Mounting device and method of assembling the same
AssigneeUnison Industries, LLC
InventorsAdam Benjamin Cox, William Ward Owens, Bruce D. Markert
Life of this patent
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Abstract
A method of assembling a mounting device for an electrical harness of a gas turbine engine is provided. The electrical harness has a wire bundle. The method includes providing a first shell and providing a second shell. The method further includes coupling the first shell to the second shell with the wire bundle disposed between the first shell and the second shell such that movement of the first shell and the second shell along the wire bundle is restricted.
Claims20
A method of assembling a mounting device for an electrical harness of a gas turbine engine, the electrical harness having a wire bundle, said method comprising:
- providing a first shell and a second shell, wherein each of the first shell and the second shell has a first end region, a second end region, and a middle region between the first end region and the second end region;
- and
- coupling the first shell to the second shell with the wire bundle disposed between the first shell and the second shell such that movement of the first shell and the second shell along the wire bundle is restricted, and such that the middle region defines a mounting seat that is closer to the wire bundle than the first end region and the second end region.
A mounting device for an electrical harness of a gas turbine engine, the electrical harness having a wire bundle, said mounting device comprising:
- a first shell and a second shell, wherein each of said first shell and said second shell comprises a first end region, a second end region, and a middle region between said first end region and said second end region, wherein said middle region defines a mounting seat that is configured to be closer to the wire bundle than said first end region and said second end region;
- and
- at least one fastener configured to couple said first shell to said second shell with the wire bundle disposed between said first shell and said second shell such that movement of said first shell and said second shell along the wire bundle is restricted.
An electrical harness for a gas turbine engine, said electrical harness comprising:
- a wire bundle comprising a covering and a plurality of wires disposed within said covering;
- and
- a mounting device coupled to said wire bundle, wherein said mounting device comprises:
- a first shell and a second shell, wherein each of said first shell and said second shell comprises a first end region, a second end region, and a middle region between said first end region and said second end region, wherein said middle region defines a mounting seat that is closer to the wire bundle than said first end region and said second end region;
- and
- at least one fastener configured to couple said first shell to said second shell with said wire bundle disposed between said first shell and said second shell such that movement of said first shell and said second shell along said wire bundle is restricted.
Dependencies are inferred from the claim text.