The present disclosure relates generally to an aircraft oven, and more specifically to an oven employing a magnetically coupled fan.
Aircraft ovens typically coupled a fan and motor for operating the fan through a mechanical shaft coupling. However, this exposes the motor to extremely high heats and steam and degrades the seals, couplings, and motor itself. Although, conventional components and methods have generally been considered satisfactory for their intended purpose, there is still a need in the art for improved fan coupling for aircraft ovens. The present disclosure provides a solution for this need.
An appliance for use in an aircraft galley is disclosed. The appliance, an oven includes, a body defining an interior space, a motor configured to drive a fan propeller situated on an outside of the body, and a fan propeller situated within the interior space, wherein a shaft of a fan propeller is not in direct contact with a shaft of the motor. The shaft of the fan propeller can be joined to a first magnet array. The shaft of the motor can be joined to a second magnet array. The motor shaft and the fan shaft can be coupled by a magnetic coupling. The motor shaft and the fan shaft can be mechanically un-coupled during operation and be coupled only using a magnetic coupling.
The motor and the fan propeller can be separated by a wall. The shaft of the motor and the shaft of the propeller can form a single axis. A barrier can separate the shaft motor and the shaft propeller. The motor shaft can be entirely outside of the interior space. The motor can be driven by aircraft power. The appliance can be a sealed oven.
These and other features of the systems and methods of the subject disclosure will become more readily apparent to those skilled in the art from the following detailed description of the preferred embodiments taken in conjunction with the drawings.
So that those skilled in the art to which the subject disclosure appertains will readily understand how to make and use the devices and methods of the subject disclosure without undue experimentation, embodiments thereof will be described in detail herein below with reference to certain FIGURES, wherein:
Reference will now be made to the drawings wherein like reference numerals identify similar structural features or aspects of the subject disclosure. For purposes of explanation and illustration, and not limitation, a partial view of an exemplary embodiment of an aircraft appliance in accordance with the disclosure is shown in
Referring now to
The methods and systems of the present disclosure, as described above and shown in the drawings, provide for an aircraft appliance that is more reliable and longer operating times. While the apparatus and methods of the subject disclosure have been shown and described with reference to preferred embodiments, those skilled in the art will readily appreciate that changes and/or modifications may be made thereto without departing from the scope of the subject disclosure.