Unmanned aerial vehicle

An unmanned aerial vehicle, comprising:

• a fuselage defining a fuselage chamber;
• a first boom extending between a proximal end and a distal end;
• said proximal end of said first boom coupled to said fuselage;
• a first rotor lift assembly coupled to said distal end of said first boom for providing a first lifting force;
• a second boom extending between a proximal end and a distal end;
• said proximal end of said second boom coupled to said fuselage;
• a second rotor lift assembly coupled to said distal end of said second boom for providing a second lifting force;
• a third boom extending between a proximal end and a distal end;
• said proximal end of said third boom coupled to said fuselage;
• a third rotor lift assembly coupled to said distal end of said third boom for providing a third lifting force;
• a fourth boom extending between a proximal end and a distal end;
• said proximal end of said fourth boom coupled to said fuselage;
• a fourth rotor lift assembly coupled to said distal end of said fourth boom for providing a fourth lifting force;
• said first rotor lift including a first motor and a first propeller;
• a first propeller connector removeably coupling said first propeller to said first motor;
• said first propeller connector including a first keyed post coupled to said first motor and a first keyed receiver coupled to said first propeller;
• a first actuator slidably coupled to said first keyed receiver and abutting said first keyed post for maintaining said first keyed post engaged within said first keyed receiver and said first actuator depressed for distancing said first actuator from said first keyed post for releasing said first keyed post from said first keyed receiver;
• said second rotor lift including a second motor and a second propeller;
• a second propeller connector removeably coupling said second propeller to said second motor;
• said second propeller connector including a second keyed post coupled to said second motor and a second keyed receiver coupled to said second propeller;
• a second actuator slidably coupled to said second keyed receiver and abutting said second keyed post for maintaining said second keyed post engaged within said second keyed receiver and said second actuator depressed for distancing said second actuator from said second keyed post for releasing said second keyed post from said second keyed receiver,
• said third rotor lift including a third motor and a third propeller;
• a third propeller connector removeably coupling said third propeller to said third motor;
• said third propeller connector including a third keyed post coupled to said third motor and a third keyed receiver coupled to said third propeller;
• a third actuator slidably coupled to said third keyed receiver and abutting said third keyed post for maintaining said third keyed post engaged within said third keyed receiver and said third actuator depressed for distancing said third actuator from said third keyed post for releasing said third keyed post from said third keyed receiver;
• said fourth rotor lift including a fourth motor and a fourth propeller;
• a fourth propeller connector removeably coupling said fourth propeller to fourth first motor;
• said fourth propeller connector including a fourth keyed post coupled to said fourth motor and a fourth keyed receiver coupled to fourth first propeller;
• and
• a fourth actuator slidably coupled to said fourth keyed receiver and abutting said fourth keyed post for maintaining said fourth keyed post engaged within said fourth keyed receiver and said fourth actuator depressed for distancing said fourth actuator from said fourth keyed post for releasing said fourth keyed post from said fourth keyed receiver.