Wireless Power Transmission System and Method for an Aircraft Sensor System
AssigneeSimmonds Precision Products, Inc.
InventorsRobert S. Bugash, Scott T. Fusare
Life of this patent
Estimating the term…
Abstract
An aircraft sensor system including a primary module configured to be attached to an aircraft portion and operative to transmit electrical power wirelessly. A secondary module configured to be attached to an aircraft component, the secondary module operative to receive electrical power wirelessly from the primary module. At least one sensor configured to be operatively attached to a portion of the aircraft component and electrically coupled to the secondary module, wherein the at least one sensor is operative to measure a desired parameter of the aircraft component.
Claims22
An aircraft sensor system, the system comprising:
- a primary module configured to be attached to an aircraft portion, the primary module operative to transmit electrical power wirelessly;
- a secondary module configured to be attached to an aircraft component, the secondary module operative to receive electrical power wirelessly from the primary module;
- and
- at least one sensor configured to be operatively attached to a portion of the aircraft component and electrically coupled to the secondary module, wherein the at least one sensor is operative to measure a desired parameter of the aircraft component.
An aircraft sensor system, the system comprising:
- a primary module configured to be attached to an aircraft portion, the primary module operative to transmit electrical power wirelessly and operative to receive data wirelessly;
- a secondary module configured to be attached to an aircraft component, the secondary module operative to receive electrical power wirelessly from the primary module and transmit data wirelessly to the primary module;
- and
- at least one sensor configured to be operatively attached to a portion of the aircraft component and electrically coupled to the secondary module, wherein the at least one sensor is operative to measure a desired parameter of the aircraft component and provide corresponding data to the secondary module.
(canceled)
22-24. (canceled)
Dependencies are inferred from the claim text.