Shipping frame for fan section of aircraft engine
AssigneeStanley Aviation Corporation
InventorsRobert F. Hatch, Ronald A. Rossway, William J. Campion, Jr.
Life of this patent
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AssigneeStanley Aviation Corporation
InventorsRobert F. Hatch, Ronald A. Rossway, William J. Campion, Jr.
Estimating the term…
A fan shipping frame includes a frame assembly for supporting a loaded fan section of a jet aircraft engine. A plurality of caster assemblies attached to the shipping frame provide locomotive capability and adjustable height positioning so that a loaded fan section may be transferred onto the appropriate transport aircraft or vehicle. Rail members mounted on the frame assembly are alignable with rail members of a fan dolly so that the fan section may be directly transferred from the fan dolly onto the shipping frame. A template integral with the shipping frame enables the fan section to be mounted thereon. A platform assembly rotatably mounted to the shipping frame may be deployed to enable the fan section to be tilted or tipped from a vertical transport position to a horizontal transport position wherein the shipping frame may be transported in either position. A storage container mounted on the shipping frame stores the removed fan blades of the fan section in either position. In one embodiment, a telescoping template support group is provided enabling the template to be raised or lowered so that it is able to readily connect to fan sections which have differing heights when mounted to structures such as the fan dolly.
A shipping frame for transporting an object such as a loaded jet aircraft engine fan section, said shipping frame comprising:
A shipping frame for transporting an object such as a fan section of a jet aircraft engine loaded thereon, said shipping frame comprising:
A shipping frame for transporting an object such as a jet aircraft engine fan section loaded thereon, said shipping frame comprising:
A method of preparing a jet aircraft engine component for transport, said method comprising the steps of:
A method of preparing a component of a jet aircraft engine for transport, said method comprising the steps of:
Dependencies are inferred from the claim text.