Engine coupling arrangement

Patent metadata

Field	Value
Publication number	US-10570816-B2
Application number	US-201715708905-A
Country	US
Kind code	B2
Filing date	Sep 19, 2017
Priority date	Sep 19, 2017
Publication date	Feb 25, 2020
Grant date	Feb 25, 2020

Abstract

An engine assembly includes an intermittent internal combustion engine having an engine shaft, a turbine having a turbine shaft, an output shaft for driving a load, and a gearbox having a first portion and a second portion. The engine shaft is in engagement with an accessory via the first portion. The turbine shaft is in driving engagement with the output shaft via the second portion. The gearbox is configurable between an engaged and a disengaged configurations. In the disengaged configuration, the first and second portions are decoupled, and the engine shaft and the turbine shaft are rotatable independently from each other. In the engaged configuration, the first and second portions are coupled, and the engine shaft and the turbine shaft are drivingly engaged with each other via the coupled first and second portions.

First claim

The invention claimed is:

1. An engine assembly comprising:
an intermittent internal combustion engine having an engine shaft;
a turbine having a turbine shaft and having an inlet in fluid communication with an exhaust of the intermittent internal combustion engine;
a rotatable accessory;
an output shaft for driving engagement with a load to be driven by the engine assembly;
a gearbox having a first portion and a second portion, the engine shaft in driving engagement with the rotatable accessory via the first portion, the turbine shaft in driving engagement with the output shaft via the second portion, the gearbox configurable between an engaged configuration and a disengaged configuration, wherein:
in the disengaged configuration, the first and second portions are decoupled, and the engine shaft and the turbine shaft are rotatable independently from each other, the rotatable accessory remaining in driving engagement with the intermittent internal combustion engine via the first portion of the gearbox; and
in the engaged configuration, the first and second portions are coupled, and the engine shaft and the turbine shaft are drivingly engaged with each other via the coupled first and second portions.

2. The engine assembly of claim 1 , further comprising a compressor in driving engagement with the turbine shaft, the compressor fluidly connected to an inlet of the intermittent internal combustion engine.

3. The engine assembly of claim 1 , wherein the intermittent internal combustion engine is a rotary engine.

4. The engine assembly of claim 1 , wherein the accessory is selected from the group consisting of: oil pump, fuel pump, coolant pump, generator, and alternator.

5. The engine assembly of claim 1 , wherein the gearbox is configurable between the engaged and disengaged configurations via a clutch including a first component forming part of the first portion and a second component forming part of the second portion, the first and second components engaged with each other in the engaged configuration and disengaged from each other in the disengaged configuration.

6. The engine assembly of claim 1 , further comprising an actuator operable to selectively position the gearbox in each of the engaged and disengaged configurations.

7. The engine assembly of claim 6 , wherein a de-energized position of the actuator corresponds to the engaged configuration.

8. The engine assembly of claim 1 , further comprising a brake selectively engageable to a component of the second portion for limiting rotation of the output shaft in the disengaged configuration.

9. An engine assembly comprising:
an intermittent internal combustion engine having an engine shaft;
a turbine having a turbine shaft and having an inlet in fluid communication with an exhaust of the intermittent internal combustion engine;
a rotatable accessory;
an output shaft for driving engagement with a load to be driven by the engine assembly; and
a gearbox defining a first load path and a second load path, the engine shaft in driving engagement with the rotatable accessory via the first load path, the turbine shaft in driving engagement with the output shaft via the second load path, the gearbox including a clutch configurable between an engaged configuration where the clutch drivingly engages the first and second load paths with each other and a disengaged configuration where the clutch disengages the first and second load paths from each other, wherein:
the engine shaft and the turbine shaft are rotatable independently from each other so that the engine shaft is rotatable independently from the output shaft to drive the rotatable accessory when the clutch is in the disengaged configuration; and
the engine shaft and the turbine shaft are both in driving engagement with the output shaft via the gearbox when the clutch is in the engaged configuration.

10. The engine assembly of claim 9 , further comprising a compressor in driving engagement with the turbine shaft, the compressor fluidly connected to an inlet of the intermittent internal combustion engine.

11. The engine assembly of claim 9 , wherein the intermittent internal combustion engine is a rotary engine.

12. The engine assembly of claim 9 , wherein the accessory is selected from the group consisting of: oil pump, fuel pump, coolant pump, generator, and alternator.

13. The engine assembly of claim 9 , wherein the clutch has two components, one of the two components in driving engagement with the first load path, the other of the two components in driving engagement with the second load path, one of the two components having male members and the other of the two components having female members engaged with the male members in the engaged configuration.

14. The engine assembly of claim 9 , further comprising an actuator operatively connected to the clutch and operable to shift the clutch between the engaged and disengaged configurations.

15. The engine assembly of claim 14 , wherein a de-energized position of the actuator corresponds to the engaged configuration.

16. The engine assembly of claim 9 , further comprising a brake selectively engageable to a component of the second load path for limiting rotation of the output shaft in the disengaged configuration.

17. A method of operating an engine assembly having an output shaft for driving a rotatable load, the method comprising:
generating a first rotational input with an intermittent internal combustion engine and transmitting the first rotational input to a rotatable accessory via a gearbox selectively configurable between engaged and disengaged configurations;
generating a second rotational input with a turbine and transmitting the second rotational input to the output shaft via the gearbox; and
configuring the gearbox between the engaged and disengaged configurations, the intermittent internal combustion engine being in driving engagement with the output shaft via the gearbox in the engaged configuration and being rotatable independently from the output shaft to drive the rotatable accessory when the gearbox is in the disengaged configuration;
wherein with the gearbox in the disengaged configuration, the first and second rotational inputs are transmitted independently from each other, and with the gearbox in the engaged configuration, the first and second rotational inputs are combined in a combined rotational input transmitted to the output shaft via the gearbox.

18. The method of claim 17 , further comprising transmitting the second rotational input to a compressor fluidly connected to an inlet of the intermittent internal combustion engine.

19. The method of claim 17 , wherein combining the first and second rotational inputs comprises actuating a clutch to drivingly engage the first and second rotational inputs with each other.

20. The method of claim 17 , wherein configuring the gearbox comprises exerting a force on one component of the gearbox to configure the gearbox in the disengaged configuration.

Assignees

• Pratt & Whitney Canada

Inventors

• Thomassin Jean
• Villeneuve Bruno
• Fontaine Mike

Classifications

• F02B2053/005

  Wankel engines · CPC title

• F02B61/06

  Combinations of engines with mechanical gearing (F02B61/02, F02B61/04 take precedence) · CPC title

• B64D41/00

  Power installations for auxiliary purposes · CPC title

• F02B53/02

  Methods of operating · CPC title

• F02B39/04

  Mechanical drives; Variable-gear-ratio drives (non-mechanical pump drives having variable gear ratio F02B39/08) · CPC title