Fluted compressor flowpath

• US 6,561,761 B1
• Filed: 02/18/2000
• Issued: 05/13/2003
• Est. Priority Date: 02/18/2000
• Status: Expired due to Term

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Breeze-Stringfellow, Andrew, Decker, John J.
• Primary Examiner(s): Ryznic, John E.
• Application Number:
  US09/507,408
• Time in Patent Office: 1,180 Days
• Field of Search: 415/173.1, 415/173.6, 415/207, 415/221, 415/227, 415/208.1, 415/224.5, 415/191, 415/210.1, 415/181
• US Class Current: 415/173.1
• CPC Class Codes: F01D 5/143 Contour of the outer or inner working fluid flow path wall, i.e. shroud or hub contour
• CPC Class Codes: F04D 29/321 for axial flow compressors
• CPC Class Codes: F04D 29/681 especially adapted for elastic fluid pumps
• CPC Class Codes: F05D 2250/70 Shape
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A compressor flowpath includes circumferentially spaced apart airfoils having axially spaced apart leading and trailing edges and radially spaced apart outer and inner ends. An outer wall bridges the airfoil outer ends, and an inner wall bridges the inner ends. One of the walls includes a flute adjacent the leading edges for locally increasing flow area thereat.

Claims

1. A compressor flowpath for diffusing air comprising:

a plurality of airfoils spaced circumferentially apart, and each including axially spaced apart leading and trailing edges and radially spaced apart outer and inner ends;

a radially outer wall bridging said airfoils at said outer ends, and a radially inner wall bridging said airfoils at said inner ends; and

at least one of said walls includes a circumferentially concave flute adjacent said leading edges for locally increasing flow area thereat.

2. A flowpath according to claim 1 wherein said flute terminates axially forward of said trailing edges.

3. A flowpath according to claim 2 wherein said flute extends in width circumferentially between said leading edges and extends in length axially aft therefrom.

4. A flowpath according to claim 3 wherein said flute decreases in width from said leading edges toward said trailing edges.

5. A flowpath according to claim 4 wherein:

each of said airfoils further includes a generally convex suction side, and a circumferentially opposite, generally concave pressure side; and

said flute adjoins said suction side of one airfoil, and diverges from said pressure side of an adjacent airfoil.

6. A flowpath according to claim 5 wherein said flute is circumferentially concave adjacent one airfoil and transitions to a circumferentially convex land adjoining an opposite airfoil.

7. A flowpath according to claim 3 wherein said flute commences axially forward of said leading edges.

8. A flowpath according to claim 7 wherein said flute is substantially uniform in width from said commencement thereof to said leading edges and then is substantially uniform in width toward said termination thereof.

9. A flowpath according to claim 3 wherein:

said airfoils comprise fan rotor blades extending radially outwardly from a supporting disk;

said outer wall comprises an annular fan casing; and

said inner wall comprises a blade platform spaced radially outwardly from said disk.

10. A flowpath according to claim 9 further comprising a conical spinner adjoining said platform at said blade leading edges, and said flute commences in said spinner and continues aft in said platform.

11. A flowpath according to claim 3 wherein:

said airfoils comprise compressor rotor blades extending radially outwardly from a supporting rotor drum;

said outer wall comprises an annular compressor casing; and

said inner wall comprises blade platforms integrally joined to respective ones of said blades radially outwardly from said drum.

12. A flowpath according to claim 3 wherein:

said airfoils comprise compressor stator vanes;

said outer wall comprises an annular outer band affixed to said vane outer ends; and

said inner wall comprises an annular inner band affixed to said vane inner ends.

13. A flowpath according to claim 3 wherein both said outer and inner bands include respective ones of said flutes therein.

14. A fan flowpath for diffusing air comprising:

a plurality of circumferentially spaced apart fan rotor blades extending radially outwardly from a supporting rotor disk, and each including axially spaced apart leading and trailing edges and radially spaced apart root and tip;

an annular fan casing spaced radially from said blade tips and circumferentially bridging said blades thereat;

a plurality of platforms spaced radially outwardly from said disk, and circumferentially bridging said blades at said roots thereof; and

each of said platforms include a circumferentially concave flute adjacent said leading edges for locally increasing flow area thereat.

15. A flowpath according to claim 14 wherein said flute commences axially forward of said leading edges, terminates axially forward of said trailing edges, and extends in width circumferentially between adjacent blades.

16. A flowpath according to claim 15 wherein said flute is substantially uniform in width from said commencement thereof to said leading edges and then is substantially uniform in width toward said termination thereof.

17. A compressor flowpath for diffusing air comprising:

a plurality of circumferentially spaced apart compressor rotor blades extending radially outwardly from a supporting rotor drum, and each including axially spaced apart leading and trailing edges and radially spaced apart root and tip;

a compressor casing spaced radially from said blade tips and circumferentially bridging said blades thereat;

a plurality of platforms spaced radially outwardly from said drum, and circumferentially bridging said blades at said roots thereof; and

each of said platforms includes a circumferentially concave flute adjacent said leading edges for locally increasing flow area thereat.

18. A flowpath according to claim 17 wherein said flute extends in width circumferentially between said leading edges, and terminates in length axially forward of said trailing edges.

19. A flowpath according to claim 17 wherein said flute converges in with from said leading edges to said trailing edges.

20. A compressor flowpath for diffusing air comprising:

a plurality of circumferentially spaced apart compressor stator vanes each including axially spaced apart leading and trailing edges and radially spaced apart outer and inner ends;

an annular outer band affixed to said vane outer ends; and

said outer band includes a circumferentially concave flute adjacent said leading edges for locally increasing flow area thereat.

21. A flowpath according to claim 20 wherein said flute extends in width circumferentially between said leading edges, and terminates in length axially forward of said trailing edges.

22. A flowpath according to claim 21 wherein said flute converges in width from said leading edges to said trailing edges.

23. A flowpath according to claim 22 further comprising an annular inner band affixed to said vane inner ends, and said inner band includes a flute between said vane leading edges for locally increasing flow area thereat.