Stanley Aviation Corporation

Ronald A Rossway

Robert F Hatch

David E Jewell

Behzad B Suroosh

Ronald W Boscaljon

Eric Hazelwood

William J Campion, Jr

An aircraft engine shipping system includes a frame assembly for supporting the aircraft engine, and a cradle assembly mounted on the frame assembly for securing the aircraft engine to the frame assembly. The frame assembly includes shock absorbers to provide continual shock absorption to an aircraft engine loaded thereon. The shipping system may be configured in either a truck or air transport mode. In the truck transport mode, the aircraft engine is secured to the cradle assembly by an aft ring which attaches to the aft portion of the aircraft, and a pair of cradle arms which attach to the forward portion of the aircraft engine. In the air transport mode, the aircraft engine is attached to the cradle assembly by the aft ring, and a forward ring which attaches directly to the fan of the aircraft engine. In the air transport mode, the cradle arms are disconnected from the aircraft engine and rotated away from the engine in a stowed position. While in the air transport mode, the aircraft engine may be rotated wherein the forward and aft rings cooperate to achieve rotation of the aircraft engine. A jack system is used to raise or lower the aircraft engine in either the truck or air transport modes.

Shipping system for jet aircraft engine

An aircraft engine shipping system includes a frame assembly for supporting the aircraft engine, and a cradle assembly mounted on the frame assembly for securing the aircraft engine to the frame assembly. The frame assembly includes shock absorbers to provide continual shock absorption to an aircraft engine loaded thereon. The shipping system may be configured in either a truck or air transport mode. In the truck transport mode, the aircraft engine is secured to the cradle assembly by way of an aft ring which attaches to the aft portion of the aircraft, and a pair of cradle arms which attach to the forward portion of the aircraft engine. In the air transport mode, the aircraft engine is attached to the cradle assembly by way of the aft ring, and a forward ring which attaches directly to the fan of the aircraft engine. In the air transport mode, the cradle arms are disconnected from the aircraft engine and rotated away from the engine in a stowed position. While in the air transport mode, the aircraft engine may be rotated wherein the forward and aft rings cooperate to achieve rotation of the aircraft engine. A jack system is used to raise or lower the aircraft engine in either the truck or air transport modes.

Method of installing and removing jet aircraft engine

An aircraft engine shipping system includes a frame assembly for supporting the aircraft engine, and a cradle assembly mounted on the frame assembly for securing the aircraft engine to the frame assembly. The frame assembly includes shock absorbers to provide continual shock absorption to an aircraft engine loaded thereon. The shipping system may be configured in either a truck or air transport mode. In the truck transport mode, the aircraft engine is secured to the cradle assembly by means of an aft ring which attaches to the aft portion of the aircraft, and a pair of cradle arms which attach to the forward portion of the aircraft engine. In the air transport mode, the aircraft engine is attached to the cradle assembly by the aft ring the aft ring, and a forward ring which attaches directly to the fan of the aircraft engine. In the air transport mode, the cradle arms are disconnected from the aircraft engine and rotated away from the engine in a stowed position. While in the air transport mode, the aircraft engine may be rotated wherein the forward and aft rings cooperate to achieve rotation of the aircraft engine. A jack system is used to raise or lower the aircraft engine in either the truck or air transport modes.

Shipping system for jet aircraft engine and method of installing and removing jet aircraft engine

In the first embodiment, a coupling assembly is provided wherein the inner peripheral diameter of an annular spring is sized to be threadably received over the threads of a coupler and is held in a recess formed by the ends of threads and the edge of a shoulder. This structure minimizes the diameter of the annular spring and lock ring to minimize both the size and weight of coupling assembly. Additionally, it provides a quick connect, quick disconnect coupling and has a peripheral stripe to provide a visual indication of its connected or disconnected status. In the second embodiment, a wavy spring is split which allows its diameter to be temporarily enlarged so that it can be received over the threads of the coupler and then spring back to its original smaller diameter so that it is held in a recess formed by the ends of the threads and a coupler flange. This structure also minimizes the diameter of the annular spring and lock ring to minimize both the size and weight of coupling assembly. This structure also provides a quick connect, quick disconnect coupling and has an indicator stripe to identify whether or not the coupler is in locked position.

Lightweight positive lock coupling

A first coupling member has a peripheral facing surface with a pair of annular slots, each of a different length and width. A second coupling member has a lock ring longitudinally slidable thereon with a facing surface having a pair of annular raised locking tabs sized to correspond to the respective annular slots. A resilient annular spring mounted within the lock ring urges it toward the first coupling member so that the locking tabs engage their respective slots when the coupling is tightened to a predetermined extent during rotation in the locking direction to releasably and positively lock the coupling. An indicator stripe on the peripheral edge of the first coupling member is exposed before the locking tabs and slots are engaged. Alignment between the respective locking tabs and slots allows longitudinal movement of the lock ring so that it covers the indicator stripe. One of the coupling members has a peripheral groove and two angularly spaced longitudinal keyways of differing widths which intersect the peripheral groove. The annular spring has an internal peripheral edge with a plurality of peripherally spaced spring tabs for holding it in the peripheral groove. A spring key on the internal peripheral edge of the annular spring has a width corresponding to the width of one of the keyways to rotationally position the annular spring with the coupling member. The annular wall of the lock ring has two angularly spaced keys of differing widths which correspond to the widths of the keyways and are received therein to angularly position the lock ring with the coupling member and the spring.

Positive lock coupling

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.

Shipping frame for fan section of aircraft engine

A threaded coupling assembly is provided for interconnecting the ends of first and second fluid-carrying conduit members in fixed releasably locking relationship. First and second coupling members are circumferentially engageable with the ends of the conduit members to hold them in fluid communication. The coupling members are rotatable in a locking direction and in an opposite unlocking direction. The first coupling member has a peripheral facing surface with a pair of annular slots, each of a different length and width. The second coupling member has a lock ring longitudinally slidable thereon with a facing surface having a pair of annular raised locking tabs. Each locking tab is of a predetermined height but of a different length and width which corresponds to the respective length and width of the annular slots. A resilient annular spring urges the lock ring toward the first coupling member so that the locking tabs engage their respective slots when the coupling is tightened to a predetermined extent during rotation in the locking direction to releasably and positively lock the coupling. An indicator stripe is provided on the peripheral edge of the first coupling member which is exposed before the locking tabs and slots are engaged. The indicator stripe is no wider than the height of the locking tabs so that it is covered by the lock ring when the lock ring snaps into locking engagement to provide a visual indication to the mechanic that the coupling assembly is positively locked.

Growing community of inventors

Aurora, CO, United States of America

Ronald A Rossway