Back Mounted Flight Machine

Abstract

A back mounted flight machine comprises a frame comprising a connecting bracket, a pair of lateral arms extending from the connector bracket, and an engine mounted on each of the lateral arms in a selected position. A harness is mounted on the connecting bracket of the frame between the pair of lateral arms. Further, a fastening mechanism is provided for connecting the harness to the connecting bracket to permit relative movement between the harness and the frame in a plurality of orientations.

1 . A back mounted flight machine comprising:
 a frame comprising a connecting bracket, a pair of lateral arms extending from the connector bracket, and an engine mounted on each of the lateral arms in a selected and variable position;   a harness mounted on the connecting bracket of the frame and between the pair of lateral arms; and   a fastening mechanism for connecting the harness to the connecting bracket of the frame to permit relative movement between the harness and the frame in a plurality of orientations.   
     
     
         2 . (canceled) 
     
     
         3 . A back mounted flight machine as claimed in  claim 1  wherein each of the pair of lateral arms comprises a control arm to facilitate relative movement between the harness and the frame and a mounting arm for receiving the engine. 
     
     
         4 . A back mounted flight machine as claimed in  claim 1  wherein each of the pair of lateral arms comprises a control arm and a mounting bracket for mounting the engine on the control arm. 
     
     
         5 . A back mounted flight machine as claimed in  claim 1  wherein each lateral arm has multiple points for connection of the engine so that the engine may be positioned at a selected and variable point along the lateral arm. 
     
     
         6 . (canceled) 
     
     
         7 . A back mounted flight machine as claimed in  claim 1  further comprising an engine mounting bracket for mounting the engine to the lateral arm. 
     
     
         8 . A back mounted flight machine as claimed in  claim 7  wherein the engine is mounted to the engine mounting bracket at one of several mounting positions so that the distance between the engine and the lateral arm can be selectively varied. 
     
     
         9 . A back mounted flight machine as claimed in  claim 7  wherein the engine is mounted to the engine mounting bracket in one of several mounting positions so that the engine may be vertically higher or lower relative to the lateral arm. 
     
     
         10 . A back mounted flight machine as claimed in  claim 1  wherein the fastening mechanism comprises a pair of vertical brackets within the connecting bracket, a rod rotatably received by the vertical brackets, a fastening plate fixed to the harness, and a rod end having a first end rotatably secured to the rod and a second end connected to the fastening plate. 
     
     
         12 . A back mounted flight machine as claimed in  claim 1  wherein the relative movement between the harness and the frame in a plurality of orientations includes movement wherein the frame and harness can move in a clockwise and counterclockwise direction relative to each other and in a fore and aft direction relative to each other. 
     
     
         13 . A back mounted flight machine as claimed in  claim 1  further comprising a control handle formed at an end of each of the pair of lateral arms, the control handle facilitating engine control and relative orientation between the harness and the frame. 
     
     
         14 . A back mounted flight machine as claimed in  claim 13  wherein the control handle includes a rotatable engine control post for controlling engine output. 
     
     
         15 . A back mounted flight machine as claimed in  claim 13  wherein the control handle includes an emergency switch for altering engine output, the emergency switch including a tie connectable to a pilot, such that selected movement of the hand of the pilot will cause the tie to activate the emergency switch. 
     
     
         16 . A back mounted flight machine as claimed in  claim 13  wherein the control handle includes a tab on an outer surface thereof, the tab cooperating with a spring-loaded arm for controlling thrust of the engine. 
     
     
         17 . (canceled) 
     
     
         18 . A back mounted flight machine as claimed in  claim 1  wherein the engines mounted on the lateral arms are turbines which are counter-rotating, rotating in different directions to each other in order to provide stability to the flight machine. 
     
     
         19 . A back mounted flight machine as claimed in  claim 1  further comprising a pair of retractable barriers formed between the harness and the engines, the retractable barriers been movable between a first extended position between the harness and the engines, and a second retracted position. 
     
     
         20 . A back mounted flight machine as claimed in  claim 1  further comprising a retractable post for supporting the flight machine when on solid ground. 
     
     
         21 . A back mounted flight machine as claimed in  claim 1  further comprising a compartment for a stored parachute, wherein the parachute can be deployed in both emergency and non-emergency situations. 
     
     
         22 . (canceled) 
     
     
         23 . A back mounted flight machine as claimed in  claim 1  wherein each engine comprises deflectors to facilitate control of direction of the flight machine, the deflectors being connected to a hand control device formed on the lateral arms by cables. 
     
     
         24 . A back mounted flight machine as claimed in  claim 13  wherein the hand control is rotatable and calibrated such that thrust increases at a greater rate during the early stages of rotation of the hand control, and at a lesser rate once the flight device is airborne. 
     
     
         25 . A back mounted flight machine as claimed in  claim 1  further comprising a cooling mechanism whereby oil is deposited at bearings within the engine after shut down but before engine rotation has ceased.