Miniature, unmanned aircraft with interchangeable data module
First Claim
1. A powered, miniature, unmanned aircraft, comprising:
- a) an elongated airframe including a reciprocating piston internal combustion engine, a fuselage having an upper surface and a lower surface comprising a stepped, cutaway region along a longitudinal portion thereof, said stepped, cutaway region of said lower surface being adapted to receive an interchangeable data module;
b) a unitary, fixed wing removably attachable to said upper surface of said fuselage at a substantially right angle thereto;
c) a data module removably attachable to said fuselage at said stepped, cutaway region, a front end of said data module substantially abutting said fuselage at said step, a lower surface of said data module thereby forming an aerodynamically contiguous extension of a portion of said lower surface of said fuselage located forward of said step when said data module is attached to said fuselage;
d) at least one control surface disposed on at least one of said wing and said fuselage, each of said at least one control surface comprising a servomechanism operably connected thereto;
e) a remotely controlled guidance system having a radio frequency receiver carried aboard said airframe and operatively connected to at least said at least one control surface by means of said associated servomechanism associated therewith;
said powered, miniature, unmanned aircraft weighing no more than fifty-five pounds with said data module attached thereto.
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Accused Products
Abstract
A miniature, unmanned aircraft having interchangeable data handling modules, such as sensors for obtaining digital aerial imagery and other data, and radio transmitters and receivers for relaying data. The aircraft has a microprocessor for managing flight, remote control guidance system, and electrical supply system. The data handling modules have an aerodynamic housing and manual fasteners enabling ready installation and removal. One or more data acquiring sensors or data transferring apparatus and support equipment such as batteries and communications and power cables are contained within the module. A plurality of different modules are preferably provided. Each module, when attached in a preferred location below the wing, does not significantly alter the center of gravity of the airframe. Preferably, each module contains the supervisory microprocessor so that the microprocessor need not be part of the airframe.
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Citations
11 Claims
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1. A powered, miniature, unmanned aircraft, comprising:
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a) an elongated airframe including a reciprocating piston internal combustion engine, a fuselage having an upper surface and a lower surface comprising a stepped, cutaway region along a longitudinal portion thereof, said stepped, cutaway region of said lower surface being adapted to receive an interchangeable data module;
b) a unitary, fixed wing removably attachable to said upper surface of said fuselage at a substantially right angle thereto;
c) a data module removably attachable to said fuselage at said stepped, cutaway region, a front end of said data module substantially abutting said fuselage at said step, a lower surface of said data module thereby forming an aerodynamically contiguous extension of a portion of said lower surface of said fuselage located forward of said step when said data module is attached to said fuselage;
d) at least one control surface disposed on at least one of said wing and said fuselage, each of said at least one control surface comprising a servomechanism operably connected thereto;
e) a remotely controlled guidance system having a radio frequency receiver carried aboard said airframe and operatively connected to at least said at least one control surface by means of said associated servomechanism associated therewith;
said powered, miniature, unmanned aircraft weighing no more than fifty-five pounds with said data module attached thereto. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11)
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Specification