PIVOT MOUNT ASSEMBLY
First Claim
1. An aircraft tablet mount assembly for mounting a tablet computer to the steering control of an aircraft, comprising:
- a receiving piece configured to receive an electronic device and having one or more tension elements configured to secure the electronic device; and
a pivot mount assembly configured to mount the tablet mount assembly to the steering control of the aircraft, comprising;
an upper portion having a top surface including a receiving slot configured to receive and secure the receiving piece;
a lower portion connected to the upper portion such that the upper portion is rotatable with respect to the lower portion, the lower portion having positioning flange on an underside thereof and a securing mechanism disposed along a lower edge of the lower portion; and
a mounting receiver mounted on the steering control of the aircraft and configured to receive said positioning flange and said securing mechanism of said lower portion.
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Accused Products
Abstract
A tablet mount assembly for mounting an electronic device (e.g., an Apple® iPad®) in the cockpit of an aircraft, and more specifically on the steering control of the aircraft. The tablet mount includes a receiving piece and a pivot mount assembly that includes an upper portion and a lower portion. The upper portion is rotatable with respect to the lower portion. The upper portion includes a slot for connecting to the receiving piece, and the lower portion includes a securing mechanism and a positioning flange. The upper portion of the assembly is rotatable with respect to the lower portion, thereby allowing the electronic device to be mounted to be rotated from a portrait to a landscape orientation without removing the same from the mount. An indexing position system may be integrated between the lower and upper portions of the mount assembly and provides predetermined rotation increments for the device.
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Citations
10 Claims
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1. An aircraft tablet mount assembly for mounting a tablet computer to the steering control of an aircraft, comprising:
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a receiving piece configured to receive an electronic device and having one or more tension elements configured to secure the electronic device; and a pivot mount assembly configured to mount the tablet mount assembly to the steering control of the aircraft, comprising; an upper portion having a top surface including a receiving slot configured to receive and secure the receiving piece; a lower portion connected to the upper portion such that the upper portion is rotatable with respect to the lower portion, the lower portion having positioning flange on an underside thereof and a securing mechanism disposed along a lower edge of the lower portion; and a mounting receiver mounted on the steering control of the aircraft and configured to receive said positioning flange and said securing mechanism of said lower portion. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10)
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Specification