ENCLOSED DRONE APPARATUS AND METHOD FOR USE THEREOF
An unmanned aerial vehicle apparatus ( 100 ) that includes an air vehicle assembly ( 150 ) that is at least partially enclosed within a protective enclosure assembly ( 120 ) The protective enclosure assembly ( 120 ) is typically at least partially elastic, to protect the air vehicle assembly ( 150 ) from bumps, collisions, and other similar occurrences. The enclosure assembly ( 120 ) can also facilitate the ability of the apparatus ( 100 ) to operate in a ground movement mode ( 114 ), such as a rolling mode ( 116 ), in addition to a flying mode ( 112 ).
1 . A drone apparatus ( 100 ), comprising:
an enclosure assembly ( 120 ); and
an air vehicle assembly ( 150 ) securely positioned within said enclosure assembly ( 120 );
wherein said drone apparatus ( 100 ) provides for operating in a plurality of modes ( 110 ), said plurality of modes ( 110 ) including a flight mode ( 112 ) and ground mode ( 114 ).
2 . The drone apparatus ( 100 ) of claim 1 , wherein said ground mode ( 114 ) is a rolling mode ( 116 ).
3 . The drone apparatus ( 100 ) of claim, said drone apparatus further comprising a processor ( 176 ) that provides for receiving an instruction ( 178 ) from a remote control unit ( 99 ).
4 . The drone apparatus ( 100 ) of claim 1 , wherein said enclosure assembly ( 120 ) includes:
a plurality of enclosure members ( 130 ); and
a plurality of enclosure openings ( 136 );
wherein said enclosure assembly ( 120 ) is a substantially spherical enclosure assembly ( 123 ).
5 . The drone apparatus ( 100 ) of claim 2 , wherein said plurality of enclosure members ( 130 ) includes a plurality of horizontal enclosure members ( 134 ) and a plurality of vertical enclosure members ( 132 ), and wherein said plurality of enclosure openings ( 136 ) are filled by a plurality of air-permeable mesh surfaces ( 138 ).
6 . The drone apparatus ( 100 ) of claim 1 , wherein said ground mode ( 114 ) is a rolling mode ( 116 ).
7 . The drone apparatus ( 100 ) of claim 1 , wherein said air vehicle assembly ( 150 ) is a quad-copter air vehicle ( 160 ).
8 . The drone apparatus ( 100 ) of claim 1 , wherein said air vehicle assembly ( 150 ) includes a plurality of propellers ( 162 ) located within the same horizontal plane.
9 . The drone apparatus ( 100 ) of claim 1 , wherein said air vehicle assembly ( 150 ) includes a plurality of propellers ( 162 ) and a frame ( 170 ), wherein said propellers ( 162 ) are attached to said frame ( 170 ), and wherein a plurality of connectors ( 178 ) connect said frame ( 170 ) to said enclosure assembly ( 120 ).
10 . The drone apparatus ( 100 ) of claim 1 , wherein said air vehicle assembly ( 150 ) includes:
a frame ( 170 ), said frame comprising a plurality of frame members ( 174 );
a plurality of propellers ( 162 ) positioned on said plurality of frame members ( 174 );
a base ( 173 ) positioned one or more said frame members ( 174 );
wherein said plurality of propellers ( 162 ) are each positioned facing upwards from said plurality of frame members ( 174 ) when said apparatus ( 100 ) is positioned on a bottom ( 102 ) of said apparatus ( 100 ).
11 . The drone apparatus ( 100 ) of claim 11 , wherein said at least one said propeller ( 162 ) directs air upwards and at least one said propeller ( 162 ) directs air downwards when said drone apparatus ( 100 ) is a ground operating mode ( 114 ).
12 . The drone apparatus ( 100 ) of claim 11 , said drone apparatus ( 100 ) further comprising an inertial measurement system ( 182 ), a camera ( 185 ), an antenna ( 188 ), and a GPS device ( 190 ).
13 . A drone apparatus ( 100 ), comprising:
an enclosure assembly ( 120 ), wherein said enclosure assembly is a substantially spherical enclosure assembly ( 123 ) that includes a plurality of surfaces ( 135 ) and a plurality of openings ( 136 );
an air vehicle assembly ( 150 ), said air vehicle assembly ( 150 ) including a frame ( 170 ) securely attached to the interior of said enclosure assembly ( 120 ), said air vehicle assembly ( 150 ) further including a plurality of propellers ( 162 ) and a plurality of motors ( 164 ) securely positioned on said frame ( 170 );
wherein said drone apparatus ( 100 ) provides for operating in a plurality of operating modes ( 110 ), said plurality of modes including a flying mode ( 112 ) and a rolling mode ( 116 ).
14 . The drone apparatus ( 100 ) of claim 13 , wherein said plurality of surfaces ( 135 ) in said substantially spherical enclosure assembly ( 123 ) is comprised of substantially elastic material, wherein said air vehicle assembly ( 150 ) includes at least four propellers ( 162 ) positioned within the same horizontal plane and facing the same direction.
15 . A method for operating a drone apparatus ( 100 ) that that provides for operating in plurality of modes ( 110 ) that includes a ground mode ( 114 ), wherein said drone apparatus ( 100 ) includes a plurality of propellers ( 162 ), said method comprising:
selectively reversing air flow direction for at least one said propeller ( 162 ) when said drone apparatus ( 100 ) is in a ground mode ( 114 ).
16 . The method for operating a drone apparatus ( 100 ) of claim 15 , wherein said ground mode ( 114 ) provides for rolling said drone apparatus ( 100 ) on an exterior surface.
17 . The method for operating a drone apparatus ( 100 ) of claim 15 , wherein said drone apparatus ( 100 ) includes at least four said propellers ( 162 ), said method comprising selectively reversing said air flow direction for at least two said propellers ( 162 ) when said drone apparatus ( 100 ) is in a ground mode ( 114 ).
18 . The method for operating a drone apparatus ( 100 ) of claim 15 , said method further comprising:
receiving an instruction ( 178 ) from a remote control unit ( 99 ); and
changing said operation mode ( 110 ) in accordance with said instruction ( 178 ).
19 . The method for operating a drone apparatus ( 100 ) of claim 15 , said method further comprising:
changing from a flying operating mode ( 112 ) to a rolling operating mode ( 116 ) by reversing the airflow of at least one propeller ( 162 ).
20 . The method for operating a drone apparatus ( 100 ) of claim 15 , wherein said drone apparatus ( 100 ) includes an air vehicle assembly ( 160 ) that includes at least four propellers ( 162 ), and wherein the airflow for more than one adjacent propellers ( 160 ) are reversed to change into a rolling operating mode ( 116 ).