Pitch range for a variable pitch fan

Patent metadata

Field	Value
Publication number	US-10288083-B2
Application number	US-201514941799-A
Country	US
Kind code	B2
Filing date	Nov 16, 2015
Priority date	Nov 16, 2015
Publication date	May 14, 2019
Grant date	May 14, 2019

Abstract

A variable pitch fan for a propulsion device is provided. The variable pitch fan includes a plurality of fan blades coupled to a disk and a rotatable front hub covering the disk. Each fan blade is rotatable about a pitch axis to vary a pitch of the fan blade. The pitch is variable within a pitch range that is at least about 80° to about 130°. Each fan blade extends radially outward from the disk along a span from a root to a tip. A portion of the span adjacent the root defines a root span region, a portion of the span adjacent the tip defines a tip span region. A solidity of the variable pitch fan is at least 1.0 in the root span region.

First claim

What is claimed is:

1. A variable pitch fan for a propulsion device, the variable pitch fan comprising:
a plurality of fan blades coupled to a disk, each fan blade of the plurality of fan blades extending radially outward from the disk, each fan blade extending along a span from a root to a tip, a portion of the span adjacent the root defining a root span region, a portion of the span adjacent the tip defining a tip span region, each fan blade rotatable about a pitch axis to vary a pitch of the fan blade; and
a pitch change actuation assembly for varying the pitch of the plurality of fan blades, the actuation assembly comprising:
a scheduling ring rotatable relative to the disk and defining a plurality of slots,
a plurality of linkage arms, and
a plurality of sliding members,

wherein each linkage arm is coupled to one fan blade of the plurality of fan blades, each sliding member is rotatably connected to one linkage arm of the plurality of linkage arms, and each sliding member is slidably coupled to one slot of the plurality of slots to operatively couple the fan blades to the slots,
wherein the plurality of slots includes at least one linear slot and at least one non-linear slot,
wherein each of the plurality of fan blades rotates according to a blade pitch schedule defined by the slot to which it is operatively coupled,
wherein at least two of the plurality of slots define different blade pitch schedules,
wherein the pitch axis of each of the plurality of fan blades extends radially through the fan blade, the pitch variable within a pitch range, the pitch range being at least 80°,
wherein a solidity of the variable pitch fan is at least 1.0 in the root span region of each blade, and
wherein the solidity of the variable pitch fan is less than 1.0 in the tip span region of each blade.

2. The variable pitch fan of claim 1 , further comprising a rotatable front hub covering the disk, wherein a fan hub radius ratio of the variable pitch fan is less than about 0.40.

3. The variable pitch fan of claim 1 , wherein the plurality of fan blades comprises at least ten fan blades.

4. The variable pitch fan of claim 1 , wherein the pitch range of each of the plurality of fan blades corresponds to the variation in pitch between a feather pitch position and a reverse pitch position.

5. The variable pitch fan of claim 1 , wherein the pitch range of each of the plurality of fan blades corresponds to the variation in pitch between a flat pitch position and a reverse pitch position.

6. The variable pitch fan of claim 1 , wherein the pitch range of each of the plurality of fan blades is about 120°.

7. The variable pitch fan of claim 1 , further comprising a plurality of trunnion mechanisms for coupling each of the plurality of fan blades to the disk, each trunnion mechanism including a bearing having one or more components comprised of a nonferrous material.

8. The variable pitch fan of claim 1 , wherein the propulsion device is a gas turbine engine.

9. A variable pitch fan for a propulsion device, the variable pitch fan comprising:
a plurality of fan blades coupled to a disk, each fan blade of the plurality of fan blades extending radially outward from the disk, each fan blade extending along a span from a root to a tip, a portion of the span adjacent the root defining a root span region, a portion of the span adjacent the tip defining a tip span region, each fan blade rotatable about a pitch axis to vary a pitch of the fan blade;
a pitch change actuation assembly for varying the pitch of the plurality of fan blades, the actuation assembly comprising:
a scheduling ring rotatable relative to the disk and defining a plurality of slots,
a plurality of linkage arms,
a plurality of sliding members, and
an electric motor; and

a rotatable front hub covering the disk,
wherein each linkage arm is coupled to one fan blade of the plurality of fan blades, each sliding member is rotatably connected to one linkage arm of the plurality of linkage arms, and each sliding member is slidably coupled to one slot of the plurality of slots to operatively couple the fan blades to the slots, wherein the plurality of slots includes at least one linear slot and at least one non-linear slot,
wherein the electric motor is operatively coupled to the scheduling ring to rotate the scheduling ring relative to the disk,
wherein each of the plurality of fan blades rotates according to a blade pitch schedule defined by the slot to which it is operatively coupled,
wherein at least two of the plurality of slots define different blade pitch schedules,
wherein a solidity of the variable pitch fan is at least 1.0 in the root span region of each blade,
wherein the solidity of the variable pitch fan is less than 1.0 in the tip span region of each blade,
wherein a fan hub radius ratio of the variable pitch fan is less than about 0.40, and
wherein the pitch axis of each of the plurality of fan blades extends radially through the fan blade, the pitch variable within a pitch range, the pitch range being at least 80°.

10. The variable pitch fan of claim 9 , wherein the plurality of fan blades comprises at least ten fan blades.

11. The variable pitch fan of claim 9 , wherein the propulsion device is a gas turbine engine.

12. The variable pitch fan of claim 9 , further comprising a plurality of trunnion mechanisms for coupling each of the plurality of fan blades to the disk, each trunnion mechanism including a bearing having one or more components comprised of a non-ferrous material.

13. The variable pitch fan of claim 9 , wherein the pitch range of each of the plurality of fan blades is about 120°.

14. The variable pitch fan of claim 9 , wherein the pitch range of each of the plurality of fan blades corresponds to the variation in pitch between a feather pitch position and a reverse pitch position.

15. The variable pitch fan of claim 9 , wherein the pitch range of each of the plurality of fan blades corresponds to the variation in pitch between a flat pitch position and a reverse pitch position.

16. The variable pitch fan of claim 1 , wherein the pitch change actuation assembly further comprises an electric motor, and wherein the electric motor is operatively coupled to the scheduling ring to rotate the scheduling ring relative to the disk.

17. The variable pitch fan of claim 1 , wherein the different blade pitch schedules include a first blade pitch schedule and a second blade pitch schedule, wherein the first blade pitch schedule is configured to increase a rotational speed of a first set of fan blades when the pitch of the plurality of fan blades reaches a pitch position within a first pitch range, and wherein the second blade pitch schedule is configured to decrease a rotational speed of a second set of fan blades when the pitch of the plurality of fan blades reaches the pitch position within the first pitch range.

18. The variable pitch fan of claim 1 , wherein the at least one non-linear slot includes a linear portion and a bent portion.

19. The variable pitch fan of claim 9 , wherein the at least one non-linear slot includes a linear portion and a bent portion.

Assignees

• Gen Electric

Inventors

• Miller Brandon Wayne
• Breeze-Stringfellow Andrew
• Zatorski Darek Tomasz
• Khalid Syed Arif
• Kroger Christopher James
• Niergarth Daniel Alan

Classifications

• F04D29/36 Primary

  adjustable {(flexible blades F04D29/382)} · CPC title

• F05D2220/36

  specially adapted for the fan of turbofan engines · CPC title

• F04D29/522

  especially adapted for elastic fluid pumps · CPC title

• F04D29/323

  adjustable · CPC title

• F01D7/00 Primary

  Rotors with blades adjustable in operation; Control thereof (for reversing F01D1/30) · CPC title