet with an enlargement configured and adapted to reduce sensitivity to entrance-edge conditions for the bore, wherein the enlargement of the inlet includes
a countersink with a larger cross-sectional area than that of the bore downstream of the countersink, wherein the countersink has a depth of about 100% of the diameter of the bore where the bore angle is about 60° relative to the inlet surface.

Assignees

• Delavan Inc

Inventors

• Buelow Philip E O
• Ryon Jason
• Myers Steve J

Classifications

• F23D11/107

  at least one of both being subjected to a swirling motion · CPC title

• F23D14/58 Primary

  characterised by the shape or arrangement of the outlet or outlets from the nozzle, e.g. of annular configuration · CPC title

• Y10T29/49996

  Successive distinct removal operations · CPC title

• B05B7/10

  producing a swirling discharge · CPC title

• F23R3/12

  inducing a vortex · CPC title