Delta M-Wing Unmanned Aerial Vehicle
First Claim
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1. A M-wing aerial vehicle comprising of:
- a) An Unmanned Aerial Systemi) An M-wing structure wherein dihedral members are placed an upward angling from 1°
to 40° and
wing tip members are placed at a downward angling from −
1°
to −
90°
ii) A delta wing structure wherein the members are offset in the negative direction are from −
1°
to −
60°
iii) A vehicle embodying a variable incidence tailiv) A propeller driven aircrafta) A vehicle embodying a vertical propeller systemb) A vehicle embodying a horizontal propeller systemc) A propeller propulsion system combining vertical and horizontal propulsionv) Retractable landing geara) Retractable landing gear stowed into the wingsb) Retractable landing gear stowed into the fuselagec) Landing gear using latching capabilitiesvi) A vehicle comprising of control avionic and vehicle control system sensor additionsvii) A vehicle composed of a composite framea) A vehicle wherein the structure comprised of a foam coreb) A vehicle wherein the frame binding sites include composite additions
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Abstract
An aerial vehicle compromising of a streamline delta wing structure, an M-wing structure accomplished through dihedral and dropped wing tips, and a variable incidence tail. The structure of the vehicle produces high lift and drag while maintaining stability and control at high angles of attack.
45 Citations
1 Claim
-
1. A M-wing aerial vehicle comprising of:
a) An Unmanned Aerial System i) An M-wing structure wherein dihedral members are placed an upward angling from 1°
to 40° and
wing tip members are placed at a downward angling from −
1°
to −
90°ii) A delta wing structure wherein the members are offset in the negative direction are from −
1°
to −
60°iii) A vehicle embodying a variable incidence tail iv) A propeller driven aircraft a) A vehicle embodying a vertical propeller system b) A vehicle embodying a horizontal propeller system c) A propeller propulsion system combining vertical and horizontal propulsion v) Retractable landing gear a) Retractable landing gear stowed into the wings b) Retractable landing gear stowed into the fuselage c) Landing gear using latching capabilities vi) A vehicle comprising of control avionic and vehicle control system sensor additions vii) A vehicle composed of a composite frame a) A vehicle wherein the structure comprised of a foam core b) A vehicle wherein the frame binding sites include composite additions
Specification
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Current AssigneeDillon Mehul Patel
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Original AssigneeDillon Mehul Patel
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InventorsPatel, Dillon Mehul
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Application NumberUS14/046,927Publication NumberTime in Patent OfficeDaysField of SearchUS Class Current1/1CPC Class CodesB64C 39/024 of the remote controlled ve...B64U 10/25 Fixed-wing aircraft VTOL ai...B64U 30/10 WingsB64U 70/80 Vertical take-off or landin...
