Abstract: Disclosed is a turbine engine including a housing defining an interior cavity. A shaft extends axially through the housing and a turbine rotor coupled to the shaft. The turbine rotor includes a hub configured to couple to the shaft. A plurality of spokes extend radially outward from the hub. A plurality of blades is included, and each blade is disposed at a distal end of a corresponding spoke of the plurality of spokes and shaped as a hollow spherical shell having an opening. The opening is oriented to receive a working fluid and direct the working fluid tangentially to impart rotational motion to the turbine rotor. An inlet is coupled to the housing and configured to direct the working fluid into the interior cavity. An exhaust pipe is coupled to the housing and configured to discharge residual gases from the housing.

Abstract: An aircraft includes a fuselage having a top surface opposite a bottom surface, a front section, a center section, and a rear section. A first mounting rod and a second mounting rod are coupled to the top surface. The first mounting rod and the second mounting rod are single rods. A first and a second wing are coupled to the center section. A plurality of power generator systems are coupled to the first mounting rod or the second mounting rod. Each power generator system includes a power source, a first propeller and a second propeller. The power source is configured to drive the first propeller and the second propeller. The first propeller and the second propeller have an axis of rotation, and are pivotable between a first position and a second position. A shroud encloses the power generator system.

Abstract: Disclosed is a system including a turbine having a plurality of blades being spaced circumferentially around a shaft. A plurality of dispensers is included. Each dispenser of the plurality of dispensers is positioned facing the open surface of the plurality of blades and directs discharged fluid toward the open surface of the plurality of blades to drive the turbine. A housing encloses the plurality of blades and a portion of each dispenser. A plurality of exhaust pipes is coupled to the housing and extends away from the shaft directing the discharged fluid out of the housing. Each exhaust pipe corresponds to a respective dispenser of the plurality of dispensers. A controller is in communication with the plurality of dispensers and is configured to control the plurality of dispensers.

Abstract: Disclosed is a system including a turbine having a plurality of blades being spaced circumferentially around a shaft. A plurality of dispensers is included. Each dispenser of the plurality of dispensers is positioned facing the open surface of the plurality of blades and directs discharged fluid toward the open surface of the plurality of blades to drive the turbine. A housing encloses the plurality of blades and a portion of each dispenser. A plurality of exhaust pipes is coupled to the housing and extends away from the shaft directing the discharged fluid out of the housing. Each exhaust pipe corresponds to a respective dispenser of the plurality of dispensers. A controller is in communication with the plurality of dispensers and is configured to control the plurality of dispensers.

Abstract: An aircraft includes a fuselage having a top surface opposite a bottom surface, a front section, a center section, and a rear section. A first mounting rod and a second mounting rod are coupled to the top surface. The first mounting rod and the second mounting rod are single rods. A first and a second wing are coupled to the center section. A plurality of power generator systems are coupled to the first mounting rod or the second mounting rod. Each power generator system includes a power source, a first propeller and a second propeller. The power source is configured to drive the first propeller and the second propeller. The first propeller and the second propeller have an axis of rotation, and are pivotable between a first position and a second position. A shroud encloses the power generator system.

Abstract: A drone includes a frame and a fuselage. The fuselage is coupled to the frame extending away from the frame. The fuselage has a front panel and a bottom panel, and the front panel is positioned at an angle between the bottom surface of the frame and the bottom panel of the fuselage. A first wing is opposite a second wing and are coupled to the frame. The first and second wings extend outwardly from opposite sides of the frame. A first and second mounting member are coupled to the frame and extend outwardly from opposite sides of the frame. A plurality of power generator systems are included and each system is coupled to the first or second mounting member. Each power generator system comprises a power source coupled to a propeller.

Abstract: An aircraft includes a fuselage having a front, a center, and a rear section. A first mounting member is coupled to the front section. A second mounting member is coupled to the rear section. A first and a second wing are coupled to the center section. A plurality of power generator systems are included and coupled to the first or second mounting member. Each power generator system includes a power source, a first and a second propeller. The power source is configured to drive the first and second propeller. The first and second propeller have an axis of rotation, and are pivotable between a first and a second position. An amphibious landing gear system is coupled to an underside of the fuselage and has a flap and a bladder. The bladder is located under the flap, configured to inflate and deflate, and sized to provide buoyancy for the aircraft.

Abstract: A drone includes a frame and a fuselage. The fuselage is coupled to the frame extending away from the frame. The fuselage has a front panel and a bottom panel, and the front panel is positioned at an angle between the bottom surface of the frame and the bottom panel of the fuselage. A first wing is opposite a second wing and are coupled to the frame. The first and second wings extend outwardly from opposite sides of the frame. A first and second mounting member are coupled to the frame and extend outwardly from opposite sides of the frame. A plurality of power generator systems are included and each system is coupled to the first or second mounting member. Each power generator system comprises a power source coupled to a propeller.

Abstract: Disclosed is a system including a turbine having a plurality of blades being spaced circumferentially around a shaft. Each blade of the plurality of blades is a hemispherical-shaped cup with an open surface. A plurality of dispensers are included, and each dispenser of the plurality of dispensers is positioned facing the open surface of the each blade, and directs discharged fluid toward the open surface of the each blade to drive the turbine. A housing encloses the plurality of blades and a portion of each dispenser of the plurality of dispensers, and has an exhaust pipe extending away from the shaft directing the discharged fluid out of the housing. A controller is in communication with the plurality of dispensers, and controls the plurality of dispensers.

Abstract: Disclosed is a system including a turbine having a plurality of spokes. The first spoke end is coupled to a shaft and the second spoke end is coupled to a blade of a plurality of blades. Each blade is a cup with an open surface. A dispenser includes a combustion chamber. An air injector is configured to inject air into the combustion chamber. A fuel injector is configured to inject fuel into the combustion chamber. An ignitor is configured to supply a spark for combustion in the combustion chamber. A nozzle directs discharged fluid toward the open surface of the blade to drive the turbine. A housing encloses the second nozzle end and the plurality of blades, and has an exhaust pipe. A controller is configured to control the air injector, the fuel injector and the ignitor.

Abstract: Disclosed herein is an aquatic vehicle torpedo launch system comprising of an aquatic vehicle. A torpedo launch system is coupled to the aquatic vehicle. The torpedo launch system is operable in a neutral buoyance position. A plurality of torpedoes is included. Each torpedo is coupled to the torpedo launch system with a locking means. Power cables are coupled to each torpedo providing power to the plurality of torpedoes. Fiber optic cables are coupled to each torpedo enabling programming of the plurality of torpedoes. The locking means, the power cables and the fiber optic cables are disengaged from the plurality of torpedoes prior to launch. Each torpedo is launched by buoyancy.

Abstract: Disclosed herein is an aquatic vehicle torpedo launch system comprising of an aquatic vehicle. A torpedo launch system is coupled to the aquatic vehicle. The torpedo launch system is operable in a neutral buoyance position. A plurality of torpedoes is included. Each torpedo is coupled to the torpedo launch system with a locking means. Power cables are coupled to each torpedo providing power to the plurality of torpedoes. Fiber optic cables are coupled to each torpedo enabling programming of the plurality of torpedoes. The locking means, the power cables and the fiber optic cables are disengaged from the plurality of torpedoes prior to launch. Each torpedo is launched by buoyancy.

Abstract: Disclosed is a communication network for aquatic vessels. The network comprises an unmanned aquatic vehicle (UAQV) having a warhead. A fiber optic cable is bi-directional and in a closed ring configuration enabling communication within the network and to the UAQV. A power grid cable is in a closed ring configuration and coupled to a generator providing power. A node is coupled to the fiber optic cable and to the power grid cable. A relay station is coupled to the node and in communication with the UAQV. A control center is in communication with the UAQV and facilitates remote control of the UAQV, and programming of a navigational plan for the remote control of the UAQV prior to launch. The fiber optic cable, power grid cable, node and relay station are capable of being located underwater during operation. The UAQV is capable of being launched underwater from open water.

Abstract: Disclosed is a communication network for aquatic vessels. The network comprises an unmanned aquatic vehicle (UAQV) having a warhead. A fiber optic cable is bi-directional and in a closed ring configuration enabling communication within the network and to the UAQV. A power grid cable is in a closed ring configuration and coupled to a generator providing power. A node is coupled to the fiber optic cable and to the power grid cable. A relay station is coupled to the node and in communication with the UAQV. A control center is in communication with the UAQV and facilitates remote control of the UAQV, and programming of a navigational plan for the remote control of the UAQV prior to launch. The fiber optic cable, power grid cable, node and relay station are capable of being located underwater during operation. The UAQV is capable of being launched underwater from open water.

Abstract: Disclosed is a communication network for aquatic vessels. The network comprises an unmanned aquatic vehicle (UAQV) having a warhead. A fiber optic cable is bi-directional and in a closed ring configuration enabling communication within the network and to the UAQV. A power grid cable is in a closed ring configuration and coupled to a generator providing power. A node is coupled to the fiber optic cable and to the power grid cable. A relay station is coupled to the node and in communication with the UAQV. A control center is in communication with the UAQV and facilitates remote control of the UAQV, and programming of a navigational plan for the remote control of the UAQV prior to launch. The fiber optic cable, power grid cable, node and relay station are capable of being located underwater during operation. The UAQV is capable of being launched underwater from open water.

Abstract: Various aspects can be implemented to provide a reconfigurable underwater vehicle. In general, one aspect of the subject matter described in this specification can be embodied in a underwater vehicle that includes a hull that is angular in shape and capable of avoiding sonar detection. The hull can include a bow and a stern that are substantially similar in shape. The underwater vehicle can also include a plurality of reconfigurable modules that are interconnected to form the hull of the underwater vehicle. Each reconfigurable module is capable of performing a different function associated with operation of the underwater vehicle. Further, the plurality of reconfigurable modules can be built in a warehouse away from a shipyard and assembled to form the underwater vehicle at the shipyard.

Abstract: A method of operation and electronic apparatus named Mobile Safety Communication (MSC) for recording the driving data, wireless communication for voice/video/data, anti-theft device, and a GPS (Global Positioning System) unit embedded into a rearview/side mirror or stand-alone unit which is mounted onto the windshield of a vehicle. The MSC measures the vehicle various motions include acceleration, de-acceleration, up/down vibration, and flipped-over condition. A method of operation related to the acceleration/de-acceleration sensor/gauge that identifies the significant instances to the central control of MSC for coordinating the Flash memory storage, digital camera shots and alarm activation; the control or recording of the data is capable of being interfaced or networked to other digital devices such as computers or other peripherals.

Abstract: The present invention relates to a converter/bridge between an Ethernet bus and a UTOPIA bus in single or multiple channels. The converter/bridge includes a first conversion device and a second conversion device for converting Ethernet packet into ATM cells and for converting ATM cells into Ethernet packet. The first conversion device includes a first conversion unit, a combining unit and a first transmitting unit. And the second conversion device includes a receiving unit, a second conversion unit and a second transmitting unit. The present invention provides a low cost and efficient transport between the Ethernet and ATM networks.

Abstract: Received Ethernet MII packets are converted to T1/E1 HDSL frames and received T1/E1 HDSL frames are converted into Ethernet MII packets. When Ethernet MII format 4 bit data packets are received they are converted into 8 bit data packets, each 8 bit data packet having an associated signal bit. For T1, a series of twenty-one 8 bit data packets and associated signal bit are combined with three pass bits into a 192 bit T1 HDSL frame. The series of twenty-one multiple 8 bit packets and associated signal bit with three pass bits are transmitted in HDSL format.When T1 HDSL frames having a series of twenty-one 9 bit packets, each 9 bit packet including 8 data bits with an associated signal bit, and three pass bits, are received, the series of twenty-one 9 bit packets and three pass bits are converted into twenty-one groups of 9 bit packets, each 9 bit packet including an 8 bit data packet with an associated signal bit.