Coupling assembly for a turbine engine
A coupling assembly for a turbine engine. The coupling assembly includes a cold side component, a hot side component, and a fastening mechanism. The cold side component and the hot side component together at least partially form a combustion chamber. The fastening mechanism couples the hot side component to the cold side component. The fastening mechanism includes a stud disposed through the cold side component and a cap positioned on the stud. The cap defines a hollow interior and includes one or more first cap cooling holes. The one or more first cap cooling holes operably direct cooling air into the hollow interior such that the hollow interior provides a cushion of air between the combustion chamber and the stud.
1. A coupling assembly for a turbine engine, the coupling assembly comprising:
a cold side component having a first fastening mechanism aperture disposed therethrough;
a hot side component, the cold side component and the hot side component together at least partially forming a combustion chamber, wherein the hot side component has a second fastening mechanism aperture disposed therethrough; and
a fastening mechanism coupling the hot side component to the cold side component, the fastening mechanism comprising:
a stud disposed through the first fastening mechanism aperture of the cold side component; and
a cap positioned on the stud and within the second fastening mechanism aperture of the hot side component, the cap defining a hollow interior and including one or more first cap cooling holes that operably direct cooling air into the hollow interior such that the hollow interior provides a cushion of cooling air between the combustion chamber and the stud, wherein a portion of the stud is disposed within the hollow interior such that the hollow interior surrounds the stud.
2. The coupling assembly of claim 1 , wherein a space is defined between the cold side component and the hot side component, the stud being disposed in the space.
3. The coupling assembly of claim 1 , wherein the cap is disposed through the hot side component.
4. The coupling assembly of claim 1 , wherein the cap is positioned between the stud and the combustion chamber.
5. The coupling assembly of claim 1 , wherein the stud is radially spaced from the combustion chamber such that the stud is insulated from the combustion chamber.
6. The coupling assembly of claim 1 , wherein the cap includes one or more second cap cooling holes that operably direct the cooling air from the hollow interior into the combustion chamber.
7. The coupling assembly of claim 1 , wherein the hollow interior includes a diameter that is larger than an outer diameter of the stud.
8. The coupling assembly of claim 1 , wherein a shape of the hollow interior generally corresponds to a shape of the cap.
9. The coupling assembly of claim 1 , further comprising a washer disposed between the cold side component and the hot side component, the washer being flexible such that the hot side component moves with respect to the cold side component and the washer prevents the hot side component from contacting the cold side component.
10. The coupling assembly of claim 9 , wherein the washer includes one or more washer cooling holes that operably direct cooling air towards the cap.
11. The coupling assembly of claim 10 , wherein the washer includes one or more washer slots that extend radially inward from an outer edge of the washer to the one or more washer cooling holes.
12. The coupling assembly of claim 1 , wherein the cap has a generally frustoconical shape having an angled side wall.
13. The coupling assembly of claim 12 , wherein the one or more first cap cooling holes extend through the angled side wall and are in fluid communication with a space defined between the cold side component and the hot side component, the one or more first cap cooling holes operably directing the cooling air from the space into the hollow interior.
14. A turbine engine comprising:
a combustion section including a combustion chamber; and
a coupling assembly comprising:
a cold side component having a first fastening mechanism aperture disposed therethrough;
a hot side component, the cold side component and the hot side component together at least partially forming the combustion chamber, wherein the hot side component has a second fastening mechanism aperture disposed therethrough; and
a fastening mechanism coupling the hot side component to the cold side component, the fastening mechanism comprising:
a stud disposed through the first fastening mechanism aperture of the cold side component; and
a cap positioned on the stud and within the second fastening mechanism aperture of the hot side component, the cap defining a hollow interior and including one or more first cap cooling holes that operably direct cooling air into the hollow interior such that the hollow interior provides a cushion of cooling air between the combustion chamber and the stud, wherein a portion of the stud is disposed within the hollow interior such that the hollow interior surrounds the stud.
15. The turbine engine of claim 14 , wherein the cap is disposed through the hot side component.
16. The turbine engine of claim 14 , wherein the cap is positioned between the stud and the combustion chamber.
17. The turbine engine of claim 14 , wherein the stud is spaced radially from the combustion chamber such that the stud is insulated from the combustion chamber.
18. The turbine engine of claim 14 , wherein the cap includes one or more second cap cooling holes that operably direct the cooling air from the hollow interior into the combustion chamber.
19. The turbine engine of claim 14 , wherein the hollow interior includes a diameter that is larger than an outer diameter of the stud.
20. The turbine engine of claim 14 , wherein a shape of the hollow interior generally corresponds to a shape of the cap.