Ducted vehicles particularly useful as VTOL aircraft
First Claim
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1. A vehicle movable in a fluid medium, comprising:
- a vehicle body;
a first group of rotary propeller propulsion units mounted on one side of the vehicle body, each of said rotary propulsion units being oriented to produce a downward flow of the fluid and thereby an upward lift force applied to that side of the vehicle body;
a second group of rotary propeller propulsion units mounted on the opposite side of the vehicle body, each of said latter rotary propeller propulsion units being oriented to produce a downward flow of the fluid, and thereby an upward lift force applied to said opposite side of the vehicle body;
a first elongated duct on said one side of the vehicle body enclosing all the rotary propeller propulsion units of said first group and having an upper end and a lower end projecting past the upper and lower ends of said enclosed rotary propeller propulsion units;
and a second elongated duct, separate from said first elongated duct, located on said opposite side of the vehicle body and enclosing all the rotary propeller propulsion units of said second group, said second elongated duct having an upper end and a lower end projecting past the upper and lower ends of said second group of rotary propeller propulsion units;
the cross-sectional area of each of said first and second elongated ducts being larger than the sum of the cross-sectional areas of the plurality of rotary propeller propulsion units enclosed by the respective elongated duct, to augment the lift force produced by the respective rotary propeller propulsion units;
the ends of said first and second elongated ducts being spaced from each other to facilitate entry and exit from said vehicle.
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Abstract
A VTOL aircraft (or other vehicle such as a sea vehicle) includes a pair of elongated ducts on opposite sides of the vehicle body, and a plurality of powered propellers (or other propulsion units such as jet engines) mounted within and enclosed by each of the elongated ducts, such as to produce an upward lift force to the vehicle. Each of the elongated ducts has a short transverse dimension slightly larger than the diameter of the blades of each propeller enclosed thereby, and a large transverse dimension slightly larger than the sum of the diameters of the blades of all the propellers enclosed thereby.
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Citations
18 Claims
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1. A vehicle movable in a fluid medium, comprising:
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a vehicle body;
a first group of rotary propeller propulsion units mounted on one side of the vehicle body, each of said rotary propulsion units being oriented to produce a downward flow of the fluid and thereby an upward lift force applied to that side of the vehicle body;
a second group of rotary propeller propulsion units mounted on the opposite side of the vehicle body, each of said latter rotary propeller propulsion units being oriented to produce a downward flow of the fluid, and thereby an upward lift force applied to said opposite side of the vehicle body;
a first elongated duct on said one side of the vehicle body enclosing all the rotary propeller propulsion units of said first group and having an upper end and a lower end projecting past the upper and lower ends of said enclosed rotary propeller propulsion units;
and a second elongated duct, separate from said first elongated duct, located on said opposite side of the vehicle body and enclosing all the rotary propeller propulsion units of said second group, said second elongated duct having an upper end and a lower end projecting past the upper and lower ends of said second group of rotary propeller propulsion units;
the cross-sectional area of each of said first and second elongated ducts being larger than the sum of the cross-sectional areas of the plurality of rotary propeller propulsion units enclosed by the respective elongated duct, to augment the lift force produced by the respective rotary propeller propulsion units;
the ends of said first and second elongated ducts being spaced from each other to facilitate entry and exit from said vehicle. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9)
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10. A VTOL aircraft vehicle, comprising:
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a vehicle body;
a first group of rotary propeller propulsion units mounted on one side of the vehicle body, each of said propulsion units being oriented to produce a downward flow of the air and thereby an upward lift force applied to that side of the vehicle body;
a second group of rotary propeller propulsion units mounted on the opposite side of the vehicle body, each of said latter propulsion units being oriented to produce a downward flow of the air, and thereby an upward lift force applied to said opposite side of the vehicle body;
a first elongated duct on said one side of the vehicle body enclosing all the rotary propeller propulsion units of said first group and having an upper end and a lower end projecting past the upper and lower ends of said enclosed propulsion units;
and a second elongated duct, separate from said first elongated duct, located on said opposite side of the vehicle body and enclosing all the rotary propeller propulsion units of said second group, said second elongated duct having an upper end and a lower end projecting past the upper and lower ends of said second group of propulsion units;
the cross-sectional area of each of said first and second elongated ducts being larger than the sum of the cross-sectional areas of the plurality of rotary propeller propulsion units enclosed by the respective elongated duct, to augment the lift force produced by the respective propulsion units;
the ends of said first and second elongated ducts being spaced from each other to facilitate entry and exit from said vehicle. - View Dependent Claims (11, 12, 13, 14, 15, 16, 17, 18)
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Specification