Diffuser guide vane with deflector panel having curved profile
A guide vane for use in a compressor discharge plenum of a gas turbine engine is disclosed. The guide vane comprises a guide support system, a first side panel, a second side panel, and a deflector panel secured to the mounting system and extending between the first side panel and the second side panel. The deflector panel has a curved profile substantially in accordance with Cartesian coordinate values of X, Y, and Z as set forth in Table 1 where the X, Y, and Z values are in inches from a center point of a bottom surface of the deflector panel. The coordinate values are connected by smooth continuing arcs to form profile sections and the profile sections are joined together smoothly to form the curved profile of the guide vane.
1. A guide vane for a compressor discharge plenum comprising:
a guide support system;
a first side panel and a second side panel; and,
a deflector panel secured to a first mounting system, the deflector panel extending between the first side panel and the second side panel, the deflector panel having a curved profile substantially in accordance with Cartesian coordinate values of X, Y, and Z set forth in Table 1 wherein the X, Y, and Z values are in inches from a center point of a bottom surface of the deflector panel, and when connected by smooth continuing arcs, define profile sections of the deflector panel, which when joined smoothly with one another form the curved profile.
2. The guide vane of claim 1 forming a flow path in the compressor discharge plenum between a compressor and a combustor of a gas turbine engine.
3. The guide vane of claim 2 , wherein the guide vane directs compressed air from the compressor to cool a transition duct and the combustor.
4. The guide vane of claim 1 further comprising a second mounting system for mounting the guide vane to a compressor discharge case.
5. The guide vane of claim 4 , wherein the second mounting system is coupled to a bullhorn bracket, which in turn supports a transition duct.
6. The guide vane of claim 1 , wherein the deflector panel is configured to reduce flow separation for air passing through the compressor discharge plenum.
7. The guide vane of claim 1 , wherein the deflector panel has a height measured from a midpoint of a lower-most section to an upper most section of approximately 18 inches.
8. The guide vane of claim 1 , wherein the deflector panel is fabricated from a stainless steel.
9. A guide vane for a compressor discharge plenum comprising:
a guide support system;
a first side panel and a second side panel; and,
a deflector panel secured to a first mounting system, the deflector panel extending between the first side panel and the second side panel, the deflector panel having a curved profile within an envelope of approximately −0.050 to +0.050 inches in a direction normal to any surface location of the curved profile, where the curved profile is substantially in accordance with Cartesian coordinate values of X, Y, and Z set forth in Table 1 wherein the X, Y, and Z values are in inches from a center point of a bottom surface of the deflector panel, and when connected by smooth continuing arcs, define profile sections of the deflector panel, and which when joined smoothly with one another form the curved profile.
10. The guide vane of claim 9 forming a part of the compressor discharge plenum between a compressor and a combustor of a gas turbine engine.
11. The guide vane of claim 10 , wherein the guide vane directs compressed air from the compressor to cool a transition duct and the combustor.
12. The guide vane of claim 9 further comprising a second mounting system for mounting the guide vane to a compressor discharge case.
13. The guide vane of claim 9 , wherein the deflector panel is configured to reduce flow separation for air passing through the compressor discharge plenum.
14. The guide vane of claim 9 , wherein the deflector panel has a height measured from a midpoint of a lower-most section to an upper most section of approximately 18 inches.
15. The guide vane of claim 9 , wherein the deflector panel is fabricated from a stainless steel.
16. A compressor discharge region of a gas turbine engine comprising:
a compressor discharge case;
a bullhorn bracket coupled to a portion of the compressor discharge case; and,
a guide vane for directing air flow in a compressor discharge plenum comprising a guide support system, a first side panel and a second side panel, and a deflector panel secured to the guide support system and extending between the first side panel and the second side panel, the deflector panel having a curved profile substantially in accordance with Cartesian coordinate values of X, Y, and Z set forth in Table 1 wherein the X, Y, and Z values are in inches from a center point of a bottom surface of the deflector panel, and when connected by smooth continuing arcs, define profile sections of the deflector panel, which when joined smoothly with one another form the curved profile, the guide vane coupled to the bullhorn bracket.
17. The compressor discharge region of claim 16 , wherein the bullhorn bracket is also coupled to a transition duct.
18. The compressor discharge region of claim 17 , wherein the guide vane further comprises a mounting system coupled to the bullhorn bracket.
19. The compressor discharge region of claim 18 , wherein the deflector panel is configured to reduce flow separation for air passing through the compressor discharge plenum.
20. The guide vane of claim 19 , wherein the deflector panel is fabricated from a stainless steel and has a height measured from a midpoint of a lower-most section to an upper most section of approximately 18 inches.