摘要:
Described embodiments include a system, method, and apparatus. The system includes a sensor device configured to measure an unburned fuel component in an exhaust stream from a gas-fueled combustion device. The system includes a feedback controller configured to generate a combustion management signal responsive to the measured unburned fuel component and to a target value for the measured unburned fuel component. The system includes a combustion controller configured to regulate an aspect of a combustion component delivered to a burner of the gas-fueled combustion device in response to the combustion management signal. In an embodiment, the system includes a user interface configured to display a quality of combustion information responsive to the measured unburned fuel component in a human perceivable format.
摘要:
A system and method for repowering an unmanned aircraft system is disclosed. The system and method may comprise use of a utility transmission system configured to function as power system/source for UAV/aircraft and UAV/aircraft configured to interface with the power source/system. Systems and methods provide access and for administrating, managing, and monitoring access and interfacing by UAV/aircraft with the power system/source. UAV/aircraft system can be configured and operated/managed to interface with and use the power system/source (e.g. network of power lines from a utility transmission system) to enhance range and utility (e.g. for repowering and/or as a flyway or route). The system comprises an interface between the aircraft and the power source for power transfer; a monitoring system to monitor the aircraft; and an administrative/management system to manage interaction/transaction with the aircraft. The power source for power transfer may be a power line; power transfer to the aircraft may be by wireless power transfer (capacitive or inductive or optical) of an aircraft while at or operating along the power line. The aircraft may comprise a connector configured to interface with the power source/line; the power line may be configured to interface with the connector/aircraft. Data communications between the aircraft and system may be facilitated for interaction/transaction.
摘要:
A system and method for management of airspace for unmanned aircraft is disclosed. The system and method comprises administration of the airspace including designation of flyways and zones with reference to features in the region. The system and method comprises administration of aircraft including registration of aircraft and mission. A monitoring system tracks conditions and aircraft traffic in the airspace. Aircraft may be configured to transact with the management system including to obtain rights/priority by license and to operate in the airspace under direction of the system. The system and aircraft may be configured for dynamic transactions (e.g. licensing/routing). The system will set rates for licenses and use/access to the airspace and aircraft will be billed/pay for use/access of the airspace at rates using data from data sources.
摘要:
A nanoelectromechanical device is provided. The nanoelectromechanical device includes a nanotube, a first contact, and a first actuator. The nanotube includes a first end, the first end supported by a first structure, a second end opposite the first end, and a first portion. The first actuator is configured to apply a first force to the nanotube, the first force causing the nanotube to buckle such that the first portion couples to the first contact.
摘要:
Described embodiments include a system, method, and apparatus. The system includes a sensor device configured to measure an unburned fuel component in an exhaust stream generated by a gas-fueled combustion device. The system includes a combustion analysis circuit configured to generate a quality of combustion information responsive to the measured unburned fuel component. The system includes a user interface configured to display the quality of combustion information in a human perceivable format. In an embodiment, the system includes a combustion component controller configured to regulate an aspect of a combustion component delivered to the gas-fueled combustion device in response to the combustion management selection entered by a human user.
摘要:
A reconfigurable unmanned aircraft system is disclosed. A system and method for configuring a reconfigurable unmanned aircraft and system and method for operation and management of a reconfigurable unmanned aircraft in an airspace are also disclosed. The aircraft is selectively reconfigurable to modify flight characteristics. The aircraft comprises a set of rotors. The position of at least one rotor relative to the base can be modified by at least one of translation of the rotor relative to the boom, pivoting of the boom relative to the base, and translation of the boom relative to the base; so that flight characteristics can be modified by configuration of position of at least one rotor relative to the base. A method of configuring an aircraft having a set of rotors on a mission to carry a payload comprises the steps of determining properties of the payload including at least mass properties, determining the manner in which the payload will be coupled to the aircraft, determining configuration for each of the rotors in the set of rotors at least partially in consideration of the properties of the payload, and positioning the set of rotors in the configuration for the aircraft to perform the mission.
摘要:
A system and method for management of airspace for unmanned aircraft is disclosed. The system and method comprises administration of the airspace including designation of flyways and zones with reference to features in the region. The system and method comprises administration of aircraft including registration of aircraft and mission. A monitoring system tracks conditions and aircraft traffic in the airspace. Aircraft may be configured to transact with the management system including to obtain rights/priority by license and to operate in the airspace under direction of the system. The system and aircraft may be configured for dynamic transactions (e.g. licensing/routing). The system will set rates for licenses and use/access to the airspace and aircraft will be billed/pay for use/access of the airspace at rates using data from data sources.
摘要:
A system and method for management of airspace for unmanned aircraft is disclosed. The system and method comprises administration of the airspace including designation of flyways and zones with reference to features in the region. The system and method comprises administration of aircraft including registration of aircraft and mission. A monitoring system tracks conditions and aircraft traffic in the airspace. Aircraft may be configured to transact with the management system including to obtain rights/priority by license and to operate in the airspace under direction of the system. The system and aircraft may be configured for dynamic transactions (e.g. licensing/routing). The system will set rates for licenses and use/access to the airspace and aircraft will be billed/pay for use/access of the airspace at rates using data from data sources.
摘要:
Described embodiments include a system, method, and apparatus. A system includes a medicament-eluting device configured to be positioned at a location on a skin of a mammal. The system includes an ultrasonic wave transmitter configured to emit ultrasonic shear waves directable at the location. The ultrasonic shear waves have a frequency or amplitude selected to increase a permeability of the skin of the mammal to a medicament released by the medicament-eluting device. In an embodiment, the system includes a structure carrying the medicament-eluting device and the ultrasonic wave transmitter. In an embodiment, the system includes a cavitation sensor configured to detect a cavitation event in the mammal. In an embodiment, the system includes a cavitation controller configured to limit a power of the ultrasonic shear waves directed at the location to a level below a cavitation threshold of the mammal.