Conforming platform guide vane

• US 6,371,725 B1
• Filed: 06/30/2000
• Issued: 04/16/2002
• Est. Priority Date: 06/30/2000
• Status: Expired due to Term

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Noon, John Lawrence, Manteiga, John Alan, Nussbaum, Jeffrey Howard, Capozzi, Joseph
• Primary Examiner(s): Look, Edward K.
• Assistant Examiner(s): EDGAR, RICHARD A
• Application Number:
  US09/607,753
• Time in Patent Office: 655 Days
• Field of Search: 415/191, 415/189, 415/209.2, 415/209.3, 415/209.4, 415/210.1
• US Class Current: 415/209.4
• CPC Class Codes: F01D 5/14 Form or construction selecting particular materials, measures against erosion or corrosion F01D5/28
• CPC Class Codes: F01D 9/042 fixing blades to stators fixing stator-rings in the casing or to each other F01D25/246
• CPC Class Codes: F02K 3/06 with front fan
• CPC Class Codes: F05B 2260/301 Retaining bolts or nuts
• CPC Class Codes: F05D 2220/327 to drive shrouded, high solidity propeller
• CPC Class Codes: F05D 2230/60 Assembly methods
• CPC Class Codes: F05D 2240/80 Platforms for stationary or moving blades
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A fan outlet guide vane includes integral outer and inner platforms conforming to arcuate sides thereof, and multiple mounting bosses on the platforms. The platform sides are arcuate to conform with the vane sides for improving aerodynamic efficiency. The multiple mounting bosses improve mounting of the vanes to corresponding supporting rings.

Claims

1. A fan outlet guide vane comprising:

an airfoil having outer and inner platforms fixedly attached at opposite span ends thereof in a unitary assembly; and

each of said platforms having arcuate sides conforming with corresponding opposite sides of said airfoil, and respective outer and inner bosses extending from outboard surfaces thereof for receiving corresponding mounting bolts, with opposite inboard flow surfaces thereof defining flowpath boundaries.

2. A vane according to claim 1 wherein said airfoil includes:

a concave first side, and said outer and inner platforms have corresponding concave first sides; and

a convex second side, and said outer and inner platforms have corresponding convex second sides.

3. A vane according to claim 2 wherein said airfoil further includes opposite leading and trailing edges extending between corresponding leading and trailing ends of said outer and inner platforms, and said first sides of said outer and inner platforms are complementary with corresponding second sides of said outer and inner platforms between said leading and trailing edges.

4. A vane according to claim 3 wherein said inner platform is narrower than said outer platform, and said inner bosses are collectively narrower than said outer bosses.

5. A vane according to claim 4 wherein:

said inner platform includes a pair of forward and aft inner bosses coaxially aligned with said airfoil between said leading and trailing edges; and

said outer platform includes a forward outer boss and a plurality of laterally aligned aft outer bosses, coaxially aligned in part with said airfoil between said leading and trailing edges.

6. A vane according to claim 5 wherein said aft outer bosses include a center boss coaxially aligned with said airfoil, and a pair of outboard bosses disposed on opposite sides of said center boss.

7. A vane according to claim 6 in combination with a plurality of said vanes circumferentially adjoining each other, with adjacent ones of said outer and inner platforms being nested together along said arcuate sides thereof.

8. A fan outlet guide vane frame comprising:

a row of circumferentially adjoining outlet guide vanes extending radially between outer and inner rings;

each of said vanes including an airfoil with outer and inner platforms fixedly attached at opposite span ends thereof in a unitary assembly; and

each of said platforms having arcuate sides conforming with corresponding opposite sides of said airfoil, and respective outer and inner bosses extending from outboard surfaces thereof receiving corresponding mounting bolts, with opposite inboard flow surfaces thereof defining flowpath boundaries.

9. A frame according to claim 8 wherein each of said airfoils further includes opposite leading and trailing edges extending between corresponding leading and trailing ends of said outer and inner platforms, and said arcuate sides of said outer and inner platforms on one of said vanes are complementary with corresponding arcuate sides of said outer and inner platforms on a circumferentially adjoining vane between said leading and trailing edges.

10. A frame according to claim 9 wherein each of said airfoils includes:

a concave first side, and said outer and inner platforms have corresponding concave first sides; and

a convex second side, and said outer and inner platforms have corresponding convex second sides.

11. A method of assembling said fan outlet guide vane frame according to claim 10, comprising:

individually installing each of said vanes to said outer ring, and engaging said mounting bolts with said outer bosses through said outer ring; and

installing said inner ring inside said inner platforms, and engaging said mounting bolts with said inner bosses through said inner ring.

12. A method according to claim 11 further comprising circumferentially adjoining said vanes together, with adjacent ones of said platforms being nested together along said arcuate sides thereof.

13. A frame according to claim 10 wherein said inner platforms are circumferentially narrower than said outer platforms in each of said vanes, and said inner bosses are collectively circumferentially narrower than said outer bosses.

14. A frame according to claim 10 wherein:

said inner platforms each includes a pair of forward and aft inner bosses coaxially aligned with said airfoil between said leading and trailing edges; and

said outer platforms each includes include a forward outer boss and a plurality of laterally aligned aft outer bosses, coaxially aligned in part with said airfoil between said leading and trailing edges.

15. A frame according to claim 14 wherein said aft outer bosses include a center boss coaxially aligned with said airfoil, and a pair of outboard bosses disposed on opposite sides of said center boss.

16. A frame according to claim 15 wherein one of said vanes includes a mounting bolt in said center boss and not in said outboard bosses, and another one of said vanes includes mounting bolts in both said outboard bosses and not in said center boss.

17. A frame according to claim 15 wherein said outer ring includes locally thin and thick sections, and said outer bosses are bolted to said thin section, and said center boss is bolted to said thick section.

18. A frame according to claim 17 wherein said center bosses are not bolted to said thin section, and said outer bosses are not bolted to said thick section.

19. A fan outlet guide vane having integral outer and inner platforms being unitary therewith and conforming to arcuate sides thereof, and said platforms having different multiples of mounting bosses thereon.

20. A vane according to claim 19 wherein:

said platforms have concave first sides and convex opposite second sides;

said inner platform includes a pair of mounting bosses coaxially aligned with said vane between said leading and trailing edges thereof; and

said outer platform includes a forward mounting boss coaxially aligned with said vane at said leading edge, and three laterally aligned aft bosses.