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Jet rotor

A technology of rotors and internals, which is applied in the field of injection rotors, can solve the problems of cumbersome installation and adjustment of axial clearance, high cost of turbine blade processing, scrapping of exhaust gas turbochargers, etc., and achieves the advantages of light weight, high cost performance and small fluid energy loss Effect

Inactive Publication Date: 2013-12-04
周林
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In terms of performance, it has the characteristics of low speed and high torque, the pressure drop is below 4MPa, the output speed of single lobe (or single head, single line) screw drilling tool is lower than 400r / min, and the output speed of multi lobe screw drilling tool is 90 -150r / min, suitable for drilling with roller cone bits, but the fluid pressure loss is large
[0006] 3. Turbine drilling tool: it has the characteristics of high speed and high torque, no lateral vibration, and high ROP; the all-metal turbo drilling tool is resistant to high temperature and is suitable for deep wells and high temperature environments, but the drilling tool is long, about 15 meters, The application range of the drill bit is small, the processing cost of the turbine blade is high, the installation and adjustment of the axial clearance is cumbersome, and a reduction device is required
The single-stage radial turbine is the core component of the exhaust gas turbocharger. The blades of this single-stage radial turbine are not hollow. The turbine blades have no air cooling system, and they are wrapped in the center of the turbine housing. The heat dissipation effect is poor, especially for gasoline engines. The exhaust temperature of the exhaust gas is too high, the working environment of the turbine blades is extremely harsh, the speed of the turbine is much higher than that of the engine itself, and the turbine must be made light and thin to minimize the turbo hysteresis effect. All exhaust gas turbochargers that are widely used now The turbine blades are the most easily damaged and have a short lifespan. Taking a car with an exhaust gas turbocharger engine as an example, generally the turbocharging effect has dropped significantly at about 30,000 kilometers, and the entire exhaust gas turbocharger is scrapped at about 100,000 kilometers. , that is, the service life of the widely used exhaust gas turbocharger is far less than the service life of the piston engine and the car itself. For example, the service life of a good vehicle diesel engine can reach 800,000 kilometers

Method used

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Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0031] Embodiment 1: inner rotor type downhole power drilling tool with jet rotor: (as attached figure 1 , 2 As shown) the injection rotor is connected with the upper connection structure 1, the bearing assembly 2 and the lower connection structure 9 to form this kind of downhole dynamic drilling tool, wherein the injection rotor is mainly composed of the inflow channel 12 and the outer body 4 (in this embodiment, the outer body is The main part of the stator), the inner son 7 (the inner son is the main part of the rotor in this embodiment), the nozzle 5, the radial partition 3, the fluid return pipe 6 and the thrust wall 8. Outer part 4 and inner part 7 are both round tubular in shape and have a common longitudinal axis center line, outer part 4 is set outside inner part 7, and outer diameter of outer part is the maximum diameter of this kind of downhole power drilling tool, and it is smaller than borehole The diameter of each inner sub 7 has at least one nozzle pipe 5, a r...

Embodiment 2

[0032] Embodiment 2: the outer rotor type downhole power drilling tool that has jet rotor: (as attached image 3 , 4 Shown) is similar to embodiment 1, the injection rotor is connected with the upper connection structure 1, the bearing assembly 2 and the lower connection structure 9 etc. In this embodiment, the outer son is the main part of the rotor), the inner son 7 (the inner son is the main part of the stator in this embodiment), the nozzle 5, the fluid return pipe 6, the radial partition 3 and the thrust wall 8. The inner part 7, that is, the stator, has at least one spray pipe 5, a radial partition 3, and a fluid return pipe 6 that penetrate the entire layer of the stator side wall along the circumferential tangential direction; the lower connection structure 9 is a part of the outer part 4, that is, the lower section of the rotor. 4. The lower section is connected downwards with the drill bit 10; the nozzle pipe 5, the radial partition 3, and the fluid return pipe 6 are...

Embodiment 3

[0034]Embodiment 3: " turbine " jet type core machine (inner rotor type) that has injection rotor: " turbine " jet type core machine that has injection rotor of the present invention is mainly by high-pressure air compressor 14, combustion chamber 15 and driving high pressure The compressor consists of at least one injection rotor, wherein the injection rotor is mainly composed of an inflow channel 12 , an outer part 4 , an inner part 7 , a plurality of nozzle pipes 5 and a plurality of thrust walls 8 . The inflow channel 12 introduces the high-temperature and high-pressure gas generated in the upstream combustion chamber 15 into the interior of the inner son 7 along the longitudinal axis of the inner son 7; the outer son 4 and the inner son 7 have a common central longitudinal axis, and the outer son 4 is sleeved on the inner son 7 outside and can rotate relatively along the common central longitudinal axis; there are multiple converging nozzles arranged tangentially along the...

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Abstract

The invention mainly relates to a jet rotor in the fields of energy development, aircraft engines and the like. The jet rotor tangentially jets a high-energy fluid through a jet pipe on an interior so that the high-energy fluid acts on a thrust wall in a gap between the inner circle of an exterior and the outer circle of the interior to push the interior and exterior to rotate relatively; one of the interior and exterior becomes a rotor; and the rotor drives a load and converts partial energy of the high-energy fluid into the rotation energy of the rotor to replace a turbine. The jet rotor has the beneficial effects that: the jet rotor has the advantages of simple structure, few parts, light weight, short length, high reliability, long service life, high cost performance and high mechanical efficiency, ensures little loss of fluid energy, is easy to manufacture, saves a worm wheel or screw, and can sufficiently and efficiently utilize the fluid energy; and the jet rotor can be applied to the underground power jigs in drilling engineering, various power systems with turbine rotor and the like.

Description

1. Technical field: [0001] The invention mainly relates to a jet rotor in energy development, aero-engine and other fields, and in particular to downhole dynamic drilling tools in drilling engineering and various power systems with turbine rotors. 2. Background technology: [0002] (1) In the field of drilling engineering: downhole power drilling tools refer to bottom hole drilling tools that can convert the fluid energy of mud pump drilling fluid into drilling and rock breaking power. Due to the high speed and high end torque of the downhole power drilling tool, the mechanical drilling speed can be significantly increased, especially when used in conjunction with the PDC bit, the drilling speed will be greatly improved. Downhole dynamic drilling tools have advantages over traditional rotary drilling in terms of increasing mechanical penetration rate, increasing single bit footage, reducing drilling cost per meter, ensuring well quality and drilling safety, etc. To change t...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): E21B4/00F01D5/02F01D9/02
Inventor 周林周天宇
Owner 周林
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