Propeller rotor and engine overspeed control

Patent metadata

Field	Value
Publication number	US-9458844-B2
Application number	US-201313924050-A
Country	US
Kind code	B2
Filing date	Jun 21, 2013
Priority date	Jun 21, 2013
Publication date	Oct 4, 2016
Grant date	Oct 4, 2016

Abstract

An electromagnetic device for overspeed control of a propeller driven by an engine shaft comprises a clutch, an eddy-current coupler, and an electromagnetic brake. The clutch is disposed to mechanically decouple the propeller from the engine shaft. The eddy current coupler is disposed to electromagnetically couple the propeller to the engine shaft when the clutch mechanically decouples the propeller from the engine shaft. The electronic brake is disposed to artificially load the engine shaft when the propeller load on the engine shaft is reduced by mechanically decoupling the propeller from the engine shaft.

First claim

The invention claimed is:

1. An electromagnetic device for overspeed control of a propeller driven by an engine shaft, the electromagnetic device comprising:
an electromechanical clutch disposed to mechanically decouple the propeller from the engine shaft;
an eddy-current coupler disposed to electromagnetically couple the propeller to the engine shaft when the clutch mechanically decouples the propeller from the engine shaft; and
an electromagnetic brake disposed to impose an artificial load on the engine shaft when a propeller load on the engine shaft is reduced by mechanically decoupling the propeller from the engine shaft;
wherein the electromechanical clutch and the eddy-current coupler are integrated in a rotating electromagnetic assembly comprising:
a field coil configured to receive a first energizing current;
a pole shoe energized by the first energizing current to electromagnetically decouple a ferromagnetic friction clutch cone attached to the engine shaft from a friction clutch cup attached to the propeller; and
a rotating drum attached to the friction clutch cup and coupled via eddy currents to the pole shoe with a coupling strength determined by a magnitude of the first energizing current.

2. The electromagnetic device of claim 1 , wherein the first energizing current is set based on a speed of the propeller compared to a speed reference.

3. The electromagnetic device of claim 1 , wherein the electromagnetic brake is driven by a second energizing current, such that the artificial load is determined by a magnitude of the second energizing current.

4. The electromagnetic device of claim 3 , wherein the second energizing current is set based on a speed of the engine shaft.

5. The electromagnetic device of claim 3 , further comprising a double-channel synchronous exciter with a first channel providing the first energizing current, and a second channel providing the second energizing current.

6. A method of controlling speed of a propeller on an engine shaft, the method comprising:
disengaging a mechanical coupling between the propeller and the engine shaft with an electromagnetic clutch in response to a potential overspeed event, by energizing a pole shoe attached to the engine shaft with a first energizing current to separate a friction clutch cone attached to the engine shaft from a friction clutch cup attached to the propeller;
engaging an electromagnetic coupling between the propeller and the engine shaft with an eddy current coupler when the propeller is mechanically decoupled from the engine shaft; and
imposing an artificial load on the engine shaft with an electromagnetic brake when the propeller is mechanically decoupled from the engine shaft.

7. The method of claim 6 , wherein engaging an electromagnetic coupling between the propeller and the engine shaft comprises inducing eddy currents in a rotating drum attached to the friction clutch cup via the energized pole shoe.

8. The method of claim 6 , wherein slip of the electromagnetic coupling is determined by the first energizing current, and is greater than slip of the mechanical coupling.

9. The method of claim 8 , wherein strength of the artificial load is determined by a second energizing current.

10. The method of claim 9 , wherein the first energizing current is set based on a speed of the propeller compared with a first speed reference, and the second energizing current is set based on speed of the engine shaft.

11. The method of claim 9 , wherein the first energizing current is provided by a first channel of a double-channel synchronous exciter, and the second energizing current is provided by a second channel of the double-channel synchronous exciter.

12. A propeller system comprising:
a propeller on a propeller shaft;
an engine disposed to drive the propeller shaft via an engine shaft;
a clutch disposed to mechanically decouple the propeller shaft from the engine shaft;
an eddy-current coupler disposed to electromagnetically couple the propeller shaft to the engine shaft when the clutch mechanically decouples the propeller from the engine shaft; and
an electromagnetic brake disposed to impose an artificial load on the engine shaft when propeller load on the engine shaft is reduced by mechanically decoupling the propeller from the engine shaft;
wherein the clutch and the eddy-current coupler are integrated in a rotating electromagnetic assembly comprising:
a field coil configured to receive a first energizing current;
a pole shoe energized by the first energizing current to electromagnetically decouple a ferromagnetic friction clutch cone attached to the engine shaft from a friction clutch cup attached to the propeller; and
a rotating drum attached to the friction clutch cup and coupled via eddy currents to the pole shoe with a coupling strength determined by a magnitude of the first energizing current.

13. The propeller system of claim 12 , wherein the propeller is a propulsion propeller of a turboprop vehicle.

14. The propeller system of claim 12 , wherein the propeller has pitchable blades.

15. The propeller system of claim 12 , wherein the energizing current is set based on a speed of the propeller compared to a speed reference.

16. The propeller system of claim 12 , wherein the electromagnetic brake is driven by a second energizing current set based on a speed of the engine shaft, such that the artificial load is determined by a strength of the second energizing current.

17. The propeller system of claim 12 , wherein a gap spacer is disposed between the pole shoe and the clutch to preserve a gap between the pole shoe and the friction clutch cup when the pole shoe is energized.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Gieras Jacek F
• Ribarov Lubomir A

Classifications

• F04B35/04 Primary

  the means being electric · CPC title

• B60T13/748

  acting on electro-magnetic brakes (combined with fluid-pressure brake systems B60T13/667) · CPC title

• B64D35/00 Primary

  Transmitting power from power plants to propellers or rotors; Arrangements of transmissions · CPC title

• F16D63/002

  Brakes with direct electrical or electro-magnetic actuation · CPC title

• H02K49/043

  with a radial airgap · CPC title