Support system for a pilot nozzle of a turbine engine
View Patent ↗An automatic recovery pilot nozzle support system for supporting a pilot nozzle in a fuel injection system of a turbine engine. The support system includes a sleeve extending from an orifice in a support housing, wherein the sleeve has a hollow opening for containing a pilot nozzle. The sleeve may increase the natural frequency of the pilot nozzle above an excitation zone, thereby limiting destructive vibrations. The sleeve may be attached to the support housing with an interference fit. The automatic recovery aspect of the support system enables the sleeve to maintain an interference fit with the support housing such that anytime the sleeve looses contact with the support housing, an insulative film of air forms between the sleeve and the support housing. The insulative film of air causes the temperature of the sleeve to increase, and the sleeve to expand and reform the interference fit with the support housing.
1. An automatic recovery fuel nozzle support system of a turbine engine, comprising:
a support housing having at least one orifice; and
a hollow sleeve positioned in the at least one orifice and having a pre-installation outer diameter that is greater than an inner diameter of the at least one orifice of the support housing such that an interference fit exists between the support housing and the hollow sleeve;
a nozzle positioned in the at least one orifice of the hollow sleeve and generally aligned with the hollow sleeve.
2. The automatic recovery fuel nozzle support system of claim 1 , wherein the support housing further comprises a collar surrounding the orifice and forming at least a portion of the orifice.
3. The automatic recovery fuel nozzle support system of claim 2 , wherein the collar extends from a base of the support housing towards an unsupported end of the sleeve to a point that is less than about half of a total length of the sleeve from the base.
4. The automatic recovery fuel nozzle support system of claim 3 , wherein the collar extends from a base of the support housing towards the unsupported end of the sleeve to a point that is about one third of a total length of the sleeve from the base.
5. The automatic recovery fuel nozzle support system of claim 3 , wherein at least a portion of the collar proximate the unsupported end of the sleeve has an inner diameter that is slightly less than inner diameters of the orifice at other locations.
6. The automatic recovery fuel nozzle support system of claim 3 , wherein the sleeve further comprises a retention protrusion extending from a base of the sleeve.
7. The automatic recovery fuel nozzle support system of claim 6 , wherein the retention protrusion is a ring coupled to the base of the sleeve.
8. The automatic recovery fuel nozzle support system of claim 1 , wherein the sleeve has a first region proximate to the support housing having a first diameter and a second region having a second diameter located proximate to an unsupported end of the sleeve, wherein the first diameter is larger than the second diameter.
9. The automatic recovery fuel nozzle support system of claim 8 , wherein the portion of the sleeve having the second diameter is sized to contact a fuel nozzle when the fuel nozzle is inserted into the sleeve.
10. An automatic recovery support system for a pilot nozzle of a turbine engine, comprising:
a support housing having at least one orifice;
a hollow sleeve positioned in the at least one orifice and having a pre-installation outer diameter that is greater than an inner diameter of the at least one orifice of the support housing such that an interference fit exists between the support housing and the hollow sleeve; and
a pilot nozzle positioned in and supported by the hollow sleeve and generally aligned with the hollow sleeve.
11. The automatic recovery support system of claim 10 , wherein the support housing further comprises a collar surrounding the orifice and forming at least a portion of the orifice, and wherein the collar extends from a base of the support housing towards an unsupported end of the sleeve to a point that is less than half a total length of the sleeve from the base.
12. The automatic recovery support system of claim 11 , wherein the collar extends from the base of the support housing towards the unsupported end of the sleeve to a point that is about one third of a total length of the sleeve from the base.
13. The automatic recovery support system of claim 11 , wherein a portion of the collar proximate the unsupported end of the sleeve has an inner diameter that is slightly less than inner diameters of the orifice at other locations.
14. The automatic recovery support system of claim 11 , wherein the sleeve further comprises a ring extending from a base of the sleeve.
15. The automatic recovery support system of claim 10 , wherein the sleeve has a first region proximate to the support housing having a first diameter and a second region having a second diameter located proximate to an unsupported end of the sleeve, wherein the first diameter is larger than the second diameter, and the second diameter is sized to contact a pilot nozzle when the pilot nozzle is inserted into the sleeve.