초록 ▼

A transport tool is disclosed for moving an aircraft monument from one location to another. The transport tool comprises an elongated, substantially rectangular, support frame having handle members at an upper region, wheel elements at a lower region, and a leg pivoted to the mid-region of the tool

A transport tool is disclosed for moving an aircraft monument from one location to another. The transport tool comprises an elongated, substantially rectangular, support frame having handle members at an upper region, wheel elements at a lower region, and a leg pivoted to the mid-region of the tool for supporting a load mounted to the tool as the transport tool is rotated about the wheel elements from a vertical orientation in which the load can be loaded onto, or unloaded from, the tool to a horizontal orientation in which the load can be transported from one location to another. Also disclosed is a method for transporting the load between two locations using the transport tool.

대표청구항 ▼

1. A transport tool for moving an aircraft monument from a manufacturing location to an installation location, comprising: an elongated substantially planar support frame having handle members at a first end region extending in a first direction, a support plate at a second end region extending in a

1. A transport tool for moving an aircraft monument from a manufacturing location to an installation location, comprising: an elongated substantially planar support frame having handle members at a first end region extending in a first direction, a support plate at a second end region extending in a second opposite direction, and wheels at said second end region extending in said first direction,an upper monument engaging element configured to engage an upper surface of the aircraft monument, said upper monument engaging element positioned at the first end region,a lower monument engaging element configured to engage a lower side of the aircraft monument, said lower monument engaging element positioned at the second end region,a leg member pivotally attached at one end thereof to a central region of said support frame such that said leg member is movable between a first position, a second position, and a third position, said leg member having at least one wheel on its free end, wherein the free end is substantially proximate to the wheels at the second end region when said leg member is in the first position, the free end is remote from the wheels at the second end region when said leg member is in the second position, is adjacent to the first end region when said leg member is in the third position, and contacts said support frame when said leg member is in one of the first position and the third position, anda biasing mechanism coupled to said frame and said leg member for urging said leg member towards said support frame into the first position. 2. The transport tool of claim 1, wherein said biasing mechanism comprises at least one of a spring and a piston. 3. The transport tool of claim 1, wherein said biasing mechanism is carried by said support frame in the near vicinity of said central region and includes biasing elements that control the rate of pivoting movement of said leg member away from said support frame so that said support frame can be slowly rotated from a first substantially vertical orientation, in which said leg member is in the first position and the support frame can be secured to the aircraft monument, to a second substantially horizontal orientation, in which the free end of said leg member moves to at least one of the second position and the third position at a controlled rate away from the wheels at said second end region of said support frame to support the monument for movement from one location to another. 4. The transport tool of claim 3, wherein said biasing elements comprise a tubular member secured to the support frame at said central region and at least one torsion spring housed within said tubular member and coupled to said leg member. 5. The transport tool of claim 4, wherein said biasing elements further comprise at least one piston member coupled between said tubular member and said support frame for urging said leg member toward said first orientation. 6. The transport tool of claim 5, wherein said at least one piston member is compressed when said leg member free end moves away from said first position thereby countering the weight of said monument on said support frame as the latter is rotated from the first orientation to the second orientation. 7. The transport tool of claim 6, wherein said when said support frame is rotated into said second substantially horizontal orientation, the at least one piston member applies a resistive force to said leg member counteracting the movement of said leg member away from said first position. 8. The transport tool of claim 7, wherein at least one of said upper monument engaging element and said lower monument engaging element is selectively adjustable. 9. The transport tool of claim 1, and further comprising side monument engaging elements projecting forwardly from the support frame for gripping sides of the monument. 10. A tool for transporting an aircraft monument from one location to another location, comprising: a rectangular frame having rearwardly extending handle members at an upper end, a support plate at a lower end extending forwardly for engagement with a bottom surface of a monument, and wheels at said lower end on the rear side of said frame,an upper monument engaging member configured to engage an upper surface of the aircraft monument, said upper monument engaging member positioned adjacent to the upper end of said rectangular frame,a lower monument engaging member configured to engage a lower side of the aircraft monument and stabilize the aircraft monument relative to said rectangular frame when the aircraft monument is secured to said rectangular frame, said lower monument engaging member positioned adjacent to the lower end of said rectangular frame,a leg member attached at one end to a central portion of said frame such that said leg member is movable between a first position, a second position, and a third position, said leg member having at least one wheel on its other end, wherein the other end is substantially proximate to the wheels at said lower end when said leg member is in the first position, the other end is remote from the wheels at said lower end when said leg member is in the second position, is adjacent to said upper end when said leg member is in the third position, and contacts said rectangular frame when said leg member is in one of the first position and the third position, anda biasing mechanism coupled between said frame and said leg for urging the other end of said leg toward the wheels at said lower end and into the first position. 11. The tool of claim 10, wherein said one end of said leg member is attached to said frame at a pivot carried by said frame, said pivot facilitating rotation of said leg member thereabout, from the first position towards at least one of the second position and the third position, wherein said leg member is substantially adjacent to, and above the central portion of, said frame. 12. The tool of claim 11, wherein said leg member includes a wheel support member at its other end, said wheel support member being pivotally attached thereto. 13. The tool of claim 12 further comprising side monument engaging members that are disposed laterally of said tool frame.