407 results about "Air line" patented technology

A refrigerator includes a refrigerator main body having a storage chamber, a door coupled to the refrigerator main body to be opened or closed, a cool air supplying device which generates cool air, an ice maker including an ice making tray having ice making cells to produce ice and a cool air guide member installed in the door, coupled to the ice making tray and having a cool air line that guides the cool air supplied from the cool air supplying device to flow around the ice making tray. The cool air line disposed on the cool air guide member to supply the ice making tray guides the cool air supplied from the cool air supplying device to move along the surrounding of the ice making tray, thereby uniformly cooling down the ice making tray.

The invention provides unmanned helicopter pesticide applying operation automatic control system and method based on GPS (Global Positioning System) navigation, belonging to the field of agricultural technology. The main communication end of a flight control host machine is communicated with a GPS, and the main control output end is connected with the controlled end of a rotor flight system to be used for sending a navigation control signal to the flight system according to a preset air line and real-time position information transmitted by the GPS; an unmanned helicopter is also provided with a pesticide applying device and a pesticide applying control system, wherein the pesticide applying device comprises a pesticide box, a liquid pump, a spray rod and a spray head; the pesticide applying control system comprises a main control circuit, a communication module, a feedback module, a signal processing module and a power transformation module; the main control circuit is used for feeding back the state information of the pesticide applying system to the flight control host machine by the communication module; and the signal processing module is used for amplifying a pesticide applying control signal transmitted by the main control circuit into an electric signal and controlling the liquid pump to carry out pesticide applying operation. The system and the method can control the unmanned helicopter to flight according to the preset air line by the GPS and perform a spray task according to a preset GPS air line.

A permanently mounted pneumatic jack (jacklift) system for motor vehicles, as well as an impact wrench for removing and installing lug nuts. The system provides a quick and safe means of lifting one or more tires off the ground for replacement of a spare or rotating the tires on a motor vehicle. The present invention comprises two or more (typically four) pneumatic jacks, a system ON/OFF switch, an air compressor, a 120-psi air tank, air lines (hoses), individual jack extend/retract switches, jack position-locking pins, safety-locking pins, and impact wrench. Each jack can be locked in a horizontal stowaway or vertical operational position. The jack is cylindrical shaped with a telescopic body that can be extended or retracted as needed to raise and lower the vehicle. A solid cylindrical lift rod slides inside a cylindrical outer housing with a high-pressure seal means used to maintain pressure on the support rod. A ground support foot (plate) is mounted on the lower end of the solid cylindrical lift rod to provide sufficient traction with the ground to support the lifting process. A quick release air coupler is included on the pneumatic chamber to support the use of an air hose and impact wrench. An extend/retract toggle switch is included on each jack to control a solenoid valve to allow the air to flow into the jack. A quick release safety-locking pin is used to mechanically pin the solid cylindrical lift rod to the outer housing once the desired height is achieved to assure that the vehicle does not fall down in the event of a high-pressure air loss, thereby providing safety to the person(s) working around the vehicle. An air compressor located in the engine compartment of the vehicle is mechanically belt-driven off the engine. A high-pressure air line carries the air to a high-pressure (at least 120-psi) air tank located in the trunk or other suitable storage area on the vehicle. Separate air lines extend from the air tank to the individual jacks.

Embodiments of the present disclosure are directed towards a system that includes a recirculation system. The recirculation system includes a compressor discharge air line extending from a compressor to an air intake. The compressor discharge air line is configured to flow a compressor discharge air flow, and the air intake is configured to supply an air flow to the compressor. An ejector is disposed along the compressor discharge air line between the compressor and the air intake. The ejector is configured to receive and mix the compressor discharge air flow and a turbine exhaust flow to form a first mixture.

The invention discloses a flying monitoring system of an unmanned aerial vehicle, and belongs to the field of aviation electronics or aeronautical communication. The flying monitoring system comprises an airborne terminal and a ground terminal, wherein the airborne terminal is arranged on the unmanned aerial vehicle and comprises a satellite positioning communication module, a flying control module and a first wireless communication module, and the ground terminal comprises a ground control module, a man-machine interaction module and a second wireless communication module. The system is in communication with a central control processing unit and sends position information, flying information, flying control information and air line application information to the central control processing unit. The central control processing unit obtains the air line application information and sends the air line application information to the system. The flying of the unmanned aerial vehicle is effectively monitored, the application of the air line of the unmanned aerial vehicle can be more convenient and rapid, the flying air line examination and approval and the information issuing feedback can be easier and more timely, the air line application efficiency is improved, the running and management difficulty and the running cost of the unmanned aerial vehicle are reduced, and the management efficiency and safety are improved.

An adjustable air pillow includes an internal air bladder that can be incrementally inflated and deflated so that a conformable padding with a recessed upper surface that completely encloses the air bladder can support and elevate the individual's head, neck and spine for obtaining the proper alignment thereof for rest, relaxation or sleep. The incremental inflation and deflation of the air bladder is controlled from a control box that encloses an air pump interconnected to the air bladder by a flexible air line, and the control box can be powered by batteries or by plugging the control box into a standard wall outlet for being powered by normal house current.

Accordingly, the present invention transfers a message package from one communication system to another and re-directing it to an output site that shortens the time for ‘delivery’ of a message and transforming the unique recipient contact address from one communication system to the format in another. The present invention utilizes the flexibility of SGML, XML, HTML and similar codes and manages the large volume of micro-payments in an efficient manner. The originating message can be an e-mail, a fax, a letter, a voice message, message created in a private message system (e.g. air line reservation system) or other message type. The subject invention creates a standardized intermediary platform that links together the speed and near zero cost of an email with the diversity of input and output communications devices and an optimization routine for the selection of best available physical location for the final output process.

Chemical and biological protective hood assembly. The hood assembly comprises a head cover portion; a visor; a head passthrough; and an air line passthrough.

A cleaning machine is provided, in particular a single-chamber dishwashing machine, that includes a washing chamber for accommodating items to be cleaned or washed. At least one wash arm with a number of spray nozzles is located in the washing chamber. A waste-water line into which waste water is pumped runs from the washing chamber. Exhaust air from the washing chamber is conducted into the waste-water line via an exhaust-air line, with the washing chamber being bounded by at least one wall which stores a heat-exchanger fluid or through which heat-exchanger fluid flows.

A compact air pump and valve package includes pump and valve assemblies integral with a pressure housing defining inlet ports and a plurality of fittings for connecting air lines to an interior of the pressure housing. The linear diaphragm pump assembly has a permanent magnetic shuttle mounting two diaphragms reciprocated by an electromagnet. The valve assembly has a plurality of solenoid valves disposed within the pressure housing, each solenoid valve being operable to control flow into or out of the pressure housing through an associated one of the plurality of fittings. Thus, no tubes or hoses are required to transfer air from the pump assembly to the valves. The housing has special mounts to isolate vibration arising from movement of the shuttle.

A compressed air system is provided for automotive or motorcycle use, wherein compressed air is utilized to assist clearing a windshield or a windscreen during foul weather. The system comprises an electrically driven or belt driven air compressor, a compressed air reservoir tank, a network of air lines throughout the vehicle or attached to a rider's helmet, and a plurality of air nozzles that release the air from the air lines on command. The ejected air is highly pressurized and exits at a high velocity to remove water droplets and particles for improved clarity through the windshield or wind screen. A user-operated switch controls at least one valve to release the compressed air from the network of air lines and through the nozzles, wherein the compressed air tank is continually replenished to allow for consistent and repeated bursts of compressed air over an extended period.

This invention discloses a sort of refrigeration which has three gates and an evaporation, it consists of the chest body, the evaporator, above the chest body there has the folio refrigeration chamber and the safe, below the chest body there has the poikilothermal chamber. This poikilothermal chamber has the configuration that it likes a whole big drawer or it has the big airtight space configuration of the airproof gate and it only fitted an evaporator in the safe. They use the common evaporator in the working of the refrigeration, the deepfreeze, the change of temperature. It adjusts the intake of the indoor space to reach the needed temperature by the fan, the air line and the air door; thereby it saves an evaporator which can change the temperature. Especially the poikilothermal chamber become an alone chamber, it can realize the function of the change of temperature completely and independently. The poikilothermal chamber can progress the continuous regulation from the deepfreeze to the soft refrigeration then to the refrigeration, it can realize the conversion between the deep deepfreeze and the deep refrigeration, and it satisfy the request for the user to the big and wide safe.

The invention provides an unmanned helicopter air line control device which is used on an unmanned helicopter ground control system. The device comprises an air line planning unit, an air line monitoring unit and a yaw warning unit. The air line planning unit is used for planning an optimal working air line of an unmanned helicopter according to the planned working zone and the preset working width of the unmanned helicopter. The air line monitoring unit is used for receiving the real-time flying coordinate parameters of the unmanned helicopter and generating a practical working air line of the unmanned helicopter according to the real-time flying coordinate parameters. The yaw warning unit is used for comparing the practical working air line with the optimal working air line at regular intervals, and if the practical working air line deviates from the optimal working air line, yarn warning information is sent to the unmanned helicopter. The invention further provides an unmanned helicopter air line auxiliary control device which is used on the unmanned helicopter and is used for assisting the air line control device. According to the unmanned helicopter air line control device and auxiliary control device, an operator can know about deviation of the working air line of the unmanned helicopter timely and improve the working accuracy of the unmanned helicopter through adjustment.

A check valve which is positioned in the vacuum air line of an internal combustion engine. The check valve includes a single-piece valve body having an outlet port and two or more inlet ports, with one outlet port located substantially in line with the inlet port and connected by a venturi tube. The second inlet port is separated from the main air flow line by the valve stem and a diaphragm which allows communication there between and prevents back pressure. The second inlet port communicates with the outlet port through the valve stem and a second venturi tube which provides a vacuum boost to a device, usually vehicle brakes, connected to the inlet.

An ear canal pressurization device optimized for aural acoustic immittance testing is disclosed. The preferred embodiment of the device is comprised of a rigid mounting framework which holds in position, axially aligned, a first flexible chamber assembly, a centrally disposed forcer assembly, and a second flexible chamber assembly. The forcer assembly comprises a ferromagnetic bobbin and coil that provides electromotive force for a moving magnet linear motor. The motor is comprised of a rigid chamber link, which passes through the hollow core of the bobbin, with a ferromagnetic keeper washer and axially aligned rare earth ring magnet at either end, with like magnetic poles facing each other. The motor is elastically suspended between the first and second flexible chambers. Current flow through the coil of the forcer assembly provides motive force for the motor via attraction or repulsion of the motor magnets and movement of the motor increases the volume of the first flexible chamber while decreasing the volume of the second flexible chamber, or vice versa. The internal volume of the first flexible chamber is coupled via an air line to an ear canal and through a controlled valve to a small vent, and the internal volume of the second flexible chamber is vented to ambient air pressure. Changes in volume of the first flexible chamber, due to motor movement, produce changes in ear canal pressure re Boyle's law. The vent may be opened to allow ear canal pressure to gently equalize to ambient air pressure or to generate ear canal pressure sweeps free of pressure baseline offset. The vent may be closed to set a static ear canal pressure or to generate ear canal pressure sweeps with an incidental baseline offset. The vent may be controlled to generate ear canal pressure sweeps with an intended baseline offset. The device produces ear canal pressure proportional to drive voltage, so any desired pressure versus time function can be generated by applying a coil driving voltage with the appropriate amplitude versus time function. The device operates quietly to avoid interference with aural acoustic immittance measurement, and should have a long and maintenance free life span.

A fluid connector includes an extending section including a spiked end to pierce the container port. The extending section includes at least one air conduit and at least one fluid conduit therethrough. The extending section further includes a first abutment member and second abutment member. The first abutment member is adapted to abut a first or air side of the container port upon piercing of the container port. The second abutment member is spaced from the first abutment member and is adapted to abut a second or fluid sided of the container port. The fluid connector can further include grasping members extending from the extending section to facilitate rotation of the extending section relative to the container port during piercing thereof. The fluid connector can also include a check valve in fluid connection with the air line. In several embodiments, the check valve is positioned within the extending section.

For adjustment of a desired burner gas-air ratio over the broadest possible load range without additional pressure tapping of the burner, combustion chamber, or air lines, a ratio controller is provided that permits adjustment of the gas flow as a function of counterpressure. For adjustment, the ratio controller has at least one position-variable measurement site, or at least two measurement sites, connected directly or indirectly via a pilot valve, to an actuating diaphragm via a valve block or throttle valve block. Depending on whether the control pressure is picked up more from one or more from the other measurement site, the gas flow and therefore the gas-air ratio can be adjusted to be larger or smaller.

A floatable fuel tank that is capable of serving as a barge or lifeboat/dingy. Tank comprises a plurality of bladders with each having a fuel chamber and air chamber running longitudinally from stern to a forward bladder. If used as a fuel storage device, tank is attached to boat using towing lines and fuel lines so boat consumes fuel held by fuel chambers. In emergency situations, tank is capable of use as a lifeboat by detaching towing lines, air lines and fuel lines and pumping fuel out of fuel chambers with air so that persons may reside on top of tank. Under normal conditions in this configuration, it could be used as a dingy for normal transportation to and from a boat at anchor.

In an air conditioning system for an aircraft, two pre-mixing units respectively mix cold air from two air conditioning units with recirculated fuselage interior air from two recirculation units, to prepare two pre-mixed air flows that are both directed into and mixed together in a common air distribution mixing chamber from which mixed air distribution lines branch off to respectively associated separate air conditioning zones within the fuselage. Post-mixing units are respectively interposed in the mixed air distribution lines and respectively mix additional quantities of recirculated fuselage interior air into the mixed air distribution lines. Thereby, the admixture of recirculated air is divided into at least two stages, the system provides redundant failure tolerant operation, and the danger of ice formation in the air lines is reliably prevented even while the air conditioning units provide cold air at a temperature below the water freezing point.