A hovercraft assembly includes a vehicle that may be driven. A pair of propulsion units is provided and each of the propulsion units is coupled to the vehicle. Each of the propulsion units may urge air outwardly from the body. Thus, the vehicle may levitate with respect to support surface. Each of t
A hovercraft assembly includes a vehicle that may be driven. A pair of propulsion units is provided and each of the propulsion units is coupled to the vehicle. Each of the propulsion units may urge air outwardly from the body. Thus, the vehicle may levitate with respect to support surface. Each of the propulsion units may direct the air in a selected direction with respect to the body. Thus, the propulsion units may urge the vehicle along the support surface in a selected direction. Each of the propulsion units is operationally coupled to the handlebars such that the handlebars control operational parameters of each of the propulsion units.
대표청구항▼
1. A hovercraft assembly comprising: a vehicle being configured to be driven, said vehicle including a body and a pair of handlebars, said body having a front end; anda pair of propulsion units, each of said propulsion units being coupled to said vehicle, each of said propulsion units being configur
1. A hovercraft assembly comprising: a vehicle being configured to be driven, said vehicle including a body and a pair of handlebars, said body having a front end; anda pair of propulsion units, each of said propulsion units being coupled to said vehicle, each of said propulsion units being configured to urge air outwardly from said body thereby facilitating said vehicle to levitate with respect to support surface, each of said propulsion units being configured to direct the air in a selected direction with respect to said body thereby facilitating said propulsion units to urge said vehicle along the support surface in a selected direction, each of said propulsion units being operationally coupled to said handlebars such that said handlebars control operational parameters of each of said propulsion units, one of said propulsion units being a jet engine having an intake and an exhaust, said jet engine being positioned within said body such that intake extends through said front end wherein said intake is configured to draw air inwardly into said jet engine thereby facilitating said jet engine to urge the air outwardly through said exhaust. 2. The assembly according to claim 1, further comprising a pair of nozzles, each of said nozzles being movably coupled to said body, each of said nozzles having an inlet and an outlet. 3. The assembly according to claim 1, further comprising: a pair of nozzles, each of said nozzles having an inlet and an outlet; anda conduit being fluidly coupled between said jet engine and each of said nozzles wherein each of said nozzles is configured to have the air urged outwardly through said outlet thereby facilitating each of said nozzles to produce thrust. 4. The assembly according to claim 3, further comprising a pair of dampers, each of said dampers being hingedly coupled to said conduit, each of said dampers being positioned within said conduit and being aligned with said inlet corresponding to an associated one of said nozzles, each of said dampers being selectively positioned between a closed position and an open position wherein each of said dampers is configured to regulate a flow of air being urged into said associated nozzle. 5. The assembly according to claim 4, further comprising a pair of second motors, each of said second motors being coupled to an associated one of said dampers such that each of said second motors positions said associated damper at a selected point between said open position and said closed position. 6. The assembly according to claim 5, wherein said pair of propulsion units including a first propulsion unit and a second propulsion unit, said nozzles corresponding to said first propulsion unit being spaced apart from each other and being distributed on a first lateral side of said body, said nozzles corresponding to said second propulsion unit being spaced apart from each other and being distributed on a second lateral side of said body, each of said nozzles corresponding to said first propulsion unit and said second propulsion unit being positioned adjacent to a bottom side of said body. 7. The assembly according to claim 6, further comprising: each of said propulsion units including a pair of first motors; anda processor being coupled to said body, said processor being electrically coupled to said handlebars, said processor being electrically coupled each of said first motors, each of said second motors and said jet engine corresponding to each of said propulsion units. 8. The assembly according to claim 7, further comprising a power supply being coupled to said body, said power supply being electrically coupled to said processor, said power supply comprising at least one battery. 9. The assembly according to claim 1, further comprising a fuel tank being coupled to said body wherein said fuel tank is configured to contain a liquid fuel, said fuel tank being fluidly coupled to said jet engine wherein said jet engine is configured to receive the liquid fuel from said fuel tank. 10. A hovercraft assembly comprising: a vehicle being configured to be driven, said vehicle including a body and a pair of handlebars, said body having a front end;a pair of propulsion units, each of said propulsion units being coupled to said vehicle, each of said propulsion units being configured to urge air outwardly from said body thereby facilitating said vehicle to levitate with respect to support surface, each of said propulsion units being configured to direct the air in a selected direction with respect to said body thereby facilitating said propulsion units to urge said vehicle along the support surface in a selected direction, each of said propulsion units being operationally coupled to said handlebars such that said handlebars control operational parameters of each of said propulsion units;a pair of nozzles, each of said nozzles being movably coupled to said body, each of said nozzles having an inlet and an outlet;said body having a first lateral side and a second lateral side; anda pair of first motors, each of said first motors being coupled to an associated one of said nozzles, each of said first motors selectively rotating said associated nozzle about an axis extending through said first lateral side and said second lateral side of said body having said outlet corresponding to said associated nozzle being directed in a selected direction such that each of said first motors facilitates forward and rearward directional control of said vehicle. 11. The assembly according to claim 10, wherein: said body has a top side and a bottom side;each of said first motors selectively rotates said associated nozzle about an axis extending through said top side and said bottom side of said body having said outlet corresponding to said associated nozzle being directed in a selected direction such that each of said first motors facilitates lateral directional control of said vehicle. 12. A hovercraft assembly comprising: a vehicle being configured to be driven, said vehicle including a body, said body having a front end, a back end, a first lateral side, a second lateral side, a top side and a bottom side, said vehicle including a seat being positioned on said top side of said body wherein said seat is configured to support a user, said vehicle including a pair of handlebars being coupled to said top side wherein said pair of handlebars is configured to be gripped, said handlebars being positioned between said seat and said front end;a pair of propulsion units, each of said propulsion units being coupled to said vehicle, each of said propulsion units being configured to urge air outwardly from said body thereby facilitating said vehicle to levitate with respect to support surface, each of said propulsion units being configured to direct the air in a selected direction with respect to said body thereby facilitating said propulsion units to urge said vehicle along the support surface in a selected direction, each of said propulsion units being operationally coupled to said handlebars such that said handlebars control operational parameters of each of said propulsion units, each of said propulsion units comprising: a jet engine having an intake and an exhaust, said jet engine being positioned within said body such that intake extends through said front end wherein said intake is configured to draw air inwardly into said jet engine thereby facilitating said jet engine to urge the air outwardly through said exhaust,a pair of nozzles, each of said nozzles being movably coupled to said body, each of said nozzles having an inlet and an outlet,a pair of first motors, each of said first motors being coupled to an associated one of said nozzles, each of said first motors selectively rotating said associated nozzle about an axis extending through said first lateral side and said second lateral side of said body having said outlet corresponding to said associated nozzle being directed in a selected direction such that each of said first motors facilitates forward and rearward directional control of said vehicle, each of said first motors selectively rotating said associated nozzle about an axis extending through said top side and said bottom side of said body having said outlet corresponding to said associated nozzle being directed in a selected direction such that each of said first motors facilitates lateral directional control of said vehicle,a conduit being fluidly coupled between said jet engine and each of said nozzles wherein each of said nozzles is configured to have the air urged outwardly through said outlet thereby facilitating each of said nozzles to produce thrust,a pair of dampers, each of said dampers being hingedly coupled to said conduit, each of said dampers being positioned within said conduit and being aligned with said inlet corresponding to an associated one of said nozzles, each of said dampers being selectively positioned between a closed position and an open position wherein each of said dampers is configured to regulate a flow of air being urged into said associated nozzle,a pair of second motors, each of said second motors being coupled to an associated one of said dampers such that each of said second motors positions said associated damper at a selected point between said open position and said closed position,said pair of propulsion units including a first propulsion unit and a second propulsion unit, said nozzles corresponding to said first propulsion unit being spaced apart from each other and being distributed on said first lateral side of said body, said nozzles corresponding to said second propulsion unit being spaced apart from each other and being distributed on said second lateral side of said body, each of said nozzles corresponding to said first propulsion unit and said second propulsion unit being positioned adjacent to said bottom side of said body;a processor being coupled to said body, said processor being electrically coupled to said handlebars, said processor being electrically coupled each of said first motors, each of said second motors and said jet engine corresponding to each of said propulsion units;a fuel tank being coupled to said body wherein said fuel tank is configured to contain a liquid fuel, said fuel tank being fluidly coupled to said jet engine wherein said jet engine is configured to receive the liquid fuel from said fuel tank; anda power supply being coupled to said body, said power supply being electrically coupled to said processor, said power supply comprising at least one battery.
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