Contra-rotating open fan propulsion system

Patent metadata

Field	Value
Publication number	US-9835093-B2
Application number	US-201314032163-A
Country	US
Kind code	B2
Filing date	Sep 19, 2013
Priority date	Sep 19, 2013
Publication date	Dec 5, 2017
Grant date	Dec 5, 2017

Abstract

In one aspect a propulsion system comprises an engine and a drive assembly coupled to the engine, comprising a first driveshaft rotatable in a first direction about a first axis, a first fan coupled to the first driveshaft to rotate in the first direction, and a clutch assembly to selectively disengage the first fan from the first driveshaft. Other aspects may be described.

First claim

What is claimed is:

1. A drive assembly comprising:
a first driveshaft rotatable in a first direction about a first axis;
a first fan coupled to the first driveshaft and configured to rotate in the first direction; and
a clutch assembly configured to selectively disengage the first fan from the first driveshaft and configured to adjust a resistance with respect to rotation of the first fan in the first direction while the first fan is disengaged.

2. The drive assembly of claim 1 , wherein the clutch assembly comprises a hydraulic clutch and a braking system.

3. The drive assembly of claim 2 , further comprising a gearbox coupled to the first driveshaft between an engine and the first fan, wherein the gearbox is configured to drive the first fan in a second direction, opposite the first direction.

4. The drive assembly of claim 2 , further comprising:
a second driveshaft rotatable in a second direction, different from the first direction; and
a second fan coupled to the second driveshaft, wherein the first driveshaft and the second driveshaft are coaxial.

5. The drive assembly of claim 4 , wherein the first fan and the second fan are displaced by a distance that measures between 0.02 and 0.35 the distance of an overall front row fan diameter.

6. A propulsion system comprising:
an engine; and
a drive assembly coupled to the engine, the drive assembly comprising:
a first driveshaft rotatable in a first direction about a first axis;
a first fan coupled to the first driveshaft and configured to rotate in the first direction; and
a clutch assembly configured to selectively disengage the first fan from the first driveshaft and configured to adjust a resistance with respect to rotation of the first fan in the first direction while the first fan is disengaged.

7. The propulsion system of claim 6 , wherein the clutch assembly comprises a fluid coupling clutch, wherein the clutch assembly includes a multi-directional hydraulic control circuit configured to adjust the resistance, and wherein the multi-directional hydraulic control circuit comprises a multi-position valve, a multi-loop hydraulic circuit, or a combination thereof.

8. The propulsion system of claim 7 , further comprising a gearbox coupled to the first driveshaft between an engine and the first fan.

9. The propulsion system of claim 6 , further comprising:
a second driveshaft rotatable in a second direction, different from the first direction; and
a second fan coupled to the second driveshaft.

10. An aircraft comprising:
a fuselage;
an engine coupled to the fuselage; and
a drive assembly coupled to the engine, the drive assembly comprising:
a first driveshaft rotatable in a first direction about a first axis;
a first fan coupled to the first driveshaft and configured to rotate in the first direction; and
a clutch assembly configured to selectively disengage the first fan from the first driveshaft and configured to adjust a resistance with respect to rotation of the first fan in the first direction while the first fan is disengaged.

11. The aircraft of claim 10 , wherein the clutch assembly comprises a fluid coupling clutch and a braking system.

12. The aircraft of claim 11 , further comprising a gearbox coupled to the first driveshaft between an engine and the first fan, wherein the gearbox is configured to drive the first fan in a second direction, opposite the first direction.

13. The aircraft of claim 10 , further comprising:
a second driveshaft rotatable in a second direction, different from the first direction; and
a second fan coupled to the second driveshaft.

14. The drive assembly of claim 1 , wherein the clutch assembly comprises:
an impeller coupled to the first driveshaft; and
a turbine fluidly coupled to the impeller and coupled to the first fan.

15. The drive assembly of claim 14 , further comprising one or more valves of a clutch control circuit configured to reduce or stop hydraulic fluid from flowing from the impeller to the turbine, wherein reducing or stopping the hydraulic fluid from flowing from the impeller to the turbine disengages the first fan from the first driveshaft.

16. The drive assembly of claim 14 , further comprising a clutch control circuit configured to selectively control pressure and direction of hydraulic fluid flowing into the turbine, wherein the clutch control circuit includes a multi-directional hydraulic control circuit configured to adjust the resistance.

17. The drive assembly of claim 14 , wherein the clutch assembly is configured such that hydraulic fluid flows from the impeller into the turbine in the first direction to rotate the first fan, and further comprising a clutch control circuit configured to selectively direct the hydraulic fluid into the turbine in a second direction to increase viscous resistance within the turbine, wherein increasing the viscous resistance within the turbine resists the rotation of the first fan.

18. The propulsion system of claim 7 , further comprising a clutch control circuit that includes the multi-directional hydraulic control circuit, wherein the clutch control circuit is configured to selectively increase hydraulic pressure in the clutch assembly to control power output by the clutch assembly.

19. The propulsion system of claim 18 , wherein the clutch control circuit further includes:
an accumulator configured to store hydraulic fluid under pressure and to provide pressurized hydraulic fluid to a turbine of the clutch assembly; and
one or more valves in fluid connection with the accumulator.

20. The propulsion system of claim 7 , wherein the multi-directional hydraulic control circuit comprises the multi-position valve having at least two positions including a first position and a second position, the first position configured to direct hydraulic fluid from an impeller of the clutch assembly into a turbine of the clutch assembly in the first direction, and the second position configured to direct the hydraulic fluid from the impeller into the turbine in a second direction.

Assignees

• Boeing Co

Inventors

• Golshany Sina S
• Huntly David Miles
• Blom Adriana W
• Erickson Todd W
• Tretow Paul R

Classifications

• F02C6/206

  the vehicles being airscrew driven · CPC title

• F02C3/067

  having counter-rotating rotors (F02C3/073 takes precedence) · CPC title

• B64C27/12

  Rotor drives · CPC title

• F02C3/36

  Open cycles · CPC title

• F02C7/36 Primary

  Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user ({F02C3/107 - F02C3/13 and} F02C7/32 take precedence; couplings for transmitting rotation F16D; gearing in general F16H) · CPC title