CN103670269A - Turbine torsional impact generator - Google Patents

Turbine torsional impact generator Download PDF

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CN103670269A
CN103670269A CN201310698227.3A CN201310698227A CN103670269A CN 103670269 A CN103670269 A CN 103670269A CN 201310698227 A CN201310698227 A CN 201310698227A CN 103670269 A CN103670269 A CN 103670269A
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impact
sleeve
turbine
transmission
claw
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CN103670269B (en
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宋洵成
李同同
管志川
许海超
陆桃妹
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SICHUAN CHUANSHI DIAMOND BIT CO Ltd
China University of Petroleum East China
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China University of Petroleum East China
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Abstract

本发明公开了一种涡轮扭转冲击发生器,其包括转换接头、外壳、涡轮、定轴、传动套、冲击爪、冲击架、传动轴和钻头套筒,外壳上端连接转换接头,外壳下端连接钻头套筒,涡轮转子固定在定轴上,涡轮定子固定在外壳上,定轴和传动套通过花键配合,传动套安装在冲击架上端,冲击架下端安装端盖,传动轴安装在传动套和端盖上,冲击爪安装在冲击架上。涡轮带动定轴旋转,定轴通过花键带动传动套旋转,传动套拨动冲击爪,冲击爪带动冲击架高速旋转,在旋转过程中冲击爪和传动套作用并周期性地冲击传动轴,形成高频扭转冲击,传动轴将获得的高频冲击能量传递到钻头套筒上,钻头套筒带动钻头脉动地冲击地层岩石。本发明可实现大冲击功,扭冲能量利用率高。

Figure 201310698227

The invention discloses a turbine torsional impact generator, which comprises a conversion joint, a housing, a turbine, a fixed shaft, a transmission sleeve, an impact claw, an impact frame, a transmission shaft and a drill bit sleeve, the upper end of the housing is connected with the conversion joint, and the lower end of the housing is connected with the drill bit The sleeve, the turbine rotor is fixed on the fixed shaft, the turbine stator is fixed on the casing, the fixed shaft and the transmission sleeve are matched by splines, the transmission sleeve is installed on the upper end of the impact frame, the end cover is installed on the lower end of the impact frame, and the transmission shaft is installed on the transmission sleeve and On the end cap, the impact claws are mounted on the impact frame. The turbine drives the fixed shaft to rotate, and the fixed shaft drives the transmission sleeve to rotate through the spline. The transmission sleeve moves the impact claw, and the impact claw drives the impact frame to rotate at high speed. During the rotation process, the impact claw and the transmission sleeve interact and periodically impact the transmission shaft, forming High-frequency torsional impact, the drive shaft transfers the high-frequency impact energy obtained to the drill bit sleeve, and the drill bit sleeve drives the drill bit to impact the formation rock in a pulsating manner. The invention can realize large impact energy and high utilization rate of torsional impulse energy.

Figure 201310698227

Description

涡轮扭转冲击发生器Turbine Torsional Impact Generator

技术领域technical field

本发明涉及石油天然气勘探开发过程中提高深部硬地层钻井速度的工具,具体地说是涉及一种涡轮扭转冲击发生器。The invention relates to a tool for increasing the drilling speed in deep hard formations during oil and gas exploration and development, in particular to a turbine torsional impact generator.

背景技术Background technique

当前,我国陆地油气勘探开发呈现出由东向西并向深井超深井发展的趋势,与此同时,海洋油气勘探开发由滩海与浅海逐步转向深海。随着油气勘探逐步向深部地层及深海域发展,钻井操作面临越来越复杂的地层环境及钻进工艺难题,勘探开采难度不断加大。在深井超深井的钻进过程中,随着井深的增加,岩石硬度及塑性增大,研磨性增强,可钻性变差,下部钻具粘滑振动剧烈。钻具的粘滑振动现象不但造成机械钻速降低,还可能造成井下事故的发生,严重影响油气勘探开发的进行。At present, my country's onshore oil and gas exploration and development is showing a trend of developing from east to west and toward deep wells and ultra-deep wells. At the same time, offshore oil and gas exploration and development are gradually shifting from shallow seas and shallow seas to deep seas. With the gradual development of oil and gas exploration to deep formations and deep sea areas, drilling operations are faced with increasingly complex formation environments and drilling technology problems, making exploration and production more and more difficult. During the drilling process of deep and ultra-deep wells, with the increase of well depth, the hardness and plasticity of the rock increase, the abrasiveness increases, the drillability becomes poor, and the stick-slip vibration of the lower drilling tool is severe. The stick-slip vibration phenomenon of drilling tools not only reduces the ROP, but also may cause downhole accidents, seriously affecting the progress of oil and gas exploration and development.

扭转冲击钻井是一种新兴的高效钻井技术,它正是基于减缓甚至抑制下部钻具的粘滑振动而发展起来的。扭转冲击钻井是指在常规钻井的基础之上在PDC钻头的上方增设一个扭转冲击钻井工具用于给钻头提供周期性的低幅高频扭向冲击的钻井技术。冲击器对钻头产生的周期性高频冲击,可以大幅度减少或消除PDC钻头的粘滑振动,在提高机械钻速的同时,能够保护钻头,延长钻头寿命,减少起下钻次数,有效降低了钻井成本。Torsional percussion drilling is an emerging high-efficiency drilling technology, which is developed based on slowing down or even suppressing the stick-slip vibration of the lower drilling tool. Torsional percussion drilling refers to a drilling technique in which a torsional percussion drilling tool is added above the PDC bit to provide periodic low-amplitude high-frequency torsional percussion to the drill bit on the basis of conventional drilling. The periodic high-frequency impact of the impactor on the drill bit can greatly reduce or eliminate the stick-slip vibration of the PDC drill bit. While increasing the mechanical drilling speed, it can protect the drill bit, prolong the life of the drill bit, reduce the number of trips, and effectively reduce the Drilling costs.

目前,存在的扭力冲击器虽然能够实现高频的扭转冲击,但是存在很多缺陷,比如,(1)冲击结构设计不合理,导致单次冲击功小,且冲击副寿命不高;(2)不存在储能元件,使得扭冲能量利用率较低;(3)现有的扭力冲击器自身不带有稳定器;(4)涡轮叶片型线设计不合理,钻井液能量转化率低,导致扭冲工具工作性能不佳。At present, although the existing torsion impactor can achieve high-frequency torsional impact, there are many defects, for example, (1) the design of the impact structure is unreasonable, resulting in a small single impact energy, and the life of the impact pair is not high; (2) The existence of energy storage elements makes the utilization rate of torsional impulse energy low; (3) the existing torsional impactor itself does not have a stabilizer; (4) the design of the turbine blade profile is unreasonable, and the energy conversion rate of drilling fluid is low, resulting in torsional impact. Punching tool does not work well.

发明内容Contents of the invention

针对以上缺陷,本发明设计了一种涡轮扭转冲击发生器。Aiming at the above defects, the present invention designs a turbine torsional impact generator.

本发明所采用的技术解决方案是:The technical solution adopted in the present invention is:

一种涡轮扭转冲击发生器,包括转换接头、外壳、涡轮、定轴、传动套、冲击爪、冲击架、传动轴和钻头套筒,外壳上端连接转换接头,外壳下端连接钻头套筒,涡轮转子固定在定轴上,涡轮定子固定在外壳上,定轴和传动套通过花键配合,传动套安装在冲击架上端,冲击架下端安装端盖,传动轴安装在传动套和端盖上,冲击爪安装在冲击架上;定轴下端设置有挡盘,定轴上设置有侧流道,钻井液经转换接头进入外壳内,流经涡轮到达挡盘,然后上返至定轴侧流道,汇聚到定轴的主流道,然后经传动套进入传动轴,继续向下流入钻头套筒;钻井液启动涡轮,涡轮转子高速旋转,带动定轴高速旋转,定轴带动传动套旋转,传动套上开设有U形口,冲击爪包括方形部、爪扣部和连接部,方形部与U形口相配合,连接部为圆柱形,在冲击架上设置有条形槽,冲击爪的连接部卡入条形槽中,冲击爪可相对于冲击架小角度旋转,在传动轴上设置有与爪扣部相配合的爪扣槽,传动套转动时通过U形口拨动冲击爪方形部,带动冲击爪和冲击架转动,冲击爪周期性的冲击传动轴。A turbine torsional impact generator, including a conversion joint, a housing, a turbine, a fixed shaft, a transmission sleeve, an impact claw, an impact frame, a transmission shaft and a drill sleeve, the upper end of the housing is connected to the conversion joint, the lower end of the housing is connected to the drill sleeve, and the turbine rotor Fixed on the fixed shaft, the turbine stator is fixed on the casing, the fixed shaft and the transmission sleeve are matched by splines, the transmission sleeve is installed on the upper end of the impact frame, the end cover is installed on the lower end of the impact frame, the transmission shaft is installed on the transmission sleeve and the end cover, and the impact The jaws are installed on the impact frame; the lower end of the fixed shaft is provided with a baffle plate, and the fixed shaft is provided with a side channel. The drilling fluid enters the casing through the conversion joint, flows through the turbine to the baffle plate, and then returns to the side channel of the fixed shaft. Converge to the main channel of the fixed shaft, then enter the transmission shaft through the transmission sleeve, and continue to flow down into the drill bit sleeve; the drilling fluid starts the turbine, the turbine rotor rotates at high speed, drives the fixed shaft to rotate at high speed, the fixed shaft drives the transmission sleeve to rotate, and the transmission sleeve There is a U-shaped mouth. The impact claw includes a square part, a claw buckle part and a connecting part. The square part matches the U-shaped mouth. The connecting part is cylindrical. Into the bar-shaped groove, the impact claw can rotate at a small angle relative to the impact frame. A claw buckle groove that matches the claw buckle is provided on the transmission shaft. When the transmission sleeve rotates, the square part of the impact claw is moved through the U-shaped mouth to drive The impact claw and the impact frame rotate, and the impact claw periodically impacts the transmission shaft.

优选的,在外壳侧壁上均布四个刚性稳定器,所述刚性稳定器为长型螺旋叶片型。Preferably, four rigid stabilizers are evenly distributed on the side wall of the casing, and the rigid stabilizers are in the shape of long helical blades.

优选的,所述转换接头一端为连接钻铤的公扣,另一端为连接外壳的公扣;外壳上端为连接转换接头的母扣,外壳下端均布有四个45度的外壳花键,形成四个45度的外壳花键槽;在钻头套筒上有四个40度的花键环绕排列在钻头套筒端面上,形成四个50度的钻头套筒花键槽,外壳花键与钻头套筒花键槽形成间隙配合。Preferably, one end of the conversion joint is a male buckle connected to the drill collar, and the other end is a male buckle connected to the housing; the upper end of the housing is a female buckle connected to the conversion joint, and four 45-degree housing splines are evenly distributed on the lower end of the housing, forming Four 45-degree housing spline grooves; on the drill sleeve, there are four 40-degree splines arranged around the end face of the drill sleeve to form four 50-degree drill sleeve spline grooves, the housing splines and the drill sleeve The spline groove creates a loose fit.

优选的,所述定轴下部设置有台肩,侧面设置有半圆条形凸台,上部安装钢套,涡轮转子通过台肩、凸台和钢套定位,压盘安装在钢套上,二者为滑动连接,端帽和定轴通过螺纹连接将涡轮转子固定在定轴上;所述涡轮定子下部通过定位套定位,定位套座在挡盘上,挡盘座在外壳内壁的台肩上,涡轮定子上部通过压盘和转换接头固定在外壳上。Preferably, the lower part of the fixed shaft is provided with a shoulder, and the side is provided with a semicircular bar-shaped boss, and a steel sleeve is installed on the upper part, the turbine rotor is positioned through the shoulder, the boss and the steel sleeve, and the pressure plate is installed on the steel sleeve. For sliding connection, the end cap and the fixed shaft are threaded to fix the turbine rotor on the fixed shaft; the lower part of the turbine stator is positioned by a positioning sleeve, the positioning sleeve is seated on the baffle plate, and the baffle plate is seated on the shoulder of the inner wall of the housing. The upper part of the turbine stator is fixed on the casing through a pressure plate and a conversion joint.

优选的,所述外壳内壁上开设有凹槽,在凹槽内固定承压轴承,所述冲击架端盖和传动轴座在承压轴承上。Preferably, a groove is formed on the inner wall of the housing, and a pressure bearing is fixed in the groove, and the end cover of the impact frame and the transmission shaft are seated on the pressure bearing.

优选的,所述传动轴和钻头套筒通过螺纹连接,在钻头套筒上开设方形沟槽,在沟槽中安放两个半圆环形防掉挡圈,在外壳下端周向开设四个螺纹孔,在螺纹孔中装入防掉螺杆,防掉挡圈和防掉螺杆通过螺纹连接。Preferably, the drive shaft and the drill sleeve are threadedly connected, a square groove is provided on the drill sleeve, two semi-circular anti-drop retaining rings are placed in the groove, and four threaded holes are provided in the circumferential direction of the lower end of the shell. The anti-drop screw rod is loaded into the threaded hole, and the anti-drop retaining ring and the anti-drop screw rod are threadedly connected.

本发明的有益技术效果是:The beneficial technical effect of the present invention is:

(1)本发明合理设计了扭转冲击结构,在实现大冲击功的前提下,储能元件即冲击架能够将两次冲击间隔内涡轮产生的扭矩能量储存起来,在下一次冲击时完全释放,从而提高间隔内扭冲能量的利用率;(1) The present invention rationally designs the torsional impact structure. Under the premise of realizing large impact energy, the energy storage element, namely the impact frame, can store the torque energy generated by the turbine in the interval between two impacts and release it completely during the next impact, thereby Improve the utilization rate of torsional impulse energy in the interval;

(2)本发明在外壳外面设计自带稳定器,在提速快打的同时还能起到防斜作用,保证井身质量;(2) The present invention is designed with a built-in stabilizer on the outside of the casing, which can also play a role in preventing inclination while increasing the speed and fast drilling, so as to ensure the quality of the shaft;

(3)本发明在外壳下端设置便于拆卸的防掉挡圈和防掉螺杆,在传动轴钻头套筒螺纹连接的同时,对钻头套筒起到双保险作用,提高了钻井的安全性;(3) In the present invention, an anti-drop retaining ring and an anti-drop screw rod are provided at the lower end of the shell for easy disassembly, and at the same time as the drive shaft drill sleeve is threaded, it plays a double insurance role for the drill sleeve and improves the safety of drilling;

(4)本发明工作性能好,能量转化率高,使用寿命长。(4) The invention has good working performance, high energy conversion rate and long service life.

附图说明Description of drawings

下面结合附图与具体实施方式对本发明作进一步说明:Below in conjunction with accompanying drawing and specific embodiment the present invention will be further described:

图1为本发明的结构原理示意图;Fig. 1 is the structural principle schematic diagram of the present invention;

图2为图1的A-A视图;Fig. 2 is the A-A view of Fig. 1;

图3为图1的B-B视图;Fig. 3 is the B-B view of Fig. 1;

图4为图1的C-C视图;Fig. 4 is the C-C view of Fig. 1;

图5为图1的D-D视图;Fig. 5 is the D-D view of Fig. 1;

图6为图1的E-E视图;Fig. 6 is the E-E view of Fig. 1;

图7为本发明的外部结构示意图;Fig. 7 is a schematic diagram of the external structure of the present invention;

图8为图7的F-F视图;Fig. 8 is the F-F view of Fig. 7;

图9为图7的G-G视图;Fig. 9 is the G-G view of Fig. 7;

图10为涡轮定子叶型图;Figure 10 is a turbine stator vane profile;

图11为涡轮转子叶型图;Figure 11 is a turbine rotor blade profile;

图12为传动套的结构示意图;Figure 12 is a schematic structural view of the drive sleeve;

图13为冲击爪的结构示意图;Figure 13 is a schematic structural view of the impact claw;

图14为冲击架的结构示意图;Figure 14 is a schematic structural view of the impact frame;

图15为传动轴的结构示意图。Fig. 15 is a structural schematic diagram of the transmission shaft.

图中:1-转换接头,2-外壳,3-涡轮转子,4-涡轮定子,5-定轴,6-传动套,7-冲击爪,701-方形部,702-爪扣部,703-连接部,8-冲击架,801-条形槽,9-传动轴,901-爪扣槽,902-过渡部分,10-钻头套筒,11-外壳花键,12-钻头套筒花键,13-钢套,14-压盖,15-端帽,16-定位套,17-挡盘,18-压盘,19-定轴侧流道,20-U形口,21-承压轴承,22-防掉挡圈,22-防掉螺杆,24-刚性稳定器。In the figure: 1-transition joint, 2-housing, 3-turbine rotor, 4-turbine stator, 5-fixed shaft, 6-transmission sleeve, 7-impact claw, 701-square part, 702-claw buckle part, 703- Connection part, 8-impact frame, 801-bar groove, 9-drive shaft, 901-claw buckle groove, 902-transition part, 10-drill sleeve, 11-shell spline, 12-drill sleeve spline, 13-steel sleeve, 14-gland, 15-end cap, 16-positioning sleeve, 17-baffle plate, 18-pressure plate, 19-fixed shaft side flow channel, 20-U-shaped mouth, 21-pressure bearing, 22-anti-drop retaining ring, 22-anti-drop screw rod, 24-rigid stabilizer.

具体实施方式Detailed ways

结合附图,一种涡轮扭转冲击发生器,主要由转换接头1、外壳2、涡轮转子3、涡轮定子4、定轴5、传动套6、冲击爪7、冲击架8、传动轴9和钻头套筒10组成。In conjunction with the accompanying drawings, a turbine torsional impact generator is mainly composed of a conversion joint 1, a casing 2, a turbine rotor 3, a turbine stator 4, a fixed shaft 5, a transmission sleeve 6, an impact claw 7, an impact frame 8, a transmission shaft 9 and a drill bit The sleeve 10 is composed.

转换接头1一端为连接钻铤的公扣,另一端为连接外壳2的公扣。外壳2上端为连接转换接头的母扣,外壳2下端均布有四个45度的外壳花键11,形成四个45度的壳体花键槽。在钻头套筒10上有四个40度的钻头套筒花键12环绕排列在钻头套筒端面上,形成四个50度的钻头套筒花键槽,外壳花键11与钻头套筒花键槽形成间隙配合。One end of the conversion joint 1 is a male buckle connected to the drill collar, and the other end is a male buckle connected to the shell 2 . The upper end of the shell 2 is a female buckle for connecting the adapter, and four 45-degree shell splines 11 are evenly distributed on the lower end of the shell 2, forming four 45-degree shell spline grooves. On the drill sleeve 10, there are four 40-degree drill sleeve splines 12 arranged around the end face of the drill sleeve to form four 50-degree drill sleeve spline grooves, and the shell splines 11 form the drill sleeve spline grooves Clearance fit.

涡轮转子3固定在定轴5上,定轴5下部设置有台肩,侧面设置有半圆条形凸台,上部安装钢套13,涡轮转子3通过台肩、凸台和钢套定位,压盘18安装在钢套上,二者为滑动连接,端帽15和定轴通过螺纹连接将涡轮转子3固定在定轴5上。The turbine rotor 3 is fixed on the fixed shaft 5. The lower part of the fixed shaft 5 is provided with a shoulder, and the side is provided with a semicircular bar-shaped boss. The upper part is equipped with a steel sleeve 13. The turbine rotor 3 is positioned by the shoulder, the boss and the steel sleeve. 18 is installed on the steel sleeve, the two are slidingly connected, and the end cap 15 and the fixed shaft fix the turbine rotor 3 on the fixed shaft 5 through threaded connection.

涡轮定子4固定在外壳2上。涡轮定子4下部通过定位套16定位,定位套16座在挡盘17上,挡盘17座在外壳2的台肩上,再通过压盘18和转换接头1固定在外壳2上。The turbine stator 4 is fixed on the casing 2 . The lower part of the turbine stator 4 is positioned by the positioning sleeve 16, and the positioning sleeve 16 is seated on the baffle plate 17, and the baffle plate 17 is seated on the shoulder of the shell 2, and then fixed on the shell 2 by the pressure plate 18 and the adapter 1.

定轴5和传动套6通过花键配合,传动套6安装在冲击架8上端,冲击架8下端安装端盖,传动轴9安装在传动套6和端盖上,冲击爪7安装在冲击架8上。定轴5下端设置有挡盘17,挡盘17中间开孔起到扶正定位套的作用。定轴5上设置有侧流道19。钻井液经转换接头1进入外壳2内,流经涡轮到达挡盘17,然后上返至定轴侧流道19,汇聚到定轴的主流道,然后经传动套6进入传动轴9,继续向下流入钻头套筒10。The fixed shaft 5 and the transmission sleeve 6 are matched by splines, the transmission sleeve 6 is installed on the upper end of the impact frame 8, the end cover is installed on the lower end of the impact frame 8, the transmission shaft 9 is installed on the transmission sleeve 6 and the end cover, and the impact claw 7 is installed on the impact frame 8 on. The lower end of the fixed shaft 5 is provided with a stop disc 17, and the opening in the middle of the stop disc 17 plays the role of righting the positioning sleeve. The fixed shaft 5 is provided with a side channel 19 . Drilling fluid enters the housing 2 through the conversion joint 1, flows through the turbine to the baffle plate 17, then returns upward to the fixed shaft side channel 19, converges to the main channel of the fixed shaft, and then enters the transmission shaft 9 through the transmission sleeve 6, and continues to Down into the drill sleeve 10 .

钻井液启动涡轮,涡轮转子3高速旋转,带动定轴5高速旋转,定轴5带动传动套6旋转。传动套6上开设有U形口21。冲击爪7包括方形部701、爪扣部702和连接部703,方形部701与U形口20相配合,连接部703为椭圆柱形。在冲击架8上设置有条形槽801,冲击爪的连接部703卡入条形槽801中,冲击爪7可相对于冲击架8小角度旋转。在传动轴9上设置有与爪扣部702相配合的爪扣槽901,传动轴在开设爪扣槽时,要求考虑制作工艺,因此,有一段过渡部分902来满足零件加工制作过程中刀具切割的路径。传动套6转动时通过U形口21拨动冲击爪方形部701,带动冲击爪7和冲击架8转动,冲击爪7通过爪扣部702与爪扣槽901的配合作用周期性的冲击传动轴9。The drilling fluid starts the turbine, and the turbine rotor 3 rotates at high speed, driving the fixed shaft 5 to rotate at high speed, and the fixed shaft 5 drives the transmission sleeve 6 to rotate. A U-shaped opening 21 is opened on the transmission sleeve 6 . The impact claw 7 includes a square part 701 , a hook part 702 and a connection part 703 , the square part 701 fits with the U-shaped mouth 20 , and the connection part 703 is an elliptical column. A bar-shaped groove 801 is provided on the impact frame 8 , and the connecting portion 703 of the impact claw is snapped into the bar-shaped groove 801 , and the impact claw 7 can rotate at a small angle relative to the impact frame 8 . The transmission shaft 9 is provided with a claw groove 901 that matches the claw portion 702. When the transmission shaft is provided with a claw groove, it is required to consider the manufacturing process. Therefore, there is a transition portion 902 to meet the requirements of the tool cutting during the part processing and manufacturing process. path of. When the transmission sleeve 6 rotates, the impact claw square part 701 is moved through the U-shaped mouth 21, and the impact claw 7 and the impact frame 8 are driven to rotate. The impact claw 7 periodically impacts the drive shaft through the cooperation of the claw buckle part 702 and the claw buckle groove 901. 9.

在外壳2内壁上开设有凹槽,在凹槽内固定承压轴承21,所述冲击架端盖和传动轴9座在承压轴承21上。传动轴9和钻头套筒10通过螺纹连接,在钻头套筒10上开设方形沟槽,在沟槽中安放两个半圆环形防掉挡圈22,在外壳下端周向开设四个螺纹孔,在螺纹孔中装入防掉螺杆23,防掉挡圈22和防掉螺杆23通过螺纹连接。防掉挡圈22和防掉螺杆23对钻头套筒起到双保险作用,提高了钻井的安全性。A groove is opened on the inner wall of the housing 2, and a pressure bearing 21 is fixed in the groove, and the impact frame end cover and the transmission shaft 9 are seated on the pressure bearing 21. The transmission shaft 9 and the drill sleeve 10 are threadedly connected, and a square groove is provided on the drill sleeve 10. Two semi-circular rings 22 are placed in the groove, and four threaded holes are provided in the circumferential direction of the lower end of the shell. In the threaded hole, the anti-drop screw rod 23 is loaded, and the anti-drop retaining ring 22 and the anti-drop screw rod 23 are connected by threads. The anti-drop retaining ring 22 and the anti-drop screw rod 23 play a double insurance role on the drill bit sleeve, which improves the safety of drilling.

在外壳2外侧壁上均布四个刚性稳定器24,所述刚性稳定器24沿外壳长度方向伸展,呈长型螺旋叶片型,在提速快打的同时还能起到防斜作用,保证井身质量。Four rigid stabilizers 24 are evenly distributed on the outer wall of the casing 2, and the rigid stabilizers 24 extend along the length direction of the casing and are in the shape of long spiral blades. Body quality.

上述涡轮转子3和涡轮定子4的叶型是采用五次多项式法结合计算软件和工具需求的参数要求计算优化得出,具体如图10、11所示,该涡轮转子和涡轮定子叶型可使得能量的转化效率进一步提升。The airfoils of the above-mentioned turbine rotor 3 and turbine stator 4 are calculated and optimized by using the quintic polynomial method in combination with the parameter requirements of calculation software and tool requirements, specifically as shown in Figures 10 and 11, the turbine rotor and turbine stator airfoils can make The energy conversion efficiency is further improved.

下面对本发明的工作过程进行说明:The working process of the present invention is described below:

钻铤带动外壳2旋转,外壳2通过花键带动钻头套筒10从而带动钻头不断旋转剪切地层岩石。同时,钻井液经转换接头1进入涡轮扭转冲击发生器外壳内,流经压盖14上的流道进入涡轮,启动涡轮,涡轮转子3高速旋转,带动定轴5高速旋转,此时钻井液流经涡轮到达挡盘19,钻井液上返至定轴侧流道20,汇聚到定轴的主流道,进入传动套6继续向下流动。定轴5通过花键带动传动套6高速旋转,传动套6拨动冲击爪7,冲击爪7带动冲击架8高速旋转,在旋转过程中冲击爪7和传动套6作用并不断地冲击传动轴9,形成高频冲击。传动轴9将获得的高频冲击能量传递到钻头套筒10上,钻头套筒10带动钻头脉动地冲击地层岩石;同时钻井液经传动套6进入到传动轴9,继续向下流动进入钻头套筒10。The drill collar drives the casing 2 to rotate, and the casing 2 drives the drill bit sleeve 10 through splines to drive the drill bit to continuously rotate and shear formation rocks. At the same time, the drilling fluid enters the casing of the turbine torsional impact generator through the conversion joint 1, flows into the turbine through the flow channel on the gland 14, starts the turbine, and the turbine rotor 3 rotates at a high speed, driving the fixed shaft 5 to rotate at a high speed. At this time, the drilling fluid flows After reaching the baffle plate 19 through the turbine, the drilling fluid returns to the side channel 20 of the fixed shaft, converges to the main channel of the fixed shaft, enters the transmission sleeve 6 and continues to flow downward. The fixed shaft 5 drives the transmission sleeve 6 to rotate at high speed through the spline, and the transmission sleeve 6 moves the impact claw 7, and the impact claw 7 drives the impact frame 8 to rotate at high speed. During the rotation, the impact claw 7 and the transmission sleeve 6 act and continuously impact the transmission shaft 9. Form high-frequency shock. The transmission shaft 9 transmits the obtained high-frequency impact energy to the drill sleeve 10, and the drill sleeve 10 drives the drill bit to impact the formation rock in a pulsating manner; at the same time, the drilling fluid enters the transmission shaft 9 through the transmission sleeve 6, and continues to flow downward into the drill sleeve cartridge 10.

上述方式中未述及的部分采取或借鉴已有技术即可实现。Parts not mentioned in the above methods can be realized by adopting or referring to existing technologies.

需要说明的是,在本说明书的教导下,本领域技术人员所作出的任何等同替代方式,或明显变型方式,均应在本发明的保护范围之内。It should be noted that, under the teaching of this specification, any equivalent replacement or obvious modification made by those skilled in the art shall fall within the protection scope of the present invention.

Claims (6)

1.一种涡轮扭转冲击发生器,其特征在于:包括转换接头、外壳、涡轮、定轴、传动套、冲击爪、冲击架、传动轴和钻头套筒,外壳上端连接转换接头,外壳下端连接钻头套筒,涡轮转子固定在定轴上,涡轮定子固定在外壳上,定轴和传动套通过花键配合,传动套安装在冲击架上端,冲击架下端安装端盖,传动轴安装在传动套和端盖上,冲击爪安装在冲击架上;定轴下端设置有挡盘,定轴上设置有侧流道,钻井液经转换接头进入外壳内,流经涡轮到达挡盘,然后上返至定轴侧流道,汇聚到定轴的主流道,然后经传动套进入传动轴,继续向下流入钻头套筒;钻井液启动涡轮,涡轮转子高速旋转,带动定轴高速旋转,定轴带动传动套旋转,传动套上开设有U形口,冲击爪包括方形部、爪扣部和连接部,方形部与U形口相配合,连接部为圆柱形,在冲击架上设置有条形槽,冲击爪的连接部卡入条形槽中,冲击爪可相对于冲击架小角度旋转,在传动轴上设置有与爪扣部相配合的爪扣槽,传动套转动时通过U形口拨动冲击爪方形部,带动冲击爪和冲击架转动,冲击爪周期性的冲击传动轴。1. A turbine torsional impact generator, characterized in that: it comprises an adapter, a casing, a turbine, a fixed shaft, a transmission sleeve, an impact claw, an impact frame, a transmission shaft and a drill sleeve, the upper end of the casing is connected to the adapter, and the lower end of the casing is connected to the The drill bit sleeve, the turbine rotor is fixed on the fixed shaft, the turbine stator is fixed on the shell, the fixed shaft and the transmission sleeve are matched by splines, the transmission sleeve is installed on the upper end of the impact frame, the end cover is installed on the lower end of the impact frame, and the transmission shaft is installed on the transmission sleeve and on the end cover, the impact claw is installed on the impact frame; the lower end of the fixed shaft is provided with a baffle plate, and the fixed shaft is provided with a side flow channel. The drilling fluid enters the casing through the conversion joint, flows through the turbine to the baffle plate, and then returns to the The flow channel on the side of the fixed shaft converges to the main channel of the fixed shaft, then enters the transmission shaft through the transmission sleeve, and continues to flow down into the drill bit sleeve; the drilling fluid starts the turbine, and the turbine rotor rotates at high speed, driving the fixed shaft to rotate at high speed, and the fixed shaft drives the transmission When the sleeve rotates, there is a U-shaped opening on the transmission sleeve. The impact claw includes a square part, a claw buckle part and a connecting part. The square part matches the U-shaped opening. The connecting part is cylindrical. The connecting part of the impact claw is snapped into the bar-shaped groove, and the impact claw can rotate at a small angle relative to the impact frame. There is a claw buckle groove matching the claw buckle part on the transmission shaft, and the transmission sleeve is moved through the U-shaped opening when it rotates. The square part of the impact claw drives the impact claw and the impact frame to rotate, and the impact claw periodically impacts the drive shaft. 2.根据权利要求1所述的一种涡轮扭转冲击发生器,其特征在于:在外壳侧壁上均布四个刚性稳定器,所述刚性稳定器为长型螺旋叶片型。2. A turbine torsional impact generator according to claim 1, characterized in that four rigid stabilizers are evenly distributed on the side wall of the housing, and the rigid stabilizers are long spiral blades. 3.根据权利要求1所述的一种涡轮扭转冲击发生器,其特征在于:所述转换接头一端为连接钻铤的公扣,另一端为连接外壳的公扣;外壳上端为连接转换接头的母扣,外壳下端均布有四个45度的外壳花键,形成四个45度的外壳花键槽;在钻头套筒上有四个40度的花键环绕排列在钻头套筒端面上,形成四个50度的钻头套筒花键槽,外壳花键与钻头套筒花键槽形成间隙配合。3. A turbine torsional impact generator according to claim 1, characterized in that: one end of the conversion joint is a male buckle connected to the drill collar, and the other end is a male buckle connected to the housing; the upper end of the housing is a male buckle connected to the conversion joint. The female buckle has four 45-degree shell splines evenly distributed on the lower end of the shell, forming four 45-degree shell spline grooves; on the drill sleeve, there are four 40-degree splines arranged around the end face of the drill sleeve to form Four 50-degree drill sleeve spline grooves, the housing splines form a clearance fit with the drill sleeve spline grooves. 4.根据权利要求1所述的一种涡轮扭转冲击发生器,其特征在于:所述定轴下部设置有台肩,侧面设置有半圆条形凸台,上部安装钢套,涡轮转子通过台肩、凸台和钢套定位,压盘安装在钢套上,二者为滑动连接,端帽和定轴通过螺纹连接将涡轮转子固定在定轴上;所述涡轮定子下部通过定位套定位,定位套座在挡盘上,挡盘座在外壳内壁的台肩上,涡轮定子上部通过压盘和转换接头固定在外壳上。4. A turbine torsional impact generator according to claim 1, characterized in that: the lower part of the fixed shaft is provided with a shoulder, the side is provided with a semi-circular bar-shaped boss, the upper part is installed with a steel sleeve, and the turbine rotor passes through the shoulder , The boss and the steel sleeve are positioned, the pressure plate is installed on the steel sleeve, the two are slidingly connected, the end cap and the fixed shaft are threaded to fix the turbine rotor on the fixed shaft; the lower part of the turbine stator is positioned through the positioning sleeve, and the positioning The sleeve is seated on the baffle plate, the baffle plate is seated on the shoulder of the inner wall of the shell, and the upper part of the turbine stator is fixed on the shell through the pressure plate and the conversion joint. 5.根据权利要求1所述的一种涡轮扭转冲击发生器,其特征在于:所述外壳内壁上开设有凹槽,在凹槽内固定承压轴承,所述冲击架端盖和传动轴座在承压轴承上。5. A turbine torsional impact generator according to claim 1, characterized in that: a groove is opened on the inner wall of the housing, and the pressure-bearing bearing is fixed in the groove, and the end cover of the impact frame and the transmission shaft seat on pressure bearings. 6.根据权利要求1所述的一种涡轮扭转冲击发生器,其特征在于:所述传动轴和钻头套筒通过螺纹连接,在钻头套筒上开设方形沟槽,在沟槽中安放两个半圆环形防掉挡圈,在外壳下端周向开设四个螺纹孔,在螺纹孔中装入防掉螺杆,防掉挡圈和防掉螺杆通过螺纹连接。6. A turbine torsional impact generator according to claim 1, characterized in that: the transmission shaft and the drill bit sleeve are connected by threads, a square groove is opened on the drill bit sleeve, and two The semi-circular anti-drop retaining ring is provided with four threaded holes circumferentially at the lower end of the shell, and the anti-drop screw rods are put into the threaded holes, and the anti-drop retaining ring and the anti-drop screw are connected by threads.
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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105888538A (en) * 2016-04-08 2016-08-24 西南石油大学 Torsion impact drilling device
CN106499340A (en) * 2016-11-09 2017-03-15 西南石油大学 A kind of fluid power pulse generating unit and its method of operating
CN108049803A (en) * 2018-02-08 2018-05-18 西南石油大学 Vane type differential torsion impact device
CN108487856A (en) * 2018-05-23 2018-09-04 成都奥尤盖茨科技发展有限公司 A kind of flexible pressurizing torsion generator
CN110578469A (en) * 2019-09-27 2019-12-17 重庆科技学院 A casing extension drilling tool

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090321143A1 (en) * 2008-06-30 2009-12-31 Center Rock, Inc. Self-Indexing Down-The-Hole Drill
CN201554363U (en) * 2009-12-20 2010-08-18 西南石油大学 A Turbine Type Torsional Hammer Drill Used in Hard Formation
CN201778652U (en) * 2010-09-20 2011-03-30 西南石油大学 Low-amplitude and high-frequency torsional pulse generator
US20130133909A1 (en) * 2010-05-25 2013-05-30 Roland Greenwood Enhanced vibrational or hammering apparatus
CN203239230U (en) * 2013-01-30 2013-10-16 中国石油天然气集团公司 Downhole jet flow auxiliary drilling speed increasing device
CN203614029U (en) * 2013-12-18 2014-05-28 中国石油大学(华东) Turbine torsional impact generator

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090321143A1 (en) * 2008-06-30 2009-12-31 Center Rock, Inc. Self-Indexing Down-The-Hole Drill
CN201554363U (en) * 2009-12-20 2010-08-18 西南石油大学 A Turbine Type Torsional Hammer Drill Used in Hard Formation
US20130133909A1 (en) * 2010-05-25 2013-05-30 Roland Greenwood Enhanced vibrational or hammering apparatus
CN201778652U (en) * 2010-09-20 2011-03-30 西南石油大学 Low-amplitude and high-frequency torsional pulse generator
CN203239230U (en) * 2013-01-30 2013-10-16 中国石油天然气集团公司 Downhole jet flow auxiliary drilling speed increasing device
CN203614029U (en) * 2013-12-18 2014-05-28 中国石油大学(华东) Turbine torsional impact generator

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105888538A (en) * 2016-04-08 2016-08-24 西南石油大学 Torsion impact drilling device
CN106499340A (en) * 2016-11-09 2017-03-15 西南石油大学 A kind of fluid power pulse generating unit and its method of operating
CN108049803A (en) * 2018-02-08 2018-05-18 西南石油大学 Vane type differential torsion impact device
CN108049803B (en) * 2018-02-08 2023-08-08 西南石油大学 Impeller type differential torque impact device
CN108487856A (en) * 2018-05-23 2018-09-04 成都奥尤盖茨科技发展有限公司 A kind of flexible pressurizing torsion generator
CN110578469A (en) * 2019-09-27 2019-12-17 重庆科技学院 A casing extension drilling tool
CN110578469B (en) * 2019-09-27 2024-03-22 重庆科技学院 Extension drilling tool in sleeve

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