FAN ROTOR WITH CONSTRUCTION AND SAFETY PERFORMANCE OPTIMIZATION

• US 20020131865A1
• Filed: 03/13/2001
• Published: 09/19/2002
• Est. Priority Date: 03/13/2001
• Status: Active Grant

• Current Assignee: The U.S.A. As Represented By The Secretary Of Navy
• Original Assignee: The U.S.A. As Represented By The Secretary Of Navy
• Inventors: Tzortzinis, Nicholas L., Larzelere, John C., Huebner, Marh A., Sisson, Dale W. Jr., Van Doren, Thomas W., Atwell, Charles K., LaMoy, Craig S.
• Granted Patent: US 6,457,941 B1
• Time in Patent Office: Days
• US Class Current: 416/203
• CPC Class Codes: F04D 19/002 Axial flow fans
• CPC Class Codes: F04D 29/325 for axial flow fans blade mountings F04D29/34, blades F04D29/38
• CPC Class Codes: F04D 29/384 characterised by form
• CPC Class Codes: Y10S 416/50 Vibration damping features

Abstract

A one-piece fan rotor optimized for construction and safety performance criteria is provided. The rotor has a hub with a radial cross-section defined by an I-beam. A plurality of unequally-spaced rotor blades are disposed circumferentially around and extend radially outward from the hub. Each rotor blade has a root portion coupled to the hub with the root portion defined by a concave fillet circumventing the rotor blade. For rotational balance, at least one of the forward side and backside of the hub incorporates an axially extending pad. Methods are provided for controlling stress on the rotor and for balancing the rotor.

Claims

1. A fan rotor comprising:

a hub having a radial cross-section defined by an I-beam, said hub having a forward side receiving an airflow and a backside opposite said forward side;

a plurality of unequally-spaced rotor blades disposed circumferentially around and extending radially outward from said hub;

each rotor blade from said plurality of rotor blades having a root portion coupled to said hub, said root portion including a concave fillet circumventing said each rotor blade; and

at least one of said forward side and said backside of said hub incorporating an axially extending pad for rotational balance.

2. A fan rotor as in claim 1 wherein said hub, each of said plurality of rotor blades with said root portion, and said ring with said pad are made integrally from a cast aluminum alloy.

3. A fan rotor as in claim 2 wherein said cast aluminum alloy is selected from the group consisting of A356-T6, LM-6 and LM-31 aluminum alloys.

4. A fan rotor as in claim 1 wherein said hub, each of said plurality of rotor blades with said root portion, and said pad are made integrally from a machined billet of an aluminum alloy.

5. A fan rotor as in claim 4 wherein said aluminum alloy is a 6061-T6 aluminum alloy.

6. A fan rotor as in claim 1 wherein said concave fillet has a circular radius of curvature.

7. A method of reducing stress on a fan rotor, comprising the steps of:

providing a one-piece rotor having a hub with a radial cross-section defined by an I-beam having an inner annular flange and an outer annular flange coupled to one another by an annular disk, said hub having a forward side receiving an airflow and a backside opposite said forward side, said rotor further having a plurality of unequally-spaced rotor blades disposed circumferentially around and extending radially outward from said hub, each rotor blade from said plurality of rotor blades having a root portion coupled to said hub, said root portion including a concave fillet having a circular radius of curvature circumventing said each rotor blade, at least one of said forward side and said backside of said hub incorporating a pad extending axially from said annular disk;

selecting a target stress level;

rotating said rotor;

evaluating stress on said rotor during said step of rotating; and

adjusting said radius of curvature and a radial thickness of said outer annular flange based on said step of evaluating to achieve said target stress level.

8. A method according to claim 7 further comprising the step of constructing said rotor integrally from a cast aluminum alloy.

9. A method according to claim 8 further comprising the step of selecting said cast aluminum alloy from the group consisting of A356-T6, LM-6 and LM-31 aluminum alloys.

10. A method according to claim 7 further comprising the step of constructing said rotor integrally from a machined billet of an aluminum alloy.

11. A method according to claim 10 further comprising the step of selecting said aluminum alloy to be a 6061-T6 aluminum alloy.

13. A method according to claim 12 further comprising the step of constructing said rotor and said pad integrally from a cast aluminum alloy.

14. A method according to claim 13 further comprising the step of selecting said cast aluminum alloy from the group consisting of A356-T6, LM-6 and LM-31 aluminum alloys.

15. A method according to claim 12 further comprising the step of constructing said rotor and said pad integrally from a machined billet of an aluminum alloy.

16. A method according to claim 15 further comprising the step of selecting said aluminum alloy to be a 6061-T6 aluminum alloy.

17. A method according to claim 12 further comprising the steps of:

spinning said rotor;

evaluating balance of said rotor during said step of spinning; and

modifying said pad based on said step of evaluating until said rotor is balanced.

18. A method according to claim 17 wherein said step of modifying comprises the step of milling only exterior surfaces of said pad.

12. A method of balancing a fan rotor, comprising the steps of:

providing a one-piece rotor having a hub with a radial cross-section defined by an I-beam having an inner annular flange and an outer annular flange coupled to one another by an annular disk, said hub having a forward side receiving an airflow and a backside opposite said forward side, said rotor further having a plurality of unequally-spaced rotor blades disposed circumferentially around and extending radially outward from said hub;

integrating a pad with at least one of said forward side and said backside of said hub, said pad extending axially from said annular disk; and

sizing and positioning said pad to rotationally balance said rotor.