CN103573203A - Paraffin control viscosity reduction sound wave vibrator - Google Patents

Paraffin control viscosity reduction sound wave vibrator Download PDF

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Publication number
CN103573203A
CN103573203A CN201210251422.7A CN201210251422A CN103573203A CN 103573203 A CN103573203 A CN 103573203A CN 201210251422 A CN201210251422 A CN 201210251422A CN 103573203 A CN103573203 A CN 103573203A
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CN
China
Prior art keywords
hole
jet flow
wave vibrator
wedge shape
osculum
Prior art date
Legal status (The legal status 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 status listed.)
Pending
Application number
CN201210251422.7A
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Chinese (zh)
Inventor
余昌荣
李俊坤
余洋
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
HUANGSHI XINXING PETROLEUM EQUIPMENT CO Ltd
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HUANGSHI XINXING PETROLEUM EQUIPMENT CO Ltd
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.)
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Publication date
Application filed by HUANGSHI XINXING PETROLEUM EQUIPMENT CO Ltd filed Critical HUANGSHI XINXING PETROLEUM EQUIPMENT CO Ltd
Priority to CN201210251422.7A priority Critical patent/CN103573203A/en
Publication of CN103573203A publication Critical patent/CN103573203A/en
Pending legal-status Critical Current

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Abstract

The invention discloses a paraffin control viscosity reduction sound wave vibrator which comprises a jet flow head. Threads are tapped on the outer side of the jet flow head, a wedge-shaped through hole is formed in the jet flow head, the smaller-opening end of the wedge-shaped through hole is arranged in the jet flow head end and provided with a jet flow groove, the jet flow groove and a smaller opening of the wedge-shaped through hole are formed in a centering mode, and the width of the jet flow groove is larger than that of the smaller opening of the wedge-shaped through hole. The paraffin control viscosity reduction sound wave vibrator is characterized in that the length L of the jet flow head is 300-500 mm, a support is arranged on one side of the jet flow head with the jet flow groove, a vibrating elastic piece is arranged on the support, one end of the vibrating elastic piece is fixed on the outer end of the support through a hexagon socket cap screw, and the other end of the vibrating elastic piece is arranged in the jet flow groove in a suspended mode and aligned to the smaller opening of the wedge-shaped through hole. By means of the paraffin control viscosity reduction sound wave vibrator, the problem of a traditional sound wave vibrator on a paraffin control viscosity reduction oil increasing device that explosive impact force can not be generated, sound wave vibration generated by the vibrating elastic piece does not reach the standard, a paraffin control viscosity reduction effect is not ideal and the like is solved. The paraffin control viscosity reduction sound wave vibrator is mainly used for stirring petroleum, conducting dispersion and emulsification and reducing gathering and viscosity.

Description

Wax-proof viscosity reducing sonic wave vibrator
(i) technical field: the present invention relates to the building block on wax-proof viscosity-reducing oil-increasing device, especially a kind of wax-proof viscosity reducing sonic wave vibrator.
(ii) background technology: wax-proof viscosity-reducing oil-increasing device is mainly for decomposing the paraffin in crude oil, solves the problems such as former oil viscosity high fluidity is poor, thereby reduces the live load of oil pumper.Wax-proof viscosity-reducing oil-increasing device is generally separated out device, sonic wave vibrator and outstanding stream oil increasing device three by strong magnetic paraffin control and is docked and form.
At present, the vibration shell fragment in traditional sonic wave vibrator is not centering with the osculum of wedge shape through hole to be arranged, make crude oil can not be accurately impact shock shell fragment fiercely.Wedge shape through hole length is too short, does not have enough spaces to make crude oil accelerate to flow, and cannot produce the impact force of explosion.The cross-sectional length design of wedge shape through hole osculum is unreasonable, liquid flowing resistance often occurs excessive or do not produce the phenomenons such as explosion impact force.Therefore, designing a kind of wax-proof viscosity reducing sonic wave vibrator that can address the above problem well is extremely necessary.
(iii) summary of the invention: object of the present invention is exactly to solve the problems such as the not up to standard and wax-proof viscosity reducing effect of the acoustic vibration that sonic wave vibrator cannot produce the impact force of explosion, vibration shell fragment produces on traditional wax-proof viscosity-reducing oil-increasing device is undesirable, and a kind of wax-proof viscosity reducing sonic wave vibrator is provided.
Concrete scheme of the present invention is: for traditional sonic wave vibrator, improve, it has jet head, screw thread has been attacked in the outside of jet head, the inside of jet head has wedge shape through hole, the osculum end of wedge shape through hole is positioned at jet cephalic par and has jet groove, the osculum of jet groove and wedge shape through hole is that centering is arranged and the width of jet groove is greater than the width of wedge shape through hole osculum, it is characterized in that: the length L of described jet head is 300~500mm, a side direction that has jet groove on jet head is equipped with support outward, vibration shell fragment is housed on support, vibration shell fragment one end adopts hexagon socket cap head screw to be fixed on the outer end of support, the other end suspends to be placed in jet groove and with the osculum centering of wedge shape through hole and arranges.
Described in the present invention, support is prong like.
Described in the present invention, vibrate shell fragment top and bottom and be all lined with pad.
The length L of the head of jet described in the present invention is 350mm.
When the former oil mass of daily output of producing well is at 1~50 ton hour, the present invention is designed to 15mm by the osculum length a of wedge shape through hole, and width b is 2.5mm.
When the former oil mass of daily output of producing well is at 50~100 ton hours, the present invention is designed to 20mm by the osculum length a of wedge shape through hole, and width b is 2.5mm.
When the former oil mass of daily output of producing well is at 100~150 ton hours, the present invention is designed to 25mm by the osculum length a of wedge shape through hole, and width b is 2.5mm.
The present invention lengthens the length of wedge shape through hole, thereby has strengthened the mobile distance of crude oil in wedge shape through hole, can produce larger impact force, and the osculum centering of vibration shell fragment and wedge shape through hole is arranged, makes to vibrate shell fragment and produces needed acoustic vibration.Simultaneously, the cross-sectional length of the daily output flow quantity appropriate design wedge shape through hole osculum of based on crude, avoid the cross-sectional length of wedge shape through hole osculum to cause greatly not producing the impact force of explosion and the cross-sectional length of wedge shape through hole osculum is little causes the phenomenon that liquid flowing resistance is large, and vibration shell fragment adopts import 65Mn high-strength spring steel, make to vibrate shell fragment ,Gei durable in use enterprise and brought huge economic benefit.
(iv) accompanying drawing explanation:
Fig. 1 is main sectional view of the present invention;
Fig. 2 is right view of the present invention;
Fig. 3 is that the P of Fig. 1 is to view;
Fig. 4 is that the K of Fig. 1 is to view.
In figure: 1-hexagon socket cap head screw, 2-pad, 3-vibrates shell fragment, 4-support, 5-jet groove, 6-jet head, 7-wedge shape through hole.
(v) the specific embodiment:
Referring to Fig. 1, 2, 3, 4, the present invention has jet head 6, screw thread has been attacked in the outside of jet head 6, the inside of jet head 6 has wedge shape through hole 7, the osculum end of wedge shape through hole 7 is positioned at jet head 6 ends and has jet groove 5, the osculum of jet groove 5 and wedge shape through hole 7 is that centering is arranged and the width of jet groove 5 is greater than the width of wedge shape through hole 7 osculums, particularly: the length L of described jet head 6 is 350mm, a side direction that has jet groove 5 on jet head 6 is equipped with support 4 outward, support 4 is prong like, vibration shell fragment 3 is housed on support 4, top and the bottom of vibration shell fragment 3 are all lined with pad 2, vibration shell fragment 3 one end adopt hexagon socket cap head screw 1 to be fixed on the outer end of support 4, the other end suspends to be placed in jet groove 5 and with the osculum centering of wedge shape through hole 7 and arranges.
When the former oil mass of daily output of producing well is at 1~50 ton hour, the present invention is designed to 15mm by the osculum length a of wedge shape through hole 7, and width b is 2.5mm.
When the former oil mass of daily output of producing well is at 50~100 ton hours, the present invention is designed to 20mm by the osculum length a of wedge shape through hole 7, and width b is 2.5mm.
When the former oil mass of daily output of producing well is at 100~150 ton hours, the present invention is designed to 25mm by the osculum length a of wedge shape through hole 7, and width b is 2.5mm.

Claims (8)

1. wax-proof viscosity reducing sonic wave vibrator, there is jet head, screw thread has been attacked in the outside of jet head, the inside of jet head has wedge shape through hole, the osculum end of wedge shape through hole is positioned at jet cephalic par and has jet groove, the osculum of jet groove and wedge shape through hole is that centering is arranged and the width of jet groove is greater than the width of wedge shape through hole osculum, it is characterized in that: the length L of described jet head is 300~500mm, a side direction that has jet groove on jet head is equipped with support outward, vibration shell fragment is housed on support, vibration shell fragment one end adopts hexagon socket cap head screw to be fixed on the outer end of support, the other end suspends to be placed in jet groove and with the osculum centering of wedge shape through hole and arranges.
2. wax-proof viscosity reducing sonic wave vibrator according to claim 1, is characterized in that: described support is prong like.
3. wax-proof viscosity reducing sonic wave vibrator according to claim 1, is characterized in that: described vibration shell fragment top and bottom are all lined with pad.
4. wax-proof viscosity reducing sonic wave vibrator according to claim 1, is characterized in that: the length L of described jet head is 350mm.
5. wax-proof viscosity reducing sonic wave vibrator according to claim 1, is characterized in that: the osculum length a of described wedge shape through hole is 15~25mm, and width b is 2.5mm.
6. wax-proof viscosity reducing sonic wave vibrator according to claim 5, is characterized in that: the osculum length a of described wedge shape through hole is 15mm.
7. wax-proof viscosity reducing sonic wave vibrator according to claim 5, is characterized in that: the osculum length a of described wedge shape through hole is 20mm.
8. wax-proof viscosity reducing sonic wave vibrator according to claim 5, is characterized in that: the osculum length a of described wedge shape through hole is 25mm.
CN201210251422.7A 2012-07-20 2012-07-20 Paraffin control viscosity reduction sound wave vibrator Pending CN103573203A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201210251422.7A CN103573203A (en) 2012-07-20 2012-07-20 Paraffin control viscosity reduction sound wave vibrator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201210251422.7A CN103573203A (en) 2012-07-20 2012-07-20 Paraffin control viscosity reduction sound wave vibrator

Publications (1)

Publication Number Publication Date
CN103573203A true CN103573203A (en) 2014-02-12

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CN201210251422.7A Pending CN103573203A (en) 2012-07-20 2012-07-20 Paraffin control viscosity reduction sound wave vibrator

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104196480A (en) * 2014-08-13 2014-12-10 中国科学院声学研究所 Hydrodynamic force ultrasonic wave generating device for reducing viscosity of superheavy oil
CN104389555A (en) * 2014-11-25 2015-03-04 东营咸亨工贸有限公司 Underground mechanical wave oscillation paraffin controller

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104196480A (en) * 2014-08-13 2014-12-10 中国科学院声学研究所 Hydrodynamic force ultrasonic wave generating device for reducing viscosity of superheavy oil
CN104196480B (en) * 2014-08-13 2017-06-27 中国科学院声学研究所 Hydrokinetic ultrasonic generating means for reducing overweight oil viscosity
CN104389555A (en) * 2014-11-25 2015-03-04 东营咸亨工贸有限公司 Underground mechanical wave oscillation paraffin controller

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Application publication date: 20140212