石油机械
石油機械
석유궤계
China Petroleum Machinery
2015年
10期
1-4
,共4页
张友军%于东兵%张炎%胡强法%陈智
張友軍%于東兵%張炎%鬍彊法%陳智
장우군%우동병%장염%호강법%진지
喷射钻井%径向井%喷嘴%流量分配%自动调节
噴射鑽井%徑嚮井%噴嘴%流量分配%自動調節
분사찬정%경향정%분취%류량분배%자동조절
jet drilling%radial horizontal well%nozzle%flow distribution%automatic adjustment
针对常规自进式喷嘴在水射流径向钻井时可能出现破岩钻孔能力或自牵引驱动力不足的问题,设计了自动调节流量分配的喷嘴。该喷嘴由前向喷嘴、后向喷嘴、探头和节流调节盘组成,探头和调节盘可根据钻进是否遇阻自动调节前、后向流量分配,实现喷嘴在正常钻进和遇阻情况下牵引力和破岩钻孔能力转换。在对喷嘴进行参数设计和对节流调节盘做受力分析后,测试了喷嘴的前、后向流量分配及牵引力、节流盘启动特性和流量自动调节效果等。试验结果表明,在钻进遇阻时,喷嘴前向流量可增加6?7%以上,这说明其自动调节流量分配原理可行,结构参数合理,但样机前、后向流量系数分别只有0?60和0?75,效率偏低,因此喷嘴结构尚需优化。
針對常規自進式噴嘴在水射流徑嚮鑽井時可能齣現破巖鑽孔能力或自牽引驅動力不足的問題,設計瞭自動調節流量分配的噴嘴。該噴嘴由前嚮噴嘴、後嚮噴嘴、探頭和節流調節盤組成,探頭和調節盤可根據鑽進是否遇阻自動調節前、後嚮流量分配,實現噴嘴在正常鑽進和遇阻情況下牽引力和破巖鑽孔能力轉換。在對噴嘴進行參數設計和對節流調節盤做受力分析後,測試瞭噴嘴的前、後嚮流量分配及牽引力、節流盤啟動特性和流量自動調節效果等。試驗結果錶明,在鑽進遇阻時,噴嘴前嚮流量可增加6?7%以上,這說明其自動調節流量分配原理可行,結構參數閤理,但樣機前、後嚮流量繫數分彆隻有0?60和0?75,效率偏低,因此噴嘴結構尚需優化。
침대상규자진식분취재수사류경향찬정시가능출현파암찬공능력혹자견인구동력불족적문제,설계료자동조절류량분배적분취。해분취유전향분취、후향분취、탐두화절류조절반조성,탐두화조절반가근거찬진시부우조자동조절전、후향류량분배,실현분취재정상찬진화우조정황하견인력화파암찬공능력전환。재대분취진행삼수설계화대절류조절반주수력분석후,측시료분취적전、후향류량분배급견인력、절류반계동특성화류량자동조절효과등。시험결과표명,재찬진우조시,분취전향류량가증가6?7%이상,저설명기자동조절류량분배원리가행,결구삼수합리,단양궤전、후향류량계수분별지유0?60화0?75,효솔편저,인차분취결구상수우화。
To address the issues of conventional self?feeding nozzle during radial horizontal drilling like low drilling capacity and low self?traction driving force, an automatic flow distribution nozzle has been designed?The nozzle is mainly composed of front and back nozzle probe and throttle plate?The nozzle probe and throttle plate could automatically distribute the front and back flow according to whether drilling difficulty is encountered, achie?ving the conversion of traction force and hydraulic drilling force in the case of normal drilling and drilling difficul?ty?Performance test has been conducted on the nozzle prototype after the nozzle parameters design and the stress a?nalysis of the throttle plate?The test has been focused on the front and back nozzle flow distribution, traction, throttle plate starting characteristic and the automatic flow distribution performance?The results showed that when the drilling difficulty is encountered, the front jet nozzle flow could increase 6?7%, thus indicating a feasible auto?matic flow distribution principle and reasonable structure parameters?But the prototype have low front and back flow coefficient of only 0?60 and 0?75, so further optimization need to be done on the nozzle structure.