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An example bypass valve includes a sleeve providing a bore that extends along an axis. The sleeve has at least one window. The bypass valve also includes a spool received within the bore. The spool is configured to move within the bore between a first position that restricts flow through at least on

An example bypass valve includes a sleeve providing a bore that extends along an axis. The sleeve has at least one window. The bypass valve also includes a spool received within the bore. The spool is configured to move within the bore between a first position that restricts flow through at least one window and a second position that permits flow through the at least one window of the sleeve. An outer diameter of the spool is from 99.90 to 99.95 percent of a diameter of the bore.

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1. A turbomachine comprising: a combustor;a bypass valve having a sleeve and a spool, the sleeve providing a bore that extends along an axis, the sleeve having at least one window, andthe spool received within the bore, the spool configured to move back and forth within the bore between a first posi

1. A turbomachine comprising: a combustor;a bypass valve having a sleeve and a spool, the sleeve providing a bore that extends along an axis, the sleeve having at least one window, andthe spool received within the bore, the spool configured to move back and forth within the bore between a first position that restricts flow through at least one window and a second position that permits flow through the at least one window of the sleeve, wherein an outer diameter of the spool is from 99.90 to 99.95 percent of a diameter of the bore,wherein the flow moves to the combustor of the turbomachine when the spool is in the first position within the bore. 2. The turbomachine of claim 1, including a solenoid configured to actuate the spool from the first position to the second position. 3. The turbomachine of claim 1, wherein a gain through the at least one window is from 0.00 square inches/0.001 inches to 0.001185 square inches/0.001 inches. 4. The turbomachine of claim 3, wherein gain is a ratio of an area of the at least one window available to communicate fuel to an axial position of the spool within the bore. 5. The turbomachine of claim 1, wherein the at least one window has a low gain portion and a high gain portion. 6. The turbomachine of claim 5, wherein the low gain portion is positioned upstream the high gain portion, such that fuel moves first through the low gain portion and then the high gain portion when the spool moves from the first position to the second position. 7. The turbomachine of claim 1, wherein the first position permits no flow. 8. The turbomachine of claim 1, including a fuel within the bore when the spool is in the second position. 9. A bypass valve comprising: a sleeve providing a bore that extends along an axis, the sleeve having at least one window; anda spool received within the bore, the spool configured to move within the bore between a first position that restricts flow through at least one window and a second position that permits flow through the at least one window of the sleeve, wherein an outer diameter of the spool is from 99.90 to 99.95 percent of a diameter of the bore,wherein the spool moves away from an end of the sleeve when moving from the first position to the second position, and the end of the sleeve is configured to contact a seal, the end of the sleeve having a chamfer that is from 0.001 to 0.005. 10. A bypass valve comprising: a sleeve providing a bore that extends along an axis, the sleeve having at least one window; anda spool slidably received within the bore, the spool configured to move back and forth within the bore between a first position that restricts flow through at least one window and a second position that permits flow through the at least one window of the sleeve, wherein gain through the windows is from 0.00 square inches/0.001 inches to 0.001185 square inches/0.001 inches. 11. The bypass valve of claim 10, including a solenoid configured to actuate the spool from the first position to the second position. 12. The bypass valve of claim 10, wherein a gain through the at least one window is from 0.00 square inches/0.001 inches to 0.000395 square inches/0.001 inches. 13. The bypass valve of claim 12, wherein gain is a ratio of an area of the at least one window available to communicate fuel to an axial position of the spool within the bore. 14. The bypass valve of claim 10, wherein the at least one window has a low gain portion and a high gain portion. 15. The bypass valve of claim 10, wherein the spool moves away from an end of the sleeve when moving from the first position to the second position, and the end of the sleeve is configured to contact a seal, the end of the sleeve having a chamfer that is from 0.001 to 0.005 in the inner diameter of the sleeve. 16. The bypass valve of claim 10, including a fuel within the bore when the spool is in the second position. 17. A turbomachine comprising the bypass valve of claim 10, and further including a combustor, wherein the flow moves to the combustor of the turbomachine when the spool is in the first position within the bore.