Repair and replacement mechanism for personal control units on aircraft
11242148 · 2022-02-08
Assignee
Inventors
Cpc classification
B64D11/00152
PERFORMING OPERATIONS; TRANSPORTING
B64D11/00155
PERFORMING OPERATIONS; TRANSPORTING
H05K7/12
ELECTRICITY
B60R2011/0071
PERFORMING OPERATIONS; TRANSPORTING
International classification
B64D11/00
PERFORMING OPERATIONS; TRANSPORTING
H05K7/12
ELECTRICITY
Abstract
An assembly for opening or accessing an electronic communication and entertainment device holder for repair or replacement of its contents, including a latch which can be released by the contraction of an attached muscle wire actuator in response to a low current pulse sent by an attached wireless receiver.
Claims
1. A mechanism for a placement, removal, repair and replacement of an electronic communication and entertainment device attached to the interior of an aircraft, the electronic communication and entertainment device having a first position whereby the electronic communication and entertainment device is operated by a wireless remote unit from a passenger, and a second position whereby the electronic communication and entertainment device is detaching from the interior of the aircraft, wherein movement of the electronic communication and entertainment device to the second position is operated by a separate handheld unit from a service technician for the placement, removal, repair and replacement of the electronic communication and entertainment device, the mechanism comprising; a) a wireless receiver for receiving an actuation signal from the wireless remote unit operated by the passenger and the separate handheld unit operated by the service technician, said wireless receiver generating a low current pulse therefrom, the low current pulse having heat associated therewith; b) a muscle wire actuator for receiving the heat from the low current pulse and contracting the muscle wire actuator in response thereto; c} latch connected to the muscle wire actuator, releasing the latch in response to the contracting of the muscle wire actuator; and d) an electron communication and entertainment device holder and the electronic communication and entertainment device are decoupling to completely detach and separate from the interior of the aircraft upon the releasing of the latch.
Description
BRIEF DESCRIPTION OF THE DRAWING
(1)
(2)
DETAILED DESCRIPTION OF THE INVENTION
(3) Set forth below is a description of what is currently believed to be the preferred embodiment or best examples of the invention claimed. Future and present alternatives and modifications to this preferred embodiment are contemplated. Any alternatives or modifications which make insubstantial changes in function, in purpose, in structure or in result are intended to be covered by the claims in this patent.
(4)
(5) As shown in
(6) The above description is not intended to limit the meaning of the words used in the following claims that define the invention. Rather, it is contemplated that future modifications in structure, function or result will exist that are not substantial changes and that all such insubstantial changes in what is claimed are intended to be covered by the claims. For instance, the specific muscle wire actuator in the examples of the preferred embodiments of present invention is for illustrative purposes with reference to the example drawings only. Also, while the present preferred embodiment deals with aircraft, the invention is equally applicable to non-aircraft and non-vehicle applications, too. Furthermore, the way in which the holder decouples from the seat back can involve any variety of displacement, not just the bottom hinge “tilt forward” mechanism disclosed above. Likewise, it will be appreciated by those skilled in the art that various changes, additions, omissions, and modifications can be made to the illustrated embodiments without departing from the spirit of the present invention. All such modifications and changes are intended to be covered by the following claims.