Rotorcraft winch lighting device and method of operating a rotorcraft winch lighting device

Patent metadata

Field	Value
Publication number	US-9994333-B2
Application number	US-201615190442-A
Country	US
Kind code	B2
Filing date	Jun 23, 2016
Priority date	Jun 24, 2015
Publication date	Jun 12, 2018
Grant date	Jun 12, 2018

Abstract

A rotorcraft winch lighting device, which is attachable to a rotorcraft winch, mounted to a rotorcraft such as a helicopter, the rotorcraft winch including a stationary portion and a mobile portion which is movable with respect to the stationary portion, includes: a stationary unit including a stationary coil and a mobile unit. The mobile unit is movable with respect to the stationary unit and includes at least one light source, at least one electrical storage device, and at least one mobile coil, which is electrically connected to the electrical storage device and/or the at least one light source. The stationary coil and the mobile coil are configured for transferring electrical energy from the stationary unit to the mobile unit when the at least one mobile coil is positioned in an energy transfer position in the vicinity of the at least one stationary coil.

First claim

The invention claimed is:

1. A rotorcraft winch lighting device comprising:
a stationary unit, including:
at least one stationary coil; and
a mobile unit, the mobile unit being movable with respect to the stationary unit and comprising at least one light source, at least one electrical storage device, and at least one mobile coil, which is electrically connected to the electrical storage device and/or the at least one light source;

wherein the lighting device is attachable to a rotorcraft winch, mounted to a rotorcraft, the rotorcraft winch comprising a stationary portion and a mobile portion which is movable with respect to the stationary portion,
wherein the at least one stationary coil and the at least one mobile coil are configured for transferring electrical energy from the stationary unit to the mobile unit when the at least one mobile coil is positioned in an energy transfer position in the vicinity of the at least one stationary coil.

2. A rotorcraft winch lighting device of claim 1 , wherein the stationary unit is attached to or integral with the stationary portion of the rotorcraft winch.

3. A rotorcraft winch lighting device of claim 1 , wherein the at least one light source comprises at least one LED.

4. A rotorcraft winch lighting device of claim 1 , wherein the electrical storage device comprises at least one of a battery, a capacitor and a super capacitor.

5. A rotorcraft winch lighting device of claim 1 , wherein the at least one mobile coil is elastically supported by the mobile unit.

6. A rotorcraft winch lighting device of claim 1 , wherein the mobile unit comprises a first component and a second component, wherein the second component supports or houses the at least one mobile coil and is elastically supported by the first component.

7. A rotorcraft winch lighting device of claim 6 , wherein the at least one light source is supported by the first component.

8. A rotorcraft winch lighting device of claim 1 , further comprising a positional sensor, which is configured for detecting whether the mobile coil is positioned in the energy transfer position.

9. A rotorcraft winch lighting device of claim 7 , wherein the positional sensor is a capacitive sensor attached to the stationary unit and is configured for detecting a capacitive element attached to the mobile unit of the lighting device.

10. A rotorcraft winch lighting device of claim 1 , in which the mobile unit additionally comprises at least one indicator element, which is configured for providing information about the momentary storage state of the electrical storage device.

11. A rotorcraft winch lighting device of claim 1 , wherein the mobile unit further comprises a power management controller, which is configured for monitoring and/or controlling the electrical energy supplied to the electrical storage device and/or the at least light source.

12. Rotorcraft, in particular helicopter, comprising a rotorcraft winch and a rotorcraft winch lighting device according to claim 1 .

13. A method of operating a rotorcraft winch lighting device according to claim 1 , including the steps of:
positioning the mobile coil in the energy transfer position next to the stationary coil, and
supplying an alternating current to the stationary coil.

14. Method of operating a rotorcraft winch lighting device according to claim 13 , further including the steps of:
activating the at least one light source, and
moving the mobile unit from the energy transfer position next to the stationary unit to an operating position distant from the stationary unit.

Assignees

• Goodrich Lighting Systems Gmbh

Inventors

• Kube Adrian

Classifications

• B64D1/22

  Taking-up articles from earth's surface · CPC title

• B64C27/04

  Helicopters · CPC title

• H02J50/10

  using inductive coupling · CPC title

• B66D1/60 Primary

  adapted for special purposes · CPC title

• B64D47/00

  Equipment not otherwise provided for · CPC title