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58 results about "Beta angle" patented technology

The beta angle (β) is a measurement that is used most notably in orbital spaceflight. The beta angle determines the percentage of time that a satellite in low Earth orbit (LEO) spends in direct sunlight, absorbing solar energy. The term is defined as the angle between the orbital plane of the satellite and the vector to the Sun (i.e., the direction from which the Sun is shining). The beta angle is the smaller of the two angles between the Sun vector and the plane of the object's orbit.

Kinematic inverse method for installation process of steam generator examining and repairing mechanical arm

The invention provides an inverse kinematical solution method during the installation process of an overhaul robot arm of a steam generator; wherein, the definitions of Alpha, Beta, and Gamma are as follows: at the initial stage, a base coordinate system is in the same attitude with a world coordinate system, then the base coordinate system revolves around the Y axis for the Alpha angle, next revolves around the X axis for the Beta angle, and finally revolves around the Y axis again for the Gamma angle, so as to obtain the ultimate attitude of the base coordinate system. The respective positions of the articulation points are: B point is the arithmetic endpoint of the robot arm, C, D, E, F, G, and H points are respectively the sixth to first articulation points, and I point is toe arithmetic endpoint; first, the coordinates of the articulation points of the robot arm are solved, and the coordinates of B, C and D points are resolved by means of the normal solutions during installation process; then, a vector HI is acquired based on the coordinate of I point and the attitude angles Alpha, Beta, and Gamma, so the coordinate of H point can be deduced; next, the coordinate of F point is solved; finally, the turn angles Theta (i) of the articulation points can be resolved (wherein, I=1, 2, 3, 4, 5, 6). The inverse kinematical solution method in the invention has the advantages of avoiding building up the kinematical equation of the robot arm, greatly reducing the amount of calculation, quickening the operational speed, and solving all the solutions.
Owner:HARBIN ENG UNIV

Method for calculating soil pressure of limited soil

InactiveCN106638537AEconomical, reasonable and practicalIn situ soil foundationBeta angleSoil science
The invention discloses a method for calculating soil pressure of limited soil. The method comprises the following steps: determining profile parameters of a foundation pit profile and limited soil, setting the included angle between a fracture plane of the limited soil and the horizontal direction, performing force analysis on a fractured slide body, obtaining the weight of the fractured slide body, establishing an equation set by utilizing known parameters according to static balance conditions in the horizontal direction and the vertical direction, substituting an expression of soil pressure of the limited soil, deriving a shearing damage angle for soil pressure of the limited soil, enabling a derivative equation to be zero, obtaining a shearing damage angle value, reversely substituting the shearing damage angle value into the expression of soil pressure of limited soil, calculating a numerical value, namely soil pressure, generated on a surrounding structure, of every linear meter of limited soil. According to the method disclosed by the invention, values of beta angles are different, different limited soil boundary conditions are contained, stress characteristics of limited soil are sufficiently taken into consideration, and a fracture plane direction angle of limited soil is derived, so that active pressure, which conforms to reality, of limited soil is calculated, and therefore, the method has a very good popularization application value.
Owner:南昌市政公用集团有限公司 +2

Integrated-shaft and three-roller corner rolling device for continuous casting billet corner rolling

ActiveCN104985149AOvercoming shear rollingOptimizing the chamfer shapeBeta angleSlant angle
The invention relates to the field of metal solidification and continuous casting, in particular to an integrated-shaft and three-roller corner rolling device for continuous casting billet corner rolling. The device comprises a middle positioning roller (1), an upper chamfer roller (2-1), a lower chamfer roller (2-2), a roller shaft and a roller supporting frame (4); the roller shaft comprises a middle roller shaft section (3) and chamfer roller shaft sections (6) at the two ends; the chamfer roller shaft sections (6) and the middle roller shaft section (3) are arranged in an alpha angle manner; the middle positioning roller (1) is mounted on the middle roller shaft section (3); the upper chamfer roller (2-1) and the lower chamfer roller (2-2) are respectively mounted on the chamfer roller shaft sections (6); the chamfer roller shaft sections (6) are connected with the roller supporting frame (4); the alpha angle is 0-45 degrees; a roller surface slant angle beta of each chamfer roller is 30-70 degrees; and the alpha angle is less than or equal to the beta angle. The device effectively avoids the defects of shear cracks arising from shear rolling, an optimized casting billet corner chamfer shape can be obtained, and split or surface upwarping of the edge of a plate is eliminated.
Owner:ZHONG NAT ENG & RES CENT

Integrally stretched body pushing double-suction type range hood

The invention relates to an integrally stretched body pushing double-suction type range hood which comprises a box and an integrally stretched body, wherein a motor, an air wheel, an air channel, an air outlet, a decorative cover and other parts are arranged in the box; the integrally stretched body is formed by combining a transverse cavity and a vertical cavity; and the transverse cavity and the vertical cavity are in a seamless integral structure. The range hood of the invention has luxurious and beautiful appearance, can not accumulate dirt, and can be cleaned conveniently. The stretched base surface and the back stretched surface of the transverse cavity respectively form a beta angle and a gamma angle with the front surface of the vertical cavity, wherein gamma is greater than 90 degrees and less than or equal to 125 degrees, and beta is less than gamma; and air inlet holes are arranged on the back stretched surface of the transverse cavity and the front surface of the vertical cavity, thereby possessing the efficacy of secondary emission of oil smoke generated by cooking. The novel range hood of the invention has the advantages of luxurious and beautiful appearance, very convenient maintenance and the like and can thoroughly clear the oil smoke generated by cooking.
Owner:贺滨

Laser gyro combined offset frequency method and combined device for inertial measurement of laser gyro

The invention provides a laser gyro combined offset frequency method, belonging to the technical field of inertial navigation equipment. The method comprises the following steps: combination with two-way constant speed and mechanical shaking is adopted; a 1-3 axis laser gyro group is arranged on a two-way constant-speed offset-frequency rotary platform rotating around a vertical axis, all sensitive axes of the laser gyro are deviated from a beta angle of a rotary axis of the offset-frequency rotary platform and are driven by the rotary platform to rotate, and a component (alpha & cosine beta)of the rotary angle speed (alpha &) on all the sensitive axes of the laser gyro is the offset-frequency angle speed of the laser gyro; and simultaneously, the rotary angle speed (alpha &) carries outrotary modulation on the error of the laser gyro axis. In the laser gyro combined offset frequency method adopting combination of two-way constant speed offset frequency and mechanical shaking offsetfrequency, not only is the accuracy guaranteed, but also the difficulties for design and manufacture are reduced. The laser gyro combined offset frequency method can be used for high-accuracy laser gyro strapdown inertial systems.
Owner:SHAANXI BAOCHENG AVIATION INSTR

Method for portable folding novel multi-rotor unmanned aerial vehicle

InactiveCN107472508ALower the altitudeReduce the length and width dimensions in the horizontal directionFuselagesAir-flow influencersBeta anglePropeller
The invention provides a method for portable folding a novel multi-rotor unmanned aerial vehicle. Firstly, foldable propellers are folded to the direction of a vehicle body, the folded foldable propellers are aligned with corresponding foldable vehicle arms; the foldable vehicle arms are coaxially hinged to vehicle arm bases, at the moment, the vehicle arms are rotated and folded so as to be perpendicular to the vehicle arm bases, and the foldable vehicle arms form an alpha angle with the vertical direction; and the foldable vehicle arms continuously rotate for a beta angle to the direction of the vehicle body, and the portable folding of the vehicle arms is completed. According to the method for portable folding the novel multi-rotor unmanned aerial vehicle, the dimensions of the length and the width of the multiple rotors after being folded can be greatly compressed by adopting a method that folding of the vehicle arms in a tilt space is matched with folding of the propellers, meanwhile, relative to vertical folding of the vehicle arms, the requirements for the height of an undercarriage can be lowered greatly, the dimension of the overall vehicle after being folded is reduced to a largest extent, and the portability of product transporting is improved effectively.
Owner:TIANJIN AEROSPACE ZHONGWEI DATA SYST TECH CO LTD

A device for blowing and spraying powder at the bottom of a ladle in a cyclone-protected gas storage chamber

InactiveCN102296156AReduce accumulationReduced resistance to crevice entryBeta angleVertical plane
The invention discloses a ladle bottom blowing power injection device with a whirlwind-type flow-smoothing gas storage chamber, and belongs to the technical field of steel smelting. The ladle bottom blowing power injection device with a whirlwind-type flow-smoothing gas storage chamber comprises a slit-type powder injection component I and the whirlwind-type flow-smoothing gas storage chamber II.A fire-resistant material is filled into the slit-type powder injection component. Multiple slits are distributed uniformly in the fire-resistant material. A middle axle plane which passes through ends which belong to the slits and are close to an axle center, and a vertical plane where the slits are arranged form an included angle gamma. The bottom of the whirlwind-type flow-smoothing gas storage chamber is connected with a whirlwind-type accelerating chamber. A low end of the whirlwind-type accelerating chamber is provided with a whirlwind-type gas flow conveying pipes. The whirlwind-type gas flow conveying pipes are arranged at both sides of a power-gas flow conveying pipe and form respectively beta angles with the power-gas flow conveying pipe. The ladle bottom blowing power injectiondevice with the whirlwind-type flow-smoothing gas storage chamber can reduce obviously a degree of powder-gas flow pulsation, accumulation of falling powder, and resistance to a powder-gas flow when the powder-gas flow is fed into the slits, can improve obviously a uniform flow conveying rate of the powder-gas flow in the slits. The ladle bottom blowing power injection device with the whirlwind-type flow-smoothing gas storage chamber has the advantages of stable blowing, small pulsation, low corrosion on fire-resistant materials, safe and reliable characteristics, feasibility for continuous and stable blowing and long service life of fire-resistant materials.
Owner:NORTHEASTERN UNIV LIAONING

Yaw maneuvering control method and system of spacecraft by using virtual sun vector

The invention relates to a yaw maneuvering control method and system of a spacecraft by using a virtual sun vector. The yaw maneuvering control method comprises the steps that a vector expression of areal sun vector in an orbit coordinate system of the spacecraft is obtained; the included angle between the real sun vector and an orbital plane is calculated according to the expression of the realsun vector, and a Beta angle of the real solar vector is obtained; a threshold valve interval for one or more Beta angles is preset, the corresponding relationship between a Beta angle of the virtualsun vector and the Beta angle of the real solar vector which are set in the preset threshold valve interval is set; when the Beta angle of the real sun vector enters into the set threshold valve interval, the virtual sun vector is started to be calculated in real time according to the Beta angles of the real sun vector and the virtual sun vector; a target yaw angle of the spacecraft is calculatedaccording to the virtual sun vector; and according to an own attitude control system of the spacecraft, a yaw maneuvering angle of the spacecraft is controlled in real time to track the target yaw angle, and the yaw maneuvering control of the spacecraft implemented by using the virtual sun vector is realized.
Owner:TSINGHUA UNIV

Multilayer transparent imaging device

The invention relates to reflection imaging, and relates to an imaging device that at least two layers of transparent images can be displayed in the same direction, and two layers or more than two layers of transparent images can be seen from multiple directions. The imaging device comprises a display screen and reflection boards which are used for enabling the display screen to be reflected by the corresponding reflection surfaces of the reflection boards so that the image in the display screen can be imaged at the corresponding position. The imaging device is characterized by comprising at least one set of display screen. Each set at least comprises one display screen. There are at least three reflection boards, wherein an alpha angle is formed between the reflection surface of at least one reflection board and the reflection surface of another reflection board, the alpha angle is greater than or equal to 30 degrees and less than or equal to 90 degrees, a beta angle is formed between the reflection surface of at least one reflection board and the display surface of the display screen, and the beta angle is greater than or equal to 30 degrees and less than or equal to 60 degrees. The reflection boards are total reflection boards or semitransparent reflection boards. Reflection thin films are coated on the reflection boards and used for enhancing light ray reflection capacity of the reflection boards.
Owner:梁雁飞

Illumination super-resolution fluorescence microscopic imaging method and device for microstructure light

The invention relates to an illumination super-resolution fluorescence microscopic imaging method and device for microstructure light and belongs to the field of optical super-resolution microscopic imaging and fluorescence detection. A microstructure light generation device is composed of a polygonal frustum of a prism and multiple linear lasers; the polygonal frustum of a prism is made of a transparent material, the area of the lower bottom surface is larger than that of the upper bottom surface, the included angle between each side surface and the bottom surface of the polygonal frustum ofa prism is beta, two or more side surfaces of the polygonal frustum of a prism are provided with the linear lasers, all the linear lasers can be reflectively transmitted at the beta angle in a zigzagshape between the upper and lower bottom surfaces of the frustum of a prism, partial light can be reflected and leak every time that light is vibrated to the upper bottom surface, and finally clear strip structure light can be generated on the upper surface of the device. The illumination super-resolution fluorescence microscopic imaging method and device for the microstructure light can be applied to a super-resolution fluorescence microscopic system.
Owner:BEIJING UNIV OF TECH

Processing method of right-angle helicoidal surface

The invention provides a processing method of a right-angle helicoidal surface. The processing is carried out through utilizing a single-blade double-curved surface profile-shaped milling cutter. The processing method comprises the steps of during the right-angle helicoidal surface processing process through the single-blade double-curved surface profile-shaped milling cutter, maintaining the axis of the single-blade double-curved surface profile-shaped milling cutter and the axis of the right-angle helicoidal surface to form an alpha-degree angle, and maintaining the distance between the axis of the single-blade double-curved surface profile-shaped milling cutter and the axis of the right-angle helicoidal surface to be b till the processing of the right-angle helicoidal surface is over, wherein alpha is 90 to beta; beta is an include angle between a generating line of the single-blade double-curved surface profile-shaped milling cutter and the axis of the single-blade double-curved surface profile-shaped milling cutter; beta angle is calculated through the formula that beta equals to arctan (2pi*c/h); h is the lead of the right-angle helicoidal surface; c is the minimum distance between the generating line of the single-blade double-curved surface profile-shaped milling cutter and the axis of the single-blade double-curved surface profile-shaped milling cutter; and c equals to b. According to the processing method, the right-angle helicoidal surface with a relatively small error can be processed on a milling machine.
Owner:CHONGQING JIANSHE IND GRP

Processing method of right-angle helicoid

The invention provides a processing method of a right-angle helicoidal surface. The processing is carried out through utilizing a single-blade double-curved surface profile-shaped milling cutter. The processing method comprises the steps of during the right-angle helicoidal surface processing process through the single-blade double-curved surface profile-shaped milling cutter, maintaining the axis of the single-blade double-curved surface profile-shaped milling cutter and the axis of the right-angle helicoidal surface to form an alpha-degree angle, and maintaining the distance between the axis of the single-blade double-curved surface profile-shaped milling cutter and the axis of the right-angle helicoidal surface to be b till the processing of the right-angle helicoidal surface is over, wherein alpha is 90 to beta; beta is an include angle between a generating line of the single-blade double-curved surface profile-shaped milling cutter and the axis of the single-blade double-curved surface profile-shaped milling cutter; beta angle is calculated through the formula that beta equals to arctan (2pi*c / h); h is the lead of the right-angle helicoidal surface; c is the minimum distance between the generating line of the single-blade double-curved surface profile-shaped milling cutter and the axis of the single-blade double-curved surface profile-shaped milling cutter; and c equals to b. According to the processing method, the right-angle helicoidal surface with a relatively small error can be processed on a milling machine.
Owner:CHONGQING JIANSHE IND GRP

Method for determining beta angle changing curve of planar double enveloping worm

The invention discloses a method for determining a beta angle changing curve of a planar double enveloping worm. The method includes the steps that a space coordinate system is established according to a beta angle changing planar double enveloping worm forming principle, the beta value is set to be a function of worm gear turn angle phi<2>, and beta angle changing addendum thickness equation delta and tooth surface undercutting discriminant equation r1 are derived on the basis of an envelope method principle; the minimum side addendum thickness value delta<min> meeting the requirement of no sharpening is calculated according to worm parameters; the addendum thickness is made to change regularly and linearly in the worm helical line direction from side teeth to throat teeth; multiple worm gear turn angles phi<2> are obtained according to an equal difference rule to obtain the corresponding thickness values so as to form feature points (phi<2>, delta (beta)); the beta value which each point corresponds to is obtained through the beta angle changing addendum thickness equation, the beta curve is fitted, the fitted beta curve is substituted into the tooth surface undercutting discriminant equation, and an undercutting line is drawn on a worm tooth surface graph; and the undercutting ratio is estimated, if the design requirement is met, the operation is finished, if the design requirement is not met, throat addendum thickness delta<h> is reduced or the addendum thickness change rule is changed to a cosine rule, and the operation returns to the step 3.
Owner:YANSHAN UNIV
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