IP Library Granted Patent US 7,604,202
Granted Patent B2
US 7,604,202 · App. 11/662,859 · Granted Oct 20, 2009

Ice management system for tiltrotor aircraft

Assignee: Bell Helicopter Textron Inc.
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Quick Facts
Patent No.
US 7,604,202
App. No.
11/662,859
Granted
Oct 20, 2009
Kind
B2
Abstract

An ice management system is configured for an aircraft having at least one rotor, each rotor having a plurality of blades. The system has an electrical power supply adapted to be carried by the aircraft remote from the rotor, and at least one heater is carried by the rotor for heating at least a portion of the rotor. A solid-state control relay is carried by the rotor and conductively coupled between the power supply and each heater for selectively controlling the flow of electrical power from the power supply to each heater. In addition, the system may incorporate a solid-state feed relay carried by the aircraft remote from the rotor and conductively coupled between the power supply and the control relay for selectively controlling the flow of electrical power to the control relay.

Claims (31)

1. An ice management system for an aircraft having at least one rotor, each rotor having a plurality of blades, the system comprising:

an electrical power supply adapted to be carried by the aircraft remote from the rotor;

at least one heater carried by the rotor for heating at least a portion of the rotor;

a plurality of solid-state control relays, the plurality of solid-state control relays including a first solid-state control relay carried by the rotor and conductively coupled between the power supply and the at least one heater for selectively controlling a flow of electrical power from the power supply to the at least one heater,

wherein the plurality of solid-state control relays includes a second control relay in series with the first control relay; and

a solid-state feed relay adapted to be carried by the aircraft remote from the rotor, the feed relay being conductively coupled between the power supply and the at least one heater,

wherein the solid-state feed relay is connected in series with the first and second control relays and configured for selectively controlling a flow of electrical power to the control relays, and

wherein the at least one heater is connected in series between the solid-state feed relay and one of the first and second control relays.

2. The ice management system according to claim 1 , wherein the at least one heater comprises at least one heater located on each blade.

3. The ice management system according to claim 1 , wherein the flow of electrical power is conducted to at least one of the plurality of control relays through a slip ring carried on the rotor.

4. An ice management system for an aircraft having at least one rotor, each rotor having a plurality of blades, the system comprising:

an electrical power supply adapted to be carried by the aircraft, the power supply being carried remote from each rotor and being conductively connected provide a plurality of phases of electrical power;

a plurality of heaters located on each blade, each heater for heating at least a respective portion of the corresponding blade; and

a plurality of solid-state control relays, each solid-state control relay being operably associated with a respective heater, each control relay being carried in the rotor and conductively connected to receive a respective phase of electrical power from the electrical power supply between the electrical power supply and the corresponding heater and for selectively controlling a flow of current therebetween; and

a solid-state feed relay located remote from the rotor, the feed relay being conductively connected between the power supply and at least one of the solid-state control relays for selectively controlling a flow of current therebetween.

5. The ice management system according to claim 4 , wherein the flow of electrical power is conducted through a slip ring carried on the rotor.

6. The ice management system according to claim 1 , comprising:

a plurality of heaters, including the at least one heater, carried by the rotor for heating respective portions of the rotor,

wherein each control relay is carried by the rotor and conductively coupled between the power supply and a respective heater for selectively controlling the flow of electrical power from the power supply to the respective heater; and

a controller configured for controlling the control relays and the feed relay such that electrical power is independently controlled to each heater.

7. The ice management system according to claim 6 , further comprising:

a current sensor for sensing an amount of electrical current in a current path that is controlled by the feed relay and at least one of the control relays,

wherein the controller is further configured for determining whether to disable the ice management system based on the amount of electrical current sensed by the sensor.

8. The ice management system according to claim 1 , wherein the plurality of solid-state control relays includes a third control relay in series with the first and second control relays.

9. The ice management system according to claim 8 , wherein the first control relay is operable for controlling electrical current between the second and third control relays, the second control relay is operable for controlling electrical current between the first and third control relays, and the third control relay is operable for controlling electrical current between the first and second control relays.

10. The ice management system according to claim 4 , further comprising a controller configured for controlling the control relays and the feed relay such that electrical power is independently controlled to each heater.

11. The ice management system according to claim 10 , further comprising:

a current sensor for sensing an amount of electrical current in a current path that is controlled by the feed relay and at least one of the control relays,

wherein the controller is further configured for determining whether to disable the ice management system based on the amount of electrical current sensed by the sensor.

12. The ice management system according to claim 4 , wherein the plurality of control relays includes at least two control relays connected in series.

13. The ice management system according to claim 4 , wherein the plurality of control relays includes first, second, and third control relays, wherein the first control relay is operable for controlling electrical current between the second and third control relays, the second control relay is operable for controlling electrical current between the first and third control relays, and the third control relay is operable for controlling electrical current between the first and second control relays.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 30, 2009
From: BELL HELICOPTER TEXTRON INC.
To: TEXTRON INNOVATIONS INC.
Reel/Frame 022182/0461 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 28, 2007
From: FROMAN, GARY S.; TIPPETT, DANIEL R.
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 019075/0450 →
Continuity (1)
Related Publication 20070257153A1 · Nov 8, 2007