rotary lobe pump

(1) performance parameters : 1. Flow : Q=500 liters / hour ~14,000 liters / 2 .hours. O.2CP~500,000CP three areas : transportation viscosity.3.Export : 0.8-1.0Mpa maximum pressure (high viscosity) 4. Product temperature from -30 ℃ -150 ℃ 5. Model TR - I-1 aircraft models allocated variable speed drive, I said. II expressed frequency electrical distribution, allocation III said fixed speed gear reducer. TR : no need to pump rotor, rotor pump of combined TRA said. (B) parameters :

 

NO	Model	volume of rotor（L）	range of speed（rpm）	Flow （L/h）	Type I,II power spply（Kw）	Type Ⅲpower spply （Kw）	suction and discharge（mm）
1	TRA-I-05	0.028	200-500	330-840	0.55	0.37	25
2	TRA-I-1	0.04	200-500	480-1200	0.55	0.37	25
3	TRA-I-2	0.075	200-400	900-1800	0.75	0.55	25
4	TRA-I-3	0.095	200-400	1140-2280	1.1	0.75	32
5	TRA-I-4	0.118	200-400	1400-2800	1.5	1.1	38
6	TRA-I-5	0.18	200-400	2000-4000	2.2	1.5	38
7	TRA-I-6	0.28	200-400	3000-6000	3	2.2	50
8	TRA-I-7	0.34	200-400	3600-7200	4	3	50
9	TRA-I-8	0.424	200-400	4500-9000	5.5	4	50
10	TRA-I-9	0.53	200-400	5700-11000	7.5	5.5	63.5(50)
11	TRA-I-10	0.7	200-400	7000-14000	7.5	5.5	63.5(50)
12	TRA-I-11	1.0	200-400	12000-24000	11	7.5	89
13	TRA-I-12	1.6	200-400	19000-38000	11	11	89
14	TRA-I-13	2.0	200-400	24000-48000	15	11	108