IP Library Granted Patent US 10,240,792
Granted Patent B2
US 10,240,792 · App. 15/790,750 · Granted Mar 26, 2019

Directionally biased valve

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Quick Facts
Patent No.
US 10,240,792
App. No.
15/790,750
Granted
Mar 26, 2019
Kind
B2
Abstract

A valve for regulating fluid flowing bidirectionally therethrough includes a first flow body defining a passage configured to direct fluid flow in a downstream direction defined from the inlet to the outlet. The inlet includes an enlargement configured to provide decreased resistance to fluid flow in the downstream direction relative to flow in an upstream direction opposite the downstream direction.

Claims (24)

1. A valve for regulating fluid flowing bidirectionally therethrough, comprising:

a first flow body defining a passage therethrough which includes an inlet, an opposed outlet, and a bore fluidly coupling the inlet and outlet, the passage configured to direct fluid flow in a radially downstream direction defined from the inlet to the outlet, wherein the inlet includes an enlargement configured to provide decreased resistance to fluid flow in the radially downstream direction relative to flow in a radially upstream direction opposite the downstream direction; and

a second flow body operatively associated with and disposed radially outward of the first flow body, the first and second flow bodies defining an annular chamber therebetween in fluid communication with the inlet of the first flow body,

wherein the first and second flow bodies are translatable relative to one another to increase and decrease size of the annular damping chamber to provide increased damping of fluid flow in the radially upstream direction relative to the radially downstream direction, and

wherein relative translation of the first and second flow bodies selectively fluidly couples the passage to the annular chamber.

2. A valve according to claim 1 , wherein the first flow body defines a plurality of additional radially extending passages fluidly coupled to the annular damping chamber, the plurality of additional radially extending passages including two passages longitudinally offset from one another and configured to provide decreased resistance to fluid flow in the radially downstream direction relative to the radially upstream direction.

3. A valve according to claim 2 , wherein the flow bodies are configured such that translation relative to one another causes blocking of at least one passage defined in the first flow body by the second flow body to increase resistance to fluid flow in at least one of the upstream and downstream directions.

4. A method of fuel circuit control on a fuel nozzle for a gas turbine engine, comprising:

at a bidirectional valve having a first flow body and a second flow body operatively associated with the first flow body, the first flow body defining a flow passage therethrough which includes an inlet, an opposed outlet, and a bore fluidly coupling the inlet and outlet, the inlet having an enlargement, wherein the enlargement has an axial length that is smaller than an axial length of a remainder of the bore coupling the inlet to the outlet,

wherein an axial length to flow area width ratio of the remainder of the bore coupling the inlet to the outlet is greater than 1,

receiving a downstream-directed fuel flow at the first flow body

decreasing resistance to the downstream-directed fuel flow at the enlargement of the flow passage inlet defined by the first flow body;

communicating the fuel flow to the outlet of the flow passage through the bore fluidly coupling the flow passage inlet to the flow passage outlet;

issuing the fuel flow from the flow passage with a first discharge coefficient;

receiving a second fuel flow at the outlet of the first flow body;

communicating the second fuel flow to the inlet of the flow passage through the bore fluidly coupling the inlet to the outlet of the flow passage; and

issuing the second fuel flow from the inlet of the flow passage with a second discharge coefficient, wherein the second discharge coefficient is lower than the first discharge coefficient.

5. The method as recited in claim 4 , wherein the flow passage is a first flow passage, the flow body defining a second flow passage therethrough with an inlet, an opposed outlet, and a bore fluidly coupling the inlet and outlet, the inlet having an enlargement, the method further comprising:

flowing the downstream flow through the first flow passage in a radially inward direction; and

flowing the upstream fluid flow in a radially outward direction through the second flow passage.

6. The method as recited in claim 4 , further comprising increasing size of an annular damping chamber between the first flow body and the second flow body during upstream fluid flow; and decreasing size of the annular chamber during downstream fluid flow.

7. The method as recited in claim 4 , further comprising providing increased damping of fluid flow in the upstream direction relative to the downstream direction.

8. The method as recited in claim 4 , further comprising translating the first flow body relative the second flow body to increase size of an annular damping chamber between the first flow body and the second flow body during upstream fluid flow.

9. The method as recited in claim 4 , further comprising translating the first flow body relative to the second flow to decrease size of an annular damping chamber between the first flow body and the second flow body during downstream fluid flow.

Assignments (2)
CHANGE OF NAME Recorded May 23, 2022
From: DELAVAN INC
To: COLLINS ENGINE NOZZLES, INC.
Reel/Frame 060158/0981 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 24, 2017
From: RYON, JASON A.; YU, CHIEN-JUNG; BUELOW, PHILIP E. O.; THOMSON, NEAL A.
To: DELAVAN INC.
Reel/Frame 043930/0822 →