SU518584A1 - Satellite bearing unit - Google Patents

Satellite bearing unit

Info

Publication number
SU518584A1
SU518584A1 SU2039351A SU2039351A SU518584A1 SU 518584 A1 SU518584 A1 SU 518584A1 SU 2039351 A SU2039351 A SU 2039351A SU 2039351 A SU2039351 A SU 2039351A SU 518584 A1 SU518584 A1 SU 518584A1
Authority
SU
USSR - Soviet Union
Prior art keywords
satellite
bearing
bearing unit
diameter
axis
Prior art date
Application number
SU2039351A
Other languages
Russian (ru)
Inventor
Владимир Модестович Ястребов
Федор Иванович Плеханов
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed filed Critical
Priority to SU2039351A priority Critical patent/SU518584A1/en
Application granted granted Critical
Publication of SU518584A1 publication Critical patent/SU518584A1/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C19/00—Bearings with rolling contact, for exclusively rotary movement
    • F16C19/54—Systems consisting of a plurality of bearings with rolling friction
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C25/00—Bearings for exclusively rotary movement adjustable for wear or play
    • F16C25/06—Ball or roller bearings
    • F16C25/08—Ball or roller bearings self-adjusting
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C35/00—Rigid support of bearing units; Housings, e.g. caps, covers
    • F16C35/04—Rigid support of bearing units; Housings, e.g. caps, covers in the case of ball or roller bearings
    • F16C35/06—Mounting or dismounting of ball or roller bearings; Fixing them onto shaft or in housing
    • F16C35/063—Fixing them on the shaft
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2361/00—Apparatus or articles in engineering in general
    • F16C2361/61—Toothed gear systems, e.g. support of pinion shafts

Description

(54) ПОДШИПНИКОВЫЙ УЗЕЛ САТЕЛЛИТА(54) BEARING KNOT OF SATELLITE

«bix прокладок 7 и ша1 йков 8, установленных в углублени х, выполненных в центре лысюк оси 1 и вкладышей 3. Ось выполне- аа в месте посадки подшипнаков диаметром, меньшим диаметра внутреннего кольца подшипника , дл  обеспечени  требуемого углового леремещени  сателлита и устанавливгеf )TCH в щеки водила так, что плоскость ее симметрии, дел шд  ось между лысками на две части, имеет по отношению к водилу радиальное нагфавление. ;"Bix gaskets 7 and shafts 8 installed in recesses made in the center of the cooler of axle 1 and liners 3. The axis is made at the landing site of bearings with a diameter smaller than the diameter of the inner ring of the bearing to ensure the required angular displacement of the satellite and the installation of ge) in the cheek drove so that the plane of its symmetry, the axis of the ax between the flats, in two parts, has in relation to the carrier a radial inscription. ;

В результате не-ючностей изготовлени  и монтажа передачи возникает неравномерность распределешш нагрузки по ширине ау&чатых венцов, то приводит к по влению по . в6рачива{ошего|сагаллит 5 момента. Так как сателлит установлен на по.111 ипниках 4, которые , в свою очередь, гпосажены на вкладыши 3, имеющие возмогкность углового перемещени , то под действием поворачивающее FO моменту сателлит самоустанавливаетс  и занимает такое положение, при котором нагрузка распредел етс  равномерно. Шарики 8 пр штствуют линейным перемещени мAs a result of the inadequacies of the manufacture and assembly of the transmission, an uneven distribution of the load over the width of ay & crowns occurs, this results in appearance. Vrachatcha {Osho | Sagallit 5 points. Since the satellite is mounted on po.111 ipnik 4, which, in turn, is mounted on inserts 3 having the possibility of angular displacement, under the action of the FO turning point, the satellite self-adjusts and takes such a position that the load is distributed evenly. 8 balls with linear displacement

Claims (1)

сателлита в радиальном и осевом направлени х ,5 Формула изобретени satellite in radial and axial directions, 5 claims Подшипниковый узел сателлита редуктора , состо щий из оси, снабженной двум  расположенными симметрично лысками, с установленным на ней посредством подшипников качени  сателлитом, о т л и ч а ющ и и с   тем, что, с целью обеспечени  выравнивани  нагрузки по ширине зубчатого венца сателлита, подшипниковый узел снабжен взаимодействующими с внутрен1гчми опорными поверхност ми колец подшипников сегментньгми вкладьпиами, контактирующими своими плоскост ми с лысками оси, а также иарикам , к -ждый из которых установлен в выюлненньк в центре упом нутых лыс ок и плоско гей сегментных вкладышей углубл- ни х, распоюженных друг против друга, причем диаметр оси в месте посадки подшипников меньше диаметра их внутренних опорных поверхаое - j тей.The satellite bearing of the reducer, consisting of an axis equipped with two symmetrically arranged flats, mounted on it by means of rolling bearings of the satellite, is required so as to ensure that the load is equalized over the width of the gear ring of the satellite, the bearing unit is equipped with interacting with the internal bearing surfaces of the bearing rings with segmented inserts that contact their planes with the axial rails, as well as to the radar bearings, each of which is installed in the center of the pack washed bald heads and flat segmented liners of the recesses located opposite each other, and the diameter of the axis at the bearing seat is less than the diameter of their internal bearing surfaces — j tey. -rl-rl 0f/f. /0f / f. / А- fiA-fi 8eight Фиг ZFig z
SU2039351A 1974-07-02 1974-07-02 Satellite bearing unit SU518584A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU2039351A SU518584A1 (en) 1974-07-02 1974-07-02 Satellite bearing unit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU2039351A SU518584A1 (en) 1974-07-02 1974-07-02 Satellite bearing unit

Publications (1)

Publication Number Publication Date
SU518584A1 true SU518584A1 (en) 1976-06-25

Family

ID=20589471

Family Applications (1)

Application Number Title Priority Date Filing Date
SU2039351A SU518584A1 (en) 1974-07-02 1974-07-02 Satellite bearing unit

Country Status (1)

Country Link
SU (1) SU518584A1 (en)

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