SU802830A1 - Method of determining unbalanace value of cabin-lift counterweight system - Google Patents
Method of determining unbalanace value of cabin-lift counterweight system Download PDFInfo
- Publication number
- SU802830A1 SU802830A1 SU782631935A SU2631935A SU802830A1 SU 802830 A1 SU802830 A1 SU 802830A1 SU 782631935 A SU782631935 A SU 782631935A SU 2631935 A SU2631935 A SU 2631935A SU 802830 A1 SU802830 A1 SU 802830A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- counterweight
- cabin
- amount
- determining
- efforts
- Prior art date
Links
Landscapes
- Testing Of Balance (AREA)
Description
jOU Сначала усили прикладывают и заме .р ют со стороны противовеса при порожней кабине. Усили Pj создают вращением муфты талрепа 5 и фиксируют динамометром 6. Противовес лифта всегда т желее порожней кабины, поэтому при измерении усили Р., зуб черв чного колеса 10 опираетс на зуб черв ка 11. При вращении талрепа усилие с канатоведущего шкива через тихоходный вал редуктора передаетс на черв чное колесо 10 по часовой стрелке. В начале вращени талрепа усилие возрастает до момента отрыва зуба черв чного колеса от зуба черв ка. После по влени кинематического разрыва в передаче точка а на зубе черв чного колеса перейдет в положение Oi, пройд угол ф.При этом усилие на динамометре будет посто нным и может быть легко зафиксировано. После поворота черв чного колеса на угол ф показание динамометра резко возрастает, что свидетельствует о полном выборе зазора в зацеплении. Аналогично прикладывают и замер ют усилие со стороны кабины, предварительно загруженной номинальным грузом. Обозначив массу кабины К, номинальную массу Q, величину потерь в шахте F и прин в номинальный вес противовеса К + 0,5, получим PI 0.5Q А + F; р, 0,5Q + А + F; где Д -величина неуравновешенности сиетемы Отсюда А -. F . Предложенный способ определени величины неуравновешенности системы кабиФиг . 1 80jOU At first, the forces are applied and replaced by the counterweight with an empty cabin. The forces Pj are created by rotating the lanyard coupling 5 and fixed with a dynamometer 6. The elevator counterweight is always heavier than the empty cabin, therefore when measuring the force R, the tooth of the worm gear 10 rests on the tooth of the worm 11. When the lanyard is rotating, the force from the cable driving pulley through the low-speed gearbox is transmitted to the worm wheel 10 clockwise. At the start of rotation of the turnbuckle, the force increases until the moment when the tooth of the worm wheel is torn off the tooth of the screw. After the occurrence of a kinematic discontinuity in the transmission, the point a on the tooth of the worm gear will change to the position Oi, the angle f has passed. At the same time, the force on the dynamometer will be constant and can be easily fixed. After the worm gear rotates by an angle, the reading of the dynamometer increases sharply, which indicates a complete choice of the gap in the engagement. Similarly, force is applied and measured from the side of the cabin, which is preloaded with a nominal load. Denoting the cab mass K, the nominal mass Q, the value of losses in the shaft F and having received the nominal weight of the counterweight K + 0.5, we get PI 0.5Q A + F; p, 0.5Q + A + F; where D is the value of imbalance in the sietema. From here, A -. F. The proposed method for determining the imbalance of the cabi figure system. 1 80
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Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU782631935A SU802830A1 (en) | 1978-06-21 | 1978-06-21 | Method of determining unbalanace value of cabin-lift counterweight system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU782631935A SU802830A1 (en) | 1978-06-21 | 1978-06-21 | Method of determining unbalanace value of cabin-lift counterweight system |
Publications (1)
Publication Number | Publication Date |
---|---|
SU802830A1 true SU802830A1 (en) | 1981-02-07 |
Family
ID=20771535
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU782631935A SU802830A1 (en) | 1978-06-21 | 1978-06-21 | Method of determining unbalanace value of cabin-lift counterweight system |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU802830A1 (en) |
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1978
- 1978-06-21 SU SU782631935A patent/SU802830A1/en active
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