718results about How to "Improve precision control" patented technology

It is possible to respecify the product (mass flow controller) corresponding to multiple types of actual process gases and multiple flow rate ranges, even after the mass flow controller has been shipped. With the mass flow rate control device in an initial state, calibration gas characteristic data is derived by measuring actual flow rate versus a flow rate setting signal using a calibration gas, and this calibration gas characteristic data is then saved to control unit. Meanwhile, actual gas characteristic data is derived by measuring actual flow rate versus a flow rate setting signal for each of a plurality of types of actual gas, and this actual gas characteristic data is then saved to a storage medium. Subsequently, prior to operating the mass flow rate control device, the actual gas characteristic data for an actual process gas is read from the storage medium via a computer, and the calibration gas characteristic data that was saved to the control unit is read out. The calibration gas characteristic data is then converted to controlled flow rate correction data based on the actual gas characteristic data, and the controlled flow rate correction data is saved to the control unit. Actual gas flow rate is corrected based on this controlled flow rate correction data.

A raw material gas supply apparatus includes a liquid raw material gas supply source, a source tank storing liquid raw material, a gas distribution passage through which raw material gas comprising steam of the liquid raw material is supplied to a process chamber from the source tank, an automatic pressure regulator installed on an upstream side of the gas passage, wherein the automatic pressure regulator keeps supply pressure of the raw material gas at a set value, a supply gas switching valve installed on a downstream side of the gas passage, wherein this valve opens and closes the gas passage, an orifice provided on at least one of an inlet side or outlet side of the valve, wherein the orifice regulates flow rate of the raw material gas, and a constant temperature heating device heats the source tank, the gas passage, the valve and the orifice to a set temperature.

A chain hoist having a casing into which and with respect to which a chain travels is provided with an externally mounted position encoder assembly. A releasable connector, such as a ratchet strap, is employed to firmly but removably couple the position encoder assembly housing externally on the chain hoist casing. The releasable connector holds the position encoder assembly housing in a fixed position relative to the chain hoist casing. The position encoder assembly has a chain gear that is rotatably mounted relative to the position encoder assembly housing proximate to the chain access opening in the chain hoist casing. The precision encoder assembly chain gear engages the portion of the chain that is maintained under tension at a location externally of the chain hoist casing and rotates as the chain travels relative to the chain hoist casing. A releasable clamp is anchored relative to the position encoder assembly housing and is engageable to maintain engagement of the position encoder assembly chain gear with the chain. An encoder is mounted with respect to the position encoder assembly housing and detects rotational movement of the position encoder assembly chain gear. The sensor provides electrical output signals indicative of the extent and direction of rotational movement of the position encoder assembly chain gear. The position encoder assembly provides precise, reliable output signals indicative of the position of the chain relative to the chain hoist. The position encoder assembly may be readily removed from the chain hoist, and just as easily attached thereto.

Provided are a functional porous film having a plurality of functions, a method of manufacturing the same, and a sensor using the same. In the functional porous film, a functional portion having a different function from a porous body is disposed on the inner wall of a pore of the porous body. The functional porous film is formed through forming a precursor film including a pore-forming powder such as an organic powder on which a material powder of the functional portion is deposited and a material powder of the porous body, and then heating the precursor film to remove the pore-forming powder and sinter the material powder of the porous body.

This invention provides an electron source manufacturing apparatus which can be easily downsized and operated. The electron source manufacturing apparatus includes a support member for supporting a substrate (10) having a conductor (11), a vessel (12) which has a gas inlet port (15) and a gas exhaust port (16) and covers a partial region of the surface of the substrate (10); a gas inlet unit (24) connected to the gas inlet port (15) to introduce gas into the vessel, an exhaust unit (26) connected to the gas exhaust port to evacuate the interior of the vessel, and a voltage application unit (32) for applying a voltage to the conductor.

This recording-medium conveying device comprises a conveying belt, the conveying belt, a belt charging unit, and a pressing roller. The conveying belt is wound around a driving roller and a driven roller so as to convey a recording medium to an image recording part. The conveying belt includes an insulating layer formed at one side contacting the recording medium. The belt charging unit is provided in contact with the insulating layer so as to charge the insulating layer with a positive charge and a negative charge alternately in a moving direction of the conveying belt by applying an AC bias to the conveying belt. The pressing roller presses the conveying belt against the driving roller so as to prevent the conveying belt from slipping on the driving roller.

The invention discloses an integrated steel pipe and flange splicing and machining machine and a machining process thereof and aims to provide an integrated steel pipe and flange splicing and machining machine which can improve the manufacturing precision and the production efficiency and reduce the labor intensity and is high in steel pipe and flange welding quality and a machining process of the machine. The integrated steel pipe and flange splicing and machining machine comprises a working platform, and a supporting bracket which is arranged on the working platform and is used for supporting a steel pipe, wherein one end of the working platform is provided with a first welding device; a first guide rail which extends to the other end of the working platform is arranged on the top of the working platform; a first mounting plate is arranged on the first guide rail in a sliding mode; a second welding device is arranged on the first mounting plate; and flange fixing templates are arranged on the first welding device and the second welding device. The machining process comprises the following steps of: lifting the steel pipe to the supporting bracket, and fixing the flange to a flange fixing template; and welding annular gaps of the inner and outer side faces of the steel pipe and the flange through the first welding device and the second welding device.

A modified optical fiber comprises one Surface Light Field Emulation (s-LiFE) segment, comprising a core; a cladding; and multiple controlled nanoscale diffusion centers to emit light through the side of the optical fibers. Optionally, the modified optical fiber has a coating. The nanoscale diffusion centers are physical geometric patterns or composition patterns in the cladding or the coating. The s-LiFE optical fiber is a member of an illumination system further comprising a light source. The method of making of said s-LiFE optical fiber comprises a fiber spooning step.

A method, system, and medium of modeling and/or for controlling a manufacturing process is disclosed. In particular, a method according to embodiments of the present invention includes the step of identifying one or more input parameters. Each input parameter causes a change in at least two outputs. The method also includes the step of storing values of the identified inputs and corresponding empirical output values along with predicted output values. The predicted output values are calculated based on, in part, the values of the identified inputs. The method also includes the step of calculating a set of transform coefficients by minimizing a score equation that is a function of differences between one or more of the empirical output values and their corresponding predicted output values. The method further includes the steps of receiving a new set of values for the identified inputs, transforming the new set of values for the identified input using the set of coefficients, and calculating a set of predicted output values using the transformed input values.

An exposure apparatus is equipped with a table which holds a wafer and is movable along an XY plane and has a grating provided on its rear surface, an encoder which irradiates a first measurement beam on the grating from below, receives a return light, and measures a first position information of the table when the table moves in a predetermined range, and another encoder which has a head section provided in a frame and irradiates a second measurement beam on a different grating on the table from the head section, receives a return light, and can measure a second position information of the table, concurrently with measurement of the first position information by the encoder when the table moves in predetermined range. A controller drives the table, based on position information having a higher reliability of the first and the second position information.

In a capacitor microphone, a diaphragm is positioned opposite to a fixed electrode for covering inner holes of a ring-shaped support, wherein when the diaphragm is deflected to approach the fixed electrode due to electrostatic attraction upon application of a bias voltage, internal stress that occurs on the diaphragm is canceled by compressive stress that is applied to the diaphragm in advance. The diaphragm is formed using a multilayered structure including a first thin film and a second thin film whose internal stress differs from the internal stress of the first thin film, thus adjusting the total internal stress thereof. The diaphragm can be formed in such a way that a center layer having a single-layered structure is sandwiched between first and second coating layers having controlled residual tensions and resistance against hydrofluoric acid.

An exhaust line (15) connected to a chamber (13) comprises a TMP (22) and a dry pump (23). The chamber (13) and the TMP (22) are connected by a first exhaust pipe (25), and the TMP (22) and the dry pump (23) are connected by a second exhaust pipe (28). A measuring section (24) monitors a partial pressure of TiCl₄ or NH₃ in an exhaust gas flowing in the second exhaust pipe (28). Two types of process gases are alternately supplied into the chamber (13) for a predetermined time, and when the partial pressure of one of the supplied process gases in the exhaust gas is reduced to a predetermined value, a control means (12) starts supplying the other process gas.

An LED drive circuit, wherein a circuit that drives light-emitting diode with a common connected cathode has a resistor connected to the anode of the light-emitting diode, an NPN-type transistor connected to the second terminal of the resistor that approximately determines the control current for the emission of light in cooperation with the resistor, an NPN-type transistor positioned in parallel with the resistor and connected to the anode of the light-emitting diode, and a current supply, a level shifter, and a switch for selectively changing the voltage between the base-emitter of the second transistor, which are placed between the base of transistor and resistor.

A flight control system includes an Acceleration and Attitude Command/Velocity Hold mode (AACVH) algorithm which blends attitude commands with acceleration commands. This blending determines a trim attitude for a given rotorcraft flight condition.

Positional information of a stage within a movement plane is measured, using three encoders which include at least one each of an X encoder and a Y encoder. Based on position measurement values of the stage, the encoder used in position measurement is switched from an encoder (Enc1, Enc2 and Enc3) to an encoder (Enc4, Enc2 and Enc3). On the switching, a coordinate linkage method or a phase linkage method is applied to set an initial value of an encoder (Enc4) which is to be newly used. Accordingly, position measurement values of the stage before and after the switching are stored even though the encoder used in position measurement of the stage is sequentially switched, and the stage can be driven accurately two-dimensionally.

A linkage system is provided which is equipped with a compact and high-rigidity link mechanism with a large load capacity. The linkage system includes three or more link mechanisms. Each link mechanism consists of a center link member and end link members rotatably coupled to the center link member and to link hubs that are provided to an input member and an output member, respectively. An input side and an output side of a center cross-sectional plane of each link mechanism are geometrically identical. One or more of revolute joints of two or more of the link mechanisms that are coupled to the input member are provided with a stopping mechanism for stopping the output member at a given position.

The invention discloses a small-size unmanned rotary wing aircraft dynamic model identification method based on an adaptive genetic algorithm, which relates to flight status data acquisition and optimization, dynamic model building and parameter identification, and parameter optimization validation. Firstly, status data and control data when a small-size unmanned rotary wing aircraft executes standard actions are acquired through a data acquisition system, and smoothing and filtration are conducted to eliminate wild values; then aiming at the operating characteristics of the small-size unmanned rotary wing aircraft at autonomous takeoff and landing stages, a small-size unmanned rotary wing aircraft dynamic model is built through a balance point linearization method and model parameters are identified through the adaptive genetic algorithm; and finally intelligent parameter evaluation indexes are built and the effectiveness of the model parameters is evaluated and judged through a one-step predication method. The small-size unmanned rotary wing aircraft dynamic model identification method based on the adaptive genetic algorithm solves the problem in the dynamic model identificationof the small-size unmanned rotary wing aircraft, can realize the high-accuracy control of the small-size unmanned rotary wing aircraft, and has the advantages of low testing cost, short cycle, simplecalculation, high dynamic model accuracy and weak dependence on initial values.