Rotary apparatus

• US 6,181,235 B1
• Filed: 05/28/1997
• Issued: 01/30/2001
• Est. Priority Date: 09/02/1994
• Status: Expired due to Term

• Current Assignee: Ultra Electronics Limited (Ultra Electronics Holdings PLC)
• Original Assignee: Ultra Electronics Limited (Ultra Electronics Holdings PLC)
• Inventors: Smith, James Andrew Timothy
• Primary Examiner(s): Crosland, Donnie L.
• Application Number:
  US08/793,694
• Time in Patent Office: 1,343 Days
• Field of Search: 340/310.01, 340/870.3, 340/870.33, 340/870.39, 340/640, 340/595, 340/679, 340/671, 340/672, 340/686.3, 340/825.25, 340/114, 341/192, 219/201, 219/202, 219/240, 219/250, 219/244, 219/482, 219/483, 219/486, 219/493, 244/134.A, 244/134.R, 416/245.R, 416/245.A, 416/155, 416/95, 310/114, 310/115, 310/67.R
• US Class Current: 318/696
• CPC Class Codes: B64D 15/12 by electric heating electric heating elements in general H05B
• CPC Class Codes: G08C 17/04 using magnetically coupled devices

Abstract

A rotary apparatus in which at least one electrically controlled device is attached to a rotor. The rotor carries coils such that rotation of the rotor generates power for the device. A switch is provided for controlling the supply of power to the device and receives control signals via a contactless communication link.

Claims

1. A rotary apparatus incorporating at least one electrically powered device on a propeller, the apparatus comprising an electrical generator having inductive windings carried for rotation with the propeller, switching means on the propeller responsive to a control signal to supply the at least one electrically powered device, and fixed permanent magnets, in which the inductive windings co-operate with the fixed permanent magnets to generate an induced voltage when the propeller rotates relative to the fixed magnet, the control signal is supplied to the switching means via a contactless inductive communication link between the propeller and a structure on which the rotor is rotatably mounted, the inductive windings comprise part of the communication link and a control winding is provided on the magnets and in use the control winding is modulated with a control signal to transmit data over the communication link.

2. An apparatus as claimed in claim 1, characterized by a controller for controlling the supply of power to the at least one electrically powered device, the controller having a connection to the control winding for transmitting control signals by modulating the control signal in the control winding.

3. An apparatus as claimed in claim 1, characterized in that the control signal is an encoded binary signal and the switching means includes decoding means to decode the control signal.

4. An apparatus as claimed in claim 1, characterised in that a contactless communication link is used to transmit performance information from the rotor (12) to a controller (12), and the controller (12) is arranged to respond to the performance information by transmitting appropriate control signals to the switching means (4).

5. An apparatus as claimed in claim 1, characterized in that the rotary apparatus is a propeller hub carrying a plurality of propeller blades and the at least one electrically power device is a heating element provided on each propeller blade.

6. An apparatus as claimed in claim 4, characterized in that the rotary apparatus is a propeller hub carrying a plurality of propeller blades, the at least one electrically powered device is a heating element provided on each propeller blade, and at least one of the voltage and current supplied to each individual heating element is monitored and appropriate information transmitted to the controller.

7. An apparatus as claimed in claim 1, characterised in that the switch means are electrically controllable switches.

8. A rotary apparatus incorporating at least one electrically powered device on an aircraft rotor, the apparatus comprising an electrical generator having inductive windings carried for rotation with the rotor, switching means on the rotor responsive to a control signal to supply the at least one electrically powered device, and fixed permanent magnets, in which the inductive windings co-operate with the fixed permanent magnets to generate an induced voltage when the rotor rotates relative to the fixed magnets, the control signal is supplied to the switching means via a contactless inductive communication link between the rotor and a structure on which the rotor is rotatably mounted, the inductive windings comprise part of the communication link and a control winding is provided on the magnets and in use the control winding is modulated with a control signal to transmit data over the communication link.

9. An apparatus as claimed in claim 8, characterized by a controller for controlling the supply of power to the at least one electrically powered device, the controller having a connection to the control winding for transmitting control signals by modulating the control signal in the control winding.

10. An apparatus as claimed in claim 8, characterized in that a contactless communication link is used to transmit performance information from the rotor to a controller and the controller is arranged to respond to the performance information by transmitting appropriate control signals to the switching means.

11. An apparatus as claimed in claim 8, characterized in that the rotary apparatus is a propeller hub carrying a plurality of propeller blades and the at least one electrically powered device is a heating element provided on each propeller blade.

12. An apparatus as claimed in claim 8, characterized in that the switch means are electrically controllable switches.