INTERNATIONAL PATENT APPLICATION OF

THOMAS G. PACKARD

7005 150 ^th PL. SW. EDMONDS , WA. 98026 , US

TITLE OF THE INVENTION : ROTOR ENERGY VEHICLE

REFERENCE TO RELATED PRIOR APPLICATIONS:

PROVISIONAL APPLICATION : US60/817.141 , FILEING DATE 29/JUNE/2006

UTILITY APPLICATION:

TITLE: ROTOR ENERGY AUGMENTED VEHICLE

APPLICANT: THOMAS G. PACKARD

FILING DATE 19, JUNE, 2007

DATE : 25 , JUNE , 2007

ROTOR ENERGY VEHICLE : BACKGROUND OF THE INVENTION

Energy utilization and cost associated with various moving vehicles is becoming an increasing social/economic and environmental problem. The aerodynamic/ hydrodynamic energy efficiency of transportation vehicles has not improved

significantly in resent times, The proposed invention is thought to be a significant development and elementary air flow vehicle simulation tests indicate the feasibility and validity of the concept The idea of extracting energy from a generated

air/medium flow is generally not a practicable process as the input energy is of course greater than the output energy however if the input energy is not increased

in the process and the input energy in the flow is to be lost in total then extracting air/medium flow energy can be practicable.

ROTOR ENERGY VEHICLE: BRIEF DESCRIPTION OF THE INVENTION A vehicle : truck , bus , car, etc. , is designed and constructed such that the frontal area is covered or shielded with some type of air rotor and the

resistance air flow against the moving vehicle is in part or in total directed against the rotor and not against shielded area . The air rotor is designed to rotate with the air flow force against it such that energy can be extracted from the air flow which would be other wise be completely lost

without the rotor or if the rotor is not allow to rotate/spin. The energy required to drive/move the vehicle is essentially the same with a stationary rotor or

without the rotor as the rotor area is less than or no larger than the vehicle and shields the vehicles frontal resistance area however the net energy expended is less when the rotor rotates extracting energy from the air flow which would otherwise be lost and rotary energy/motion is coupled directly or indirectly to vehicle driving wheels. This extracted and saved air flow derived rotary energy can of course be used for other energy uses.

If desired more than one rotor can be attached or coupled to the front of the vehicle in a vertical arrangement for unproved driver visibility . Rotors can also be constructed or attached in tandem with a smaller diameter rotor leading a larger diameter rotor for less resistance and improved efficiency . A squirrel cage type rotor can also be attached to the front of the vehicle and also coupled to the rear of the vehicle and extract energy from the trailing pressure

differential.

A rectangular assembly of air foil slats or wings can also be

arranged on two thin belts between two separated two wheel rotating assemblies , see drawings, Fig. 9/10.

A marine vessel can also be constructed with a rotor on the submerged bow of the vessel/ship to extract energy from the motion displaced water that would otherwise be lost . The water resistance against hull would be decreased by the

shield effect of the rotor and the overall resistance would not be significantly increased as the rotor frontal resistance area would be less or no larger than the hull frontal resistance . This extracted or generated rotary energy can utilized to

reduce the net/total energy to required to drive the ship by connecting to stern propellers.

An aircraft can also be constructed with a front fuselage shielding rotor/turbine/fan that is smaller in resistance area than the fuselage itself . More than one rotors/turbines/fans may be arranged in a tandem to form a cone shape for better aerodynamics. The rotor/turbine/fan with an associated appropriate mechanical and or electrical arrangement would be connected to a

rear fuselage, tail driving propeller , or other propellers , for a net reduction in expended energy .

DESCRIPTION OF THE DRAWINGS

Figure 1, Front view of truck with shrouded, louvered turbine/fan rotor and drive wheels

Figure 2, Side view of the rotor , automatic transmission , differential and drive wheel.

Figure 3 , Side view of rotor shroud.

Figure 4, side view of vehicle with drive rotor and independent drive wheels

Figure 5 , Side view of rotor vehicle with internal power coupling to the vehicle wheels

Figure 6 , Front view of rotor vehicle with squirrel cage type rotor.

Figure 7 , Side view of vehicle with front and rear squirrel cage type rotors with associated drive wheels.

Figure 8 , Front view of vehicle with raised driver cab and rotor.

Figure 9 , Side view of vehicle with dual rectangular rotor assemblies and belt/chain coupling to each independent front rectangular/rotor drive wheels.

Figure 10 , Front view of dual rectangular rotor.

DETAILED DESCRIPTION OF A ROTOR ENERGY VECHICLE

The front of the vehicle will have a large diameter axial/turbine ( windmill type) air rotor Fig. 1,1 , Fig. 2,1 , Fig. 4, 1 , Fig. 5, 1 , Fig.8,1 that approximately equals or is a little less than the overall width of the vehicle frontal area and does not protrude above or below . For a general truck/bus this is about eight feet

however for current vehicle designs seven feet will provide better driver visibility . The rotor will have sixteen ,16, overlapping blades , Fig. 1 ,2 , Fig 2, 2 , Fig. 4,1 ,

Fig. 5,1 , Fig. 8 ,2 that are made of clear 1/2 inch or more thick plexiglass or clear plastic material and will also have a circular shroud Fig. 3,1. The center axle of the rotor Fig. 2,3 will be connected to an automatic transmission/gear box Fig.1,3 , Fig 2,4 , Fig.4 , Fig.5 . The output drive shaft , Fig.1 ,4 , Fig. 2,5 , Fig.4 , will connect to a lower differential Fig 1,5 ,Fig. 2,6 , The two differential output axles Fig.l,6 , Fig.2,7 will connect to two rotor drive wheels Fig. 1,7 , Fig. 2,8 , Fig. 4,2 . The axle , wheel connections will allow for horizontal , vertical miss alignment and turning as each rotor drive wheel will connected to the adjacent main steering wheel and turn in the horizontal plane . The rotor drive wheels will also have vertical movement ability .The rotor drive wheels will be centered in line with the vehicles main front wheels Fig.1,8 , Fig. 4, 3 to minimize air flow resistance. Larger diameter air rotors can be constructed into vehicles if the height of the drivers location/position and cab Fig. 8,2 is raised for better visibility over and /or

around the rotor.

The air rotor vehicle can also be constructed with a squirrel cage type of air rotor Fig. 6,1 , Fig.7,1 with drive wheels Fig. 7,3 , Fig. 7,4 , for better driver visibility and in this construction the enclosed rotor end will be made of a clear plastic material or the driver cab itself can form and makeup the enclosing end of the rotor . This type of rotor can also be constructed into or onto the rear trailing

end of the vehicle Fig. 7,2 and abstract useful energy from the trailing pressure differential . The air rotor vehicle can also be constructed such that its

transmission output is coupled to the vehicles engine or main wheels Fig.5, Fig 6 , Fig.8 , . If the vehicle is electrically powered or a hybrid , the rotor can drive a generator/alternator. A vehicle , Fig. 9, is shown with a rectangular type of moving assemblies Fig.9, 1 . The front view of the dual , independent airfoil slats moving assemblies Fig. 10 , one driving assembly coupled to each independent front wheel shown in Fig. 9.2. Other rotor designs/variations , types , vehicles and

vehicle connections are of course possible.