![]() Mechanical reduction gear
专利摘要:
The invention relates to mechanical engineering and can be used in robotics, in agricultural machines, in clock mechanisms, in analog display devices, micromechanics, tools and measuring mechanisms, gears, etc. The purpose of the invention is to reduce. dimensions and improved manufacturability. When moving the rotor 12, driven by an eccentric 13 connected to the drive shaft 1, pairs of junction bodies successively interact with all the slots 10 and 11 of the gear units 6 and 7. At the same time, no more than two pairs of moving bodies are coupled with the slots 10, 11, while a third pair is free. Thus, the rotation of the driven shaft 5 is made up of a large number of single steps of a pair of running bodies due to their adhesion with the corresponding pair of grooves, which increases the accuracy, and the gaps resulting from wear do not accumulate. 20 hp f-ly, 29 ill., 2 tab. 15 10 i WITH 公开号:SU1442085A3 申请号:SU853863653 申请日:1985-03-01 公开日:1988-11-30 发明作者:Бажюла Роже 申请人:Редюто С.А. (Фирма); IPC主号:
专利说明:
sixteen 4 4 S ABOUT 00 ate cm Phie. i The invention relates to a mechanical gearbox having a leading axis and a driven member coaxially with it, which rotate at different angular speeds in the gear ratio function, also containing first and second gear units moving at an angle relative to each other, each containing a number of 10 reducible elements evenly distributed around the rotation center. appropriate gear unit. The purpose of the invention is to reduce the size of the gearbox and to improve technological consistency. FIG. I presents a mechanical gearbox, axial section; in fig. 2 is a view along arrow A in FIG. (gearbox, with cover removed); in FIG. 3-9 - seven successive stages required to rotate the driven gear unit 1/11 of a turn relative to the support body; on .fig. 10-20 - eleven stages necessary for turning the external driven gear unit 1/7 of a turn relative to the internal support gearing body; in fig. 21 -. instant rotation of the gearbox rotor; 30 in FIG. 22 — reducer with a four-blade rotor; in fig. 23 is a variant of the gearbox of FIG. 22; in fig. 24 - reducer, with two rotors, axial, section; in fig. 25 is a view along arrow B 35 of FIG. 24 (gearbox with a raised housing); in fig. 26 - gearbox with the location of the travel bodies between the reducing bodies, axial section; in fig. 27 - gearbox with 40 parallel-arranged rotors, axial cut; in fig. 28 — reducer, side view (with the removal of the side wall); in fig. 29 - drive elements and running gears .45 The mechanical gearbox contains a drive shaft 1 rotating in two bearings 2 and 3, one of which is housed in the gearbox casing 4, and the other in the hub of the output shaft 5 Be- 50 blowing shaft 1 and the output shaft 5 are coaxial, their angular velocities rotation depends on the gear ratio of the mechanical gearbox (Fig. 1-9). The mechanical gearbox contains two 55 gearbox bodies 6 and 7 which are coaxial with each other to the drive shaft 1. The gear member 6 is the supporting and fixedly connected to the casing 4, the gear member 7 is connected to the output shaft 5 and is the follower. Each of the gear units 6 and 7, respectively, contains an annular crown 8 and 9, they have different sizes and are installed concentrically. Each of the v crowns 8 and 9 contains a series of drive elements, in this case, respectively, formed by the slots 10 and II uniformly distributed around the center of rotation corresponding to the gear unit 6 and 7. In FIG. 1 crown 9 of the driven gear member 7 has eleven grooves 11, while the crown 8 of the support gear member 6 has seven grooves 10. The gearbox has an eccentric rotor 12 driven by an eccentric 13 connected to the drive shaft 1. The eccentric rotor 12 is made in the form of three radial arms 14 located symmetrically with respect to the center of the rotor and carrying bodies 15–20. The eccentric rotor 12 has two groups of drive bodies, each consisting of at least three body bodies. The running bodies 15, 16 and 19 form the first group of driving bodies, the running bodies 16, 18 and 20 - the second group. Each of the groups is located at the appropriate diameter of the rotor (- torus 12. The running gears of one group are combined with the running gears of the other group to form a pair of running gears 15 and 16, 17 and 18, 19 and 20. The number of slots 10 and 11 of the gear units 6 and 7 is determined by the following formula V n, - n N + X. N 2, -, one (one) in de N, is the number of grooves 10 of the supporting gear unit in this case, the external gear unit 6; Ui-pb are integers; X O is an integer; N is the number of drive elements of the driven gear unit; N. is the number of drive elements of the Ved-reducer organ, in this case the case of the reducer organ 7, p is a slal1) between the 1442085 running bodies 16, 18, 20 belonging to different pairs engaged in engagement with the driven gear unit 7. The number of drive elements of the gearbox body as a function of Islam drive elements of the support unit that ni to 6 do and shu vr vedu vayu ie in flax prices in the house N Y. N. + n N .. Z-N, (2) where Y and Z are integers. . The gear ratio is determined by the formula: U N ..- and- NI state of emergency n where n4 and the number of drive elements of the support gear unit 6, located between the two suspension bodies, belonging to different pairs that are in engagement with this gear unit. K equal in this case tea 2; N is the number of reducible elements of the driven gear unit 7, equal in this case P n is an integer equal to. In this case, I,. 1 For example, NI And Ni. i, 3, У 2y n I and X О, then N - 7, and the gear ratio U. «.22, If. Hi .. "2 that completely agrees . ,, With ierbrazhenn in FIG. 3-9 example where the driven gear body 7 contains eleven grooves II, and the support gear body 6 - seven grooves 10, Y - I, n «1, Z -, N, - 7, then N, P. In tab. 1 shows the various options; providing many different gear ratios. All combinations of arbitrary values for the coefficients V, X, Y, Z and n cannot provide constructively realizable structures, if the condition that the Number of drive elements N and N, and also, their corresponding values NI and L ,. are integers. o five in t. n When the reference gear opra; i 6 is external to the driven gear unit 7, the drive shaft 1 and the driven gear member 7 rotate in the same direction. The rotor 12 rotates in the opposite direction. The mechanical gearbox may have a driven gear unit 7, covering the support gear unit 6, i.e. external to organ 6 and rotates in the opposite direction to rotation of drive shaft 1 and eccentric 13 (fig. 10-20). The rotor 12 is rotated in the same direction as the driven gear unit 7. When the directions of rotation of the eccentric 13 and the driven gear organ 7 are opposite, the formula for determining the number of drive elements of the gear bodies is as follows: V. N -g n N, + X N. (3) thirty 35 When comparing formulas ()) and (3) n from.tabl. 2 that, depending on whether the support organ is external or internal, the gear ratio will change. The rotor 12 of the mechanical gearbox can be made in the form of four radial arms 14 (FIG. “22”), each of which carries a pair of running members 15 and 16, 1-7 and 8, 19 and 20, 40 21 and 22, successively interacting with the grooves 10 and 11, respectively, of the p-bearing organs b and 7. The supporting gearbox b covers the driven gearbox 7. The mechanical gearbox can have at least one additional rotor 23, driven by the drive shaft I and the eccentric 13. (Fig. 25). Each of the rotors 12 and 23 0 in FIG. 23 has two arms each carrying the main rotor 12, the driving bodies 15 and 16, 17 and 18, the additional rotor 23, the driving bodies 24 and 25, 26 and 27. The rotors 12 and 23 are concentrically mounted with the possibility of angular shift relative to each other by the spring element 28. This design is special. preferred because it allows 45 five . The UA2085 precisely adjusts the diameters of the pins forming the rotor's running bodies to the width of the grooves that drive the gear elements of the gear bodies, thereby arranging L1xft. The additional rotor 23 can have three arms and is installed on. ring & a surface of the main rotor I2 concentric with an eccentric 13, (Fig. 25-26), the shoulders of the additional rotor 23 go along the bisector of the angles formed by the shoulders of the main rotor 12, on the shoulders of the additional rotor 23 placed in pairs running bodies 24 and 25, 26 and 27, 29 and 30, interacting with grooves 10 and P gearboxes. bodies 6 and 7. elements 34 and 35 (Figs. 27 and 29), the supporting gear unit 6 in the form of the HYPR element of the PLA has two rows of eighteen drive elements in the form of uniformly distributed holes 36 and 37. Each row is located in a plane, 10 perpendicular to drive shaft I. The driven gear unit 7, made in the form of a cylindrical element 35, covering a cylindrical element 34, also has two rows The t5 of the drive elements in the form of circular holes 38 and 39, oriented with respect to the holes 36 and 37, in each row are eleven holes 38 and 39, the diameter of the holes 38 and 39 of the large Supporting gear body 6 contains seven grooves 10, as in FIG. 1 - 20 of the diameter of the holes 36 and 37. 9 but, since the additional rotor Primary 12 and additional 23 23 are offset at an angle relative to the main rotor 12, the number of grooves 11 of the driven gear member 7 is doubled, which, however, does not cause the unique center 40, 41 rotations affecting operation or transfer full-time Rotors 12 and 23 are installed with possible probes displaced axially one relative to another, but placed in identical angular positions relative to the gearbox ratio. Each of the rotors 12 and 23 works by itself, ji this condition is taken into account when calculating the gearbox. One of the advantages of this design is to increase the torque transmitted by the gearbox, since two pairs of running bodies are always in engagement with the reduction bodies, one on each rotor. Each pair of running bodies 15 and 16 may be formed by a cylindrical protrusion. rotation on eccentrics 13 and 42 arranged in series along the axis of the drive shaft I with an offset of 180, i.e. against each other The shoulder of each rotor 13 and 42 bears a pair of moving bodies 43 and 44, 45 and 46 formed by projections, - peripheral 3g whose surface represents the edge of the sphere. The diameter of the spherical edges forming the outer protrusions 43 and 45, designed to interact with the holes 36 and 37 reducer combined with the axis 31, of the extruded member 6, corresponds to the diameter or pinned hole of the po. holes 36 and 37. Spherical craters 12 (Fig. 26), the protrusions of the inner arms: stupid 44 and 46, designed to interact with the holes 38 and 39 of the slave gear They are located on opposite sides of the rotor 12. The pcto, divided to the axis of their axis, may be very small, and it does not affect the dimensions and strength of each protrusion. In this case, the gearbox has a supporting gearbox body 6 formed by one of the side walls of the casing 4, and a driven gearbox 7, rotated on the input shaft I and connected to the output shaft 5. The drive elements of gear gears 6 and 7 are located in planes perpendicular to the drive shaft 1, on both sides of the rotor 12 and are formed by radial slits 32 and 33. Gear units 6 and 7 moss () are formed A2085 elements 34 and 35 (Figs. 27 and 29), the supporting gear unit 6 in the form of the HYPR element of the PLA has two rows of eighteen drive elements in the form of uniformly distributed holes 36 and 37. Each row is located in a plane, 10 perpendicular to drive shaft I. The driven gear unit 7, made in the form of a cylindrical element 35, covering a cylindrical element 34, also has two rows The t5 of the drive elements in the form of circular holes 38 and 39, oriented relative to the holes 36 and 37, in each row are eleven holes 38, and 39, the diameter of the holes 38 and 39 is the diameter of the holes 36 and 37. The main 12 and an additional 23 25 of the corresponding centers of rotation 40, 41, Rotors 12 and 23 are installed with possible diameter of holes 36 and 37. Main 12 and additional 23 of rotation center 40, 41 of rotation, Rotors 12 and 23 are installed with possible motors displaced axially relative to each other, but placed in identical angular relative positions Tew rotation on eccentrics 13 and 42 arranged in series along the axis of the drive shaft I with smescheni30 .em 180, i.e. against each other The shoulder of each rotor 13 and 42 bears a pair of moving bodies 43 and 44, 45 and 46 formed by projections, - peripheral 3g whose surface represents the edge of the sphere. The diameter of the spherical edges forming the outer protrusions 43 and 45, designed to interact with the openings 36 and 37 of the gear member 6, corresponds to the diameter of the opening 36 and 37. The spherical edges organ 6, corresponds to the diameter of the nest 36 and 37. Spherical edges internal bolsholes: stupid, 44 and 46, designed to interact with the openings 38 and 39 of the driven, reducer body 7, have a larger diameter and correspond to the diameter of the holes 38 to 39. The gap between the holes 37, 36 and 38, 39 is sufficient to the protrusions of the running bodies could pass through the holes 38, 39 before they began to interact with the holes 36, 37. In the interior of the casing 4, there is a certain amount of oil intended for s.maeki of moving surfaces, podsigigiikov and running bodies during operation of the gearbox. ten shown in FIG. 10 to the position shown in FIG. eleven, The rotor 12 is symbolically represented by a triangle, the tops of which are carried by pairs of moving bodies 15-20. At that moment, when the undercarriage 18 leaves the groove of AND of the supporting gearbox 7 and when the undercarriage 17 leaves the notch 10 of the driven gearbox 6, the undercarriages 15 and 16 enter into the grooves 10 and -1 of the gearboxes 6 and 7, which are located at the previous step of the rotor 12 15 against each other. During the final step, the rotor moves from the position indicated by the solid line to the position indicated by the dotted line. This is achieved due to the instantaneous rotation around the center of the running member 16, trapped in the groove 11. of the supporting reducer member 7. During this turn, only a pair of running members 15 and 16 are in 25 engagement with the gearbox bodies 6 and 7, the undercarriage 16 remains stationary, and its axis serves as the axis of rotation of the rotor 12, while the undercarriage 15 is in engagement 30 with a groove 10 and carries the last of the SRI to the position shown by the bar. The mechanical gearbox works as follows. During the movements of the rotor, 12 pairs of travel bodies 15–20 consistently interact with all slots 10 and II of gear units 6 and 7. At the same time, no more than two pairs of travel members are engaged with slots 10 and 11, while the third pair is free. In the embodiment shown in FIG. In 3 states, the eccentric 13 is carried away in the direction of the Research Institute of the arrow f, a pair of travel bodies 15 and 16 penetrates groove 10 and 1 of gear units 6 and 7, while a pair of travel bodies 19 and 20 comes out of grooves 10 and P, and - hooks 17 and 18 of the head out of the slots 10 and I. When the rotor 12, carried away by the drive shaft I, is transferred from the state shown in FIG. 3, to the state shown in FIG. 4, it simultaneously rotates around the running gear 13, trapped in the groove 10 of the support gear member 6 in which it is located. Such an instantaneous turn leads to the movement of the groove 11 of the driven gear member seized by the driving member 16 in the direction of the arrow g. During the said movement of the rotor 12, the pair of the traveling bodies 19 and 20 discharges from the slots 10 and 11, and at the end of the movement or pitch of the rotor 12, the pair moves 35 10 when it is positioned at the point 15, 10. At this point in time, a certain groove 10 slave gearbox body goes into the polo against some groove 11 of the gearbox 7. The bodies 17 and 18 enter into the grooves IO and 11 at the moment when the running bodies 15 and 16 leave the grooves 10 and 11 interacting with them. During such a single movement or rotor pitch, the angular variation of the driven gear unit 7 in this example is 1/77 revolution. The drive shaft I must make two full turns in order for the other of the arms 14 of the rotor 12 to return to the state shown in FIG. 3 From the states of the respective slots 10 and P in FIG. 3 and 9 it can be seen that the driven gear unit 7 made 1/11 of its turnover in seven consecutive steps. FIG. 21 schematically shows an instantaneous rotation of the rotor, causing one step of the driven gear member 7 when moving from a position. ten 420858 shown in FIG. 10 to the position shown in FIG. eleven, The rotor 12 is symbolically represented by a triangle, the tops of which are carried by pairs of moving bodies 15-20. At that moment, when the undercarriage 18 leaves the groove of AND of the supporting gearbox 7 and when the undercarriage 17 leaves the notch 10 of the driven gearbox 6, the undercarriages 15 and 16 enter into the grooves 10 and -1 of the gearboxes 6 and 7, which are located at the previous step of the rotor 12 15 against each other. During the final step, the rotor moves from the position indicated by the solid line to the position indicated by the dotted line. This is achieved due to the instantaneous rotation around the center of the running member 16, trapped in the groove 11. of the supporting reducer member 7. During this turn, only a pair of running members 15 and 16 are in 25 engagement with the gearbox bodies 6 and 7, the undercarriage 16 remains stationary, and its axis serves as the axis of rotation of the rotor 12, while the undercarriage 15 is in engagement 30 with a groove 10 and carries away the last-. SRI to the position shown by dash 35 10 when it is located at a dotted point 15, 10. At this point in time, a certain groove 10 slave gearbox body goes into the polo 10, when it is positioned opposite a certain groove 11 of the gear unit 7. During the instantaneous rotation of the rotor 12 around the axis of the running body 16, the driven, gear unit 6 moves by an angular value oL. At the moment when the driving device 15 comes to position 15 and is about to leave groove 10, the moving bodies 19 and 20 come to position 19 and 20, ready to engage with the grooves 11. Then, due to the instantaneous rotation of the rotor 12 around the traveling body 20, step out.
权利要求:
Claims (5) [1] Invention Formula step out. 1, A mechanical gearbox containing the drive and drive shafts for rotation with different angular speeds depending on the reduction gear ratio of the gearbox, two coaxial gear units set 91 with the possibility of angular displacement one relative to the other, each of which has a number of drive elements, concentrated and evenly distributed around, the points of rotation of the corresponding gear member and each row has a different number of drive elements, at least one eccentric rotor driven in motion by at least one eccentric, which is made together with the leading v. shaft and I have two groups at the water station, consisting of at least three travel bodies in each, evenly spaced The center of the rotor and placed on the two diameters of the latter for simultaneous interaction of the moving bodies of each group with the drive elements of the corresponding gear unit, and the eccentricity of the rotor is chosen such that each drive body of the rotor has an extreme external position a position in which it is not connected to any drive element, characterized in that, in order to reduce overall dimensions and improve processability, each group of drive bodies has the same number of travel bodies, the travel body of one group is connected to the travel body of another group to form a pair, and the travel bodies of the same pair are installed with the possibility of alignment on the same rotor radius. 2. Reducer POP.1, distinguished by the fact that one of. the gearbox bodies is the supporting [2] and is connected to the housing and the other is connected to the driven shaft. 3. Reducer according to claim 1, characterized in that the number of driving elements of the supporting gear unit is located on a circle on which the drive elements of the driven gear member are located. [3] 4. Reducer under item 1, about tl and - [4] drive elements of the support gear unit N + n N. + X n de v and p 1 X O 2; „ whole numbers; integer; 4 1 ABOUT N Z oh lin the number of drive elements of the driven gear unit; the number of drive elements of the driven gear unit located between two suspension bodies belonging to different pairs of rotor that are in engagement with the gear member body; the cam rotates in the same direction as the driven gear unit; they rotate in different directions, 5. Reducer for paragraphs. 1-5, about tl and - a that the number of input elements of the driven reduction organ [5] II, P Y N, t 1 N + Z N f Z Oh, 11ts.N integer; the cam rotates in the same direction as the driven gear unit; they rotate in different directions. 4 and 5, about t - the fact that re 6. Gearbox for PP gearing N, N and 2; n P 7. Reducer for paragraphs. 1-6, characterized in that it is equipped with at least one additional rotor, the pairs of the last and the main rotor bodies are alternately arranged, and the number of drive elements of at least one gear unit is doubled. 8. Reducer on PP. 1-7, characterized in that the two adjacent pairs of the rotor travel elements are mounted with the possibility of angular displacement one relative to the other. 9. Reducer on PP. 1-6, characterized in that, with one rotor, the number of registered elements of at least one operating organ is odd. 10. The gearbox according to claim 1 or 8, which is characterized by the fact that the drive elements of the support and driven gear units are located in a plane perpendicular to the drive shaft, on one side of the rotor, and the running bodies of this rotor are perpendicular to one of its lateral parties, The gearbox according to claim I or 9, is attributed to the fact that the drive elements of the support and driven reuttor organs are located in planes perpendicular to the drive shaft, on both sides of the rotor, and the single bodies of each pair of rotor are located on opposite sides of this rotor. . 12, Reducer under p. 4 or 5, in that about t- 20 N ; 14 g ten 15 Ni;, 2, 7, oo l and -, What is the main or 13. Reducer for c. due to the fact and the additional rotor is connected to the drive shaft by means of either one eccentric or two - one for each rotor, or concentric with each other, or arranged in series, 14. Reducer according to claim 13, characterized by However, the eccentrics are diametrically opposed. 15, Reducer for PP. 1-6, from the field with the fact that when using several additional rotors on the drive shaft, the appropriate number of eccentrics uniformly distributed around its axis are set to interact with the latter. 16, Reducer for PP. 1-15, characterized in that the reducer bodies are formed by two d 20 concentric cylindrical elements that encircle the rotor or rotors, and the drive elements of the gearbox g bodies are formed by holes. 17. Reducer according to claim 16, characterized in that the holes are round, and the diameter of the holes of the internal gear member is larger than 10 meter hole external gear unit .. 18. Reducer according to claim 17, characterized in that each pair of branch bodies has two coaxial protrusions, the diameters of which correspond to the diameters of the holes, respectively. Kiih gear units. 19. Reducer under item 18, about tl and -. The fact that the peripheral surface of each protrusion is shaped as a segment of a sphere. 20. Reducer according to claim 13, characterized in that the rotors are located in the same plane between the driven gear unit for the interaction of the first row of drive elements with the corresponding driving bodies of the main rotor and the second row of drive elements with the corresponding running bodies of the main rotor, yes drive elements - with the corresponding running bodies of the additional rotor and 35 between the support gear unit for the interaction of one series of drive elements with the corresponding running bodies of both rotors. 21. Reducer on PP. 13, 14 or 15, 40 characterized in that The rotors are located in parallel planes, and the running bodies of each rotor are installed with the ability to interact with the corresponding 5 drive elements of each gear unit. 25 thirty 13 Table 1 View 12 1442085 14 table 2 ten but i5 iO 15 Fiz.9 Fi $. FIG. eleven nineteen S FIG. 78 sixteen Yu Fig.20 Fig.yy, Yu: 75 G / 7s 11 G6 eleven 23 25 X nineteen P FIG. ge Figg vidb GB FIG. 25 Jf .g ffS 56 55 V6 Fi $. B8 sy Fi.29
类似技术:
公开号 | 公开日 | 专利标题 SU1442085A3|1988-11-30|Mechanical reduction gear KR920000037B1|1992-01-06|Gearing machanism CA1234709A|1988-04-05|Planetary gear box with double eccentrics EP0255323B1|1991-04-10|Differential planetary gear apparatus US3783712A|1974-01-08|High ratio frictionless speed reductor EP0037287B1|1985-05-08|Motion-transmitting devices and toothed wheels for use therein US3258994A|1966-07-05|Speed changing device JPH11508675A|1999-07-27|Compact gear transmission with large gear ratio KR900002005A|1990-02-28|Variable speed differential US2884815A|1959-05-05|Rotary speed changer US4843911A|1989-07-04|Speed reducing or increasing planetary gear apparatus US4173906A|1979-11-13|Planetary gear US5123882A|1992-06-23|Compound planocentric cycloidal gear drives with orthogonal planet arrangements US3203262A|1965-08-31|Limited multiple turn rotary mechanism US4543841A|1985-10-01|Power Machine KR100294461B1|2001-10-24|Reduction gear composed of planetary gear and differential gear set US1277193A|1918-08-27|Power-transmission gear. WO2021166539A1|2021-08-26|Transmission mechanism SU1677425A1|1991-09-15|Continuous rotation-to-oscillation planetary converter EP3816481A1|2021-05-05|Compact compound harmonic drive assembly KR100454761B1|2004-11-05|Backlash Adjustable Planetary Gear Reducer SU1569469A1|1990-06-07|Device for conversion of rotary motion CN101334093A|2008-12-31|Retarding mechanism RU2154759C1|2000-08-20|Mechanical transmission by engagement at variable gear ratios KR0185811B1|1999-04-01|Epicycle reduction gear using phase displacement
同族专利:
公开号 | 公开日 EP0155497A1|1985-09-25| US4699023A|1987-10-13| BR8500884A|1985-10-15| HK14793A|1993-03-05| ES540896A0|1985-12-01| JPS60188653A|1985-09-26| ES8603045A1|1985-12-01| CH655554B|1986-04-30| DE3561116D1|1988-01-14| DE155497T1|1985-12-19| KR930007003B1|1993-07-26| CA1225259A|1987-08-11| JPH0573936B2|1993-10-15| US4841811A|1989-06-27| AT31206T|1987-12-15| DD232963A5|1986-02-12| EP0155497B1|1987-12-02| KR850006590A|1985-10-14|
引用文献:
公开号 | 申请日 | 公开日 | 申请人 | 专利标题 RU2626422C1|2016-07-05|2017-07-27|Валерий Александрович Мухин|Orbital gearbox|DE127529C|1900-07-10| DE312164C| US24288A|1859-06-07|Chain pump | USRE24288E|1957-03-19|Speed changing device | US404958A|1889-06-11|Differential hoisting mechanism | US702793A|1900-12-03|1902-06-17|Carl Heinrich Otto Hamann|Differential gearing.| CH142829A|1928-12-03|1930-10-15|Deckel Fa Friedrich|Transmission gear.| US2750814A|1951-10-30|1956-06-19|Wildhaber | US2884815A|1956-02-23|1959-05-05|Globe Ind Inc|Rotary speed changer| US3190149A|1962-10-05|1965-06-22|Alex M Gorfin|Speed reduction drive mechanism| US3472097A|1966-03-21|1969-10-14|Paul Huska|Reversible speed reducer| US3427901A|1966-10-14|1969-02-18|Ernest Wildhaber|Gearing| GB1359655A|1970-08-01|1974-07-10|Leeson P G|Speed changing mechanisms| DE2332842A1|1973-06-28|1975-01-16|Julius Leiter|Reduction gear for machine drives - for constant speed and low noise, has two coupled differential gears| GB1519588A|1974-08-02|1978-08-02|Precision Mechanical Dev|Motion transmiting devices| JPS5342865B2|1975-10-22|1978-11-15| IE51023B1|1980-04-02|1986-09-03|Precision Mechanical Dev|Motion transmitting devices having a toothed wheel and independently movable meshing elements| US4429595A|1980-10-23|1984-02-07|Emerson Electric Co.|Motion transmitting device| JP5250457B2|2009-03-13|2013-07-31|日立オムロンターミナルソリューションズ株式会社|Identification device, paper sheet handling device, automatic cash transaction device, and abnormality detection method|US5351568A|1993-03-19|1994-10-04|Core Industries, Inc.|Rotary speed changing apparatus| DE19849987A1|1998-10-29|2000-05-04|Takata Europ Gmbh|Harmonic reduction gear and seat belt device in motor vehicles with such a reduction gear| US6336502B1|1999-08-09|2002-01-08|Halliburton Energy Services, Inc.|Slow rotating tool with gear reducer| DE20012444U1|2000-07-18|2001-08-23|Kuka Roboter Gmbh|Gear, especially for a robot| JP3849918B2|2000-12-04|2006-11-22|株式会社東京精密|Wafer polishing equipment| US6458058B1|2001-02-28|2002-10-01|Chun-Fa Fu|Speed reducer in a portable electric tool| US20090068034A1|2007-09-12|2009-03-12|Pumptec, Inc.|Pumping system with precise ratio output| US9316216B1|2012-03-28|2016-04-19|Pumptec, Inc.|Proportioning pump, control systems and applicator apparatus| US9856968B2|2013-11-10|2018-01-02|II Thurman Tyus|Automatic transmission device| WO2016146927A1|2015-03-16|2016-09-22|Mip Robotics|Movement transmission device, in particular for a robot arm| FR3033861A1|2015-03-16|2016-09-23|Franck Olivier Loriot|MOVEMENT TRANSMISSION DEVICE FOR USE PRINCIPALLY IN A ROBOT ARM| US10760557B1|2016-05-06|2020-09-01|Pumptec, Inc.|High efficiency, high pressure pump suitable for remote installations and solar power sources| US10823160B1|2017-01-12|2020-11-03|Pumptec Inc.|Compact pump with reduced vibration and reduced thermal degradation|
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申请号 | 申请日 | 专利标题 CH103984A|CH655554B|1984-03-02|1984-03-02| 相关专利
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