Unducted thrust producing system

Patent metadata

Field	Value
Publication number	US-10202865-B2
Application number	US-201314437872-A
Country	US
Kind code	B2
Filing date	Oct 23, 2013
Priority date	Oct 23, 2012
Publication date	Feb 12, 2019
Grant date	Feb 12, 2019

Abstract

An unducted thrust producing system has a rotating element with an axis of rotation and a stationary element. The rotating element includes a plurality of blades each having a blade root proximal to the axis, a blade tip remote from the axis, and a blade span measured between the blade root and the blade tip. The rotating element has a load distribution such that at any location between the blade root and 30% span the value of ΔRCu in the air stream is greater than or equal to 60% of the peak ΔRCu in the air stream.

First claim

What is claimed is:

1. An unducted thrust producing system for a design operating condition including flight speed, rotational speed, and thrust, comprising:
a stationary element; and
a rotating element comprising:
an axis of rotation;
and
a plurality of blades, each of said plurality of blades comprising:
a blade root proximal to said axis;
a blade tip remote from said axis; and
a blade span measured between said blade root and said blade tip,

wherein said rotating element at said design operating condition has a load distribution such that at any location between said blade root and 30% span the value of ΔRCu is greater than or equal to 70% of the peak ΔRCu.

2. The unducted thrust producing system of claim 1 , wherein said rotating element has a load distribution such that at any location between said blade root and 30% span the value of ΔRCu in the air stream is greater than or equal to 80% of the peak ΔRCu in the air stream.

3. The unducted thrust producing system of claim 1 , wherein said unducted thrust producing system is a propeller system.

4. The unducted thrust producing system of claim 1 , wherein said unducted thrust producing system is an open rotor system.

5. The unducted thrust producing system of claim 1 , wherein said stationary element comprises a plurality of vanes each comprising a vane root proximal to said axis, a vane tip remote from said axis, and a vane span measured between said vane root and said vane tip configured to impart a change in tangential velocity of the air opposite to that imparted by said rotating element.

6. The unducted thrust producing system of claim 5 , wherein said vanes are positioned upstream of said rotating element.

7. The unducted thrust producing system of claim 5 , wherein said vanes are positioned downstream of said rotating element.

8. The unducted thrust producing system of claim 5 , wherein said vanes are variable in pitch.

9. The unducted thrust producing system of claim 5 , wherein at least one of said vanes comprise a shroud distally from said axis.

10. The unducted thrust producing system of claim 5 , wherein the Cu in the air stream aft of said unducted thrust producing system is relatively low compared to ΔCu of said rotating element over the majority of the span of said vanes.

11. The unducted thrust producing system of claim 5 , wherein at least one of said vanes is attached to an aircraft structure.

12. The unducted thrust producing system of claim 5 , wherein said stationary element comprises more than two of said plurality of vanes.

13. The unducted thrust producing system of claim 12 , wherein said stationary element comprises more than four of said plurality of vanes.

14. The unducted thrust producing system of claim 1 , wherein said unducted thrust producing system is a tilt rotor system.

15. The unducted thrust producing system of claim 1 , wherein said unducted thrust producing system is a helicopter lift system.

16. The unducted thrust producing system of claim 1 , wherein said rotating element is driven via a torque producing device.

17. The unducted thrust producing system of claim 16 , wherein said torque producing device is selected from the group consisting of electric motors, gas turbines, gear drive systems, hydraulic motors, and combinations thereof.

18. The unducted thrust producing system of claim 1 , wherein said rotating element has a shaft power per unit annulus area greater than about 20 SHP/ft2 at cruise operating conditions.

19. The unducted thrust producing system of claim 1 , wherein said blades are variable in pitch.

20. An unducted torque producing system for extracting energy from an air stream for a design operating condition including air stream velocity, rotational speed, and energy extraction, said unducted torque producing system comprising:
a stationary element; and
a rotating element comprising:
an axis of rotation;
and
a plurality of blades, each of said plurality of blades comprising:
a blade root proximal to said axis;
a blade tip remote from said axis; and
a blade span measured between said blade root and said blade tip,

wherein said rotating element at said design operating condition has a load distribution such that at any location between said blade root and 30% span the value of ΔRCu is greater than or equal to 70% of the peak ΔRCu.

21. The unducted torque producing system of claim 20 , wherein said unducted torque producing system is a wind turbine.

22. The unducted torque producing system of claim 20 , wherein said stationary element comprises a plurality of vanes each comprising a vane root proximal to said axis, a vane tip remote from said axis, and a vane span measured between said vane root and said vane tip configured to impart a change in tangential velocity of the air opposite to that imparted by said rotating element.

23. The unducted torque producing system of claim 22 , wherein said vanes are positioned upstream of said rotating element.

24. The unducted torque producing system of claim 22 , wherein said vanes are positioned downstream of said rotating element.

Assignees

• Gen Electric

Inventors

• Breeze-Stringfellow Andrew
• Khalid Syed Arif
• Smith Jr Leroy Harrington

Classifications

• F05D2250/70

  Shape · CPC title

• F05D2240/301

  Cross-sectional characteristics · CPC title

• F05D2220/90

  in vehicles adapted for vertical or short take off and landing (v/stol vehicles) · CPC title

• F05B2260/96

  Preventing, counteracting or reducing vibration or noise · CPC title

• F01D9/02

  Nozzles; Nozzle boxes; Stator blades; Guide conduits {, e.g. individual nozzles (nozzle boxes F01D9/047)} · CPC title