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63results about How to "Avoid drafts" patented technology

Pipeline all-position laser and arc combined welding system

The invention provides a pipeline all-position laser and arc combined welding system. The pipeline all-position laser and arc combined welding system comprises a laser sensor, an image processing computer, a controller, an actuator and a guard plate. The laser sensor is used for collecting first position image information and second position image information of a welding seam; the image processing computer is used for calculating the transverse deviation and the longitudinal deviation of the welding seam according to the first position image information and the second position image information; the transverse deviation is transformed into a transverse deviation voltage, the longitudinal deviation is transformed into a longitudinal deviation voltage, and after delay calculation is conducted according to the preact delay quantity, the transverse deviation voltage and the longitudinal deviation voltage are sent to the controller; the controller is used for correcting the transverse deviation according to the transverse deviation voltage and correcting the longitudinal deviation according to the longitudinal deviation voltage; the actuator is used for controlling a combined welding torch and the welding seam to be maintained in an accurate centering state according to the corrected transverse deviation and the corrected longitudinal deviation, and then welding is conducted; the guard plate is used for preventing welding spatter from polluting a focusing lens of the laser welding torch to protect a lens, the pressure intensity of a laser welding torch protection gas curtain is lowered, and the welding quality is ensured.
Owner:BC P INC CHINA NAT PETROLEUM CORP +1

New disffuser in central air conditioning system

InactiveCN1494647AAppropriate and even distributionNo cleaning problemsDucting arrangementsLighting and heating apparatusEngineeringFlange
An improved diffuser (27) for central air conditioning system comprising of a single piece centre core (30), at least one intermediate core (29) and an outer frame (28), the single piece centre core consisting of an outwardly and downwardly directed slanting surface (35) originating from a centre point and ending into a substantially horizontal flange at its bottom periphery, a pair of vertical strips (36) attached at the back side of the slanting surface in spaced apart relationship and opposing to each other, at least a pair of spaced apart holes (25) provided in each vertical strips, the said intermediate core consisting of vertical collar (31) at its top, an outwardly and downwardly directed slanting surface (16) ending into a substantially horizontal flange (17) at its bottom, at least a pair of holes (25) provided into two opposing vertical sides (34) of the said collar, the said outer frame consisting of a vertical collar (7) at the top, an outwardly downwardly directed slanting surface (9) ending into a substantially horizontal flange (10), at least a pair of holes provided in two opposing sides of the said collar and at least one pair of rods (19) passing through the said holes for attaching the said centre core to the said intermediate core and said outer frame.
Owner:拉梅什纳纳穆哈特

Flight direction control device of aircraft

The invention discloses a flight direction control device of an aircraft. The flight direction control device comprises a girder and two propellers. The flight direction control device is characterized in that the girder is a hollow circular tube, the middle of an inner cavity of the hollow circular tube is provided with an adjusting screw, and nuts are screwed to the two ends of the adjusting screws respectively; the two ends of the adjusting screw are provided with half shaft tubes respectively, and the inner end of each half shaft tube is rotatably arranged on the corresponding nut in a sleeved mode; the lower walls, corresponding to the two ends of the adjusting screw, of the girder are provided with arc holes, an electric cylinder and a rotating force arm are arranged below the positions, corresponding to the arc holes, of the girder, a stretching and contracting shaft of the electric cylinder is connected with the lower end of the rotating force arm, and the upper end of the rotating force arm is fixedly connected with the half shaft tubes; the outer ends of the two half shaft tubes are provided with bearing seats respectively, and the two bearing seats are internally provided with propeller shafts respectively; the upper ends of the two propeller shafts are provided with belt wheels, and a transmission belt is connected between the two belt wheels; the propellers are connected to the lower ends of the two propeller shafts. By means of the adjusting structure, the power loss of a small aircraft can be lowered, and effective lift force is improved; the flight direction control device is suitable for controlling the small aircraft in four directions.
Owner:杨海燕

High-protection frequency converter

The invention discloses a high-protection frequency converter. The high-protection frequency converter comprises a cabinet, a partition board, a frequency converter unit, a radiator and a radiating substrate, wherein the partition board is located in the cabinet and divides inside of the cabinet into a front bin and a back bin; the radiating substrate is located in the front bin and is in sealed connection with the partition board through a sealing element; the frequency converter unit is arranged on the front side of the radiating substrate; the partition board is provided with a through hole allowing penetration of the radiator, the radiator is arranged on the back side of the radiating substrate, and the sealing element is located on the periphery of the radiator. According to the high-protection frequency converter, the radiating substrate is arranged in the front bin and is in sealed connection with the partition board through the sealing element, the frequency converter unit is arranged on the front side of the radiating substrate, so that the front bin and the back bin on two sides of the partition board are completely isolated through the sealing element and the radiating substrate, and the protection level is further increased; ventilation between the front bin and the back bin is avoided, heat energy of the front bin is totally conducted to the back bin through the radiator, and the radiation efficiency is improved; meanwhile, mounting of the whole frequency converter unit is facilitated, and the mounting efficiency is improved.
Owner:SHENZHEN INVT ELECTRIC
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