Hollow core airfoil

• US 5,253,824 A
• Filed: 09/01/1992
• Issued: 10/19/1993
• Est. Priority Date: 04/16/1991
• Status: Expired due to Term

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Hansen, Kurt L., Halila, Herbert
• Primary Examiner(s): Huppert, Michael S.
• Assistant Examiner(s): Ansley, Virna Lissi
• Application Number:
  US07/939,531
• Time in Patent Office: 413 Days
• Field of Search: 244/123, 244/35 R, 416/232, 416/233, 416/229 A, 416/241 A, 416/241 B
• US Class Current: 244/123.14
• CPC Class Codes: F01D 5/147 Construction, i.e. structural features, e.g. of weight-saving hollow blades F01D5/148, F01D5/16 and F01D5/20 take precedence; blade shape F01D5/141; blades with cooling or heating channels or cavities F01D5/18; heating, heat-insulating or cooling means on blades F01D5/18

Abstract

A hollow core airfoil including a root adapted to attach the airfoil to a disk. An airfoil portion including a leading edge, a trailing edge, and a tip portion. The hollow core airfoil includes radial ribs extending from the root to the tip. Chord-wise stringers run from the leading edge to the trailing edge providing support along the chord-wise direction.

Claims

1. A hollow core airfoil comprising:

first and second halves diffusion bonded together;

a substantially hollow central portion between said first and second halves;

a root portion, a tip portion, a leading edge and a trailing edge;

a plurality of radial ribs extending from said root portion to said tip portion within said hollow portion wherein said radial ribs comprise ridges of said first and second half diffusion bonded to form continuous ribs; and

a plurality of chord-wise stringers within said hollow portion wherein said stringers are arranged such that said stringers on said first half are not bonded to said stringers on said second half and a portion of said chord-wise stringers extend from said leading edge to said trailing edge wherein said chord-wise stringers are arranged in a foot print pattern starting at said leading edge and having a length proportional to a predetermined load concentration at said leading edge.

2. A hollow core airfoil according to claim 1 wherein said predetermined load concentration corresponds to a probability of foreign object damage in said airfoil.

3. A hollow core airfoil comprising;

an outer skin surrounding said hollow core;

a root, a tip, a leading edge and a trailing edge;

a plurality of radial ribs in said hollow core; and

a plurality of chord-wise stringers arranged substantially perpendicular to said radial ribs in said hollow core wherein said stringers comprise raised portions of said outer skin which are not bonded within said hollow core and wherein said chord-wise stringers increase in frequency from said root to said tip.