Turbodrill turbine

 

(57) Abstract:

The invention relates to the drilling technique. The turbine of the turbo-drill includes a rotor 1 and a stator 2 with hubs 3 and 4. Blade apparatus (LA) 5 and 6 fixed to the hub 3 and 4. LA 5 and 6 made in the form of blades 7 with rims 8. LA 5 and 6 are made with flat connector 9, passing through the point of maximum deflection surfaces of the blades 7. The weekend of 10 and 11 LA 5 and 6 can be made of a more wear resistant material than the input part 12 and 13. The output part 10 LA 5 can be made identical to the input part 13 LA 6, and the input part 12 LA 5 - output part 11 LA 6. This embodiment of the turbine of the turbo-drill will simplify manufacturing technology turbines. 2 C. p. F.-ly, 2 Il.

The invention relates to the drilling process and can be used in turbines turbodrills.

The aim of the invention is the simplification of the manufacture of turbines.

In Fig. 1 shows a turbine of the turbo-drill, an axial slit; Fig. 2 - circular cross-section a-a in Fig. 1.

The turbine of the turbo-drill includes a rotor 1 and a stator 2 with the hub 3 and 4 and fixed on them vane devices 5 and 6, made in the form of blades 7 with the rim 8. Blade devices 5 and 6 to be executed 11 blades 5 and 6 can be made of a more wear-resistant material, the input part 12 and 13. The output part 10 of blades 5 of the rotor 1 can be made identical to the input part 13 of guide vanes 6 of the stator 2, and the input part 12 of blades 5 of the rotor 1 - output part 11 of guide vanes 6 of the stator 2.

Part of the blades 5 and 6 turbines cast on the machines handle the docking surface, fixed to the hub 3 and 4 and are fastened to each other, for example, by gluing, soldering, welding. To reduce the influence of the interface on the hydraulic flow at blade devices 5, 6 turbines are coated, for example, from polymeric compositions based on epoxy resins. In the case of complete turbines symmetrical profiles blade devices 5, 6 of the rotor 1 and the stator 2 can be cast in two molds in which they cast on one half of the profile. Moreover, the parts 10 and 13, 11 and 12 are interchangeable. The greatest influence on the change of the energy characteristics has wear on the output edges of the blades 7, so part of the blades 5, 6, including weekends edges, it is advisable to produce a more wear resistant material such as ceramics.

The turbine of the turbo-drill set in case and fix the rotor 1 and the stator 2 and the rotor 1, the fluid flow changes direction and, flowing from the stage to the stage, gives a part of its hydraulic capacity of each stage.

As a result, the power generated by all stages, summarized on the shaft of the turbo-drill.

This turbine will significantly simplify the manufacturing technology of complex profiles of active turbines turbodrills, cast them on the semi-automatic, detachable forms. (56) USSR Author's certificate N 844806, CL F 03 B 13/02, 1979.

1. The TURBINE of the turbo-drill, containing the rotor and the stator and hub fixed on them vane apparatus, made in the form of blades rims, characterized in that, to simplify manufacturing techniques turbine blade apparatus of the rotor and stator are made with flat connector passing through the point of maximum deflection surfaces of the blades.

2. Turbine under item 1, characterized in that the output part of the blades are made of a more wear resistant material than the input.

3. Turbine under item 1, characterized in that the output part of the guide vanes of the rotor is made identical to the input side of the guide vanes of the stator, and the inlet guide vanes of the rotor - output part of the guide vanes of the stator is

 

Same patents:

FIELD: oil and gas extractive industry.

SUBSTANCE: device has metallic hubs of stator and rotor, wherein crowns of stator and rotor are concentrically pressed. Crowns of stator and rotor are made of durable ceramics and are additionally equipped with connections, allowing to exclude non-controlled turning of crowns in hubs and spontaneous axial displacement thereof.

EFFECT: higher reliability and efficiency.

2 dwg

FIELD: engine manufacturing.

SUBSTANCE: invention relates to method of operation of self-contained power station powered by diesel-generator set. According to proposed method of operation of self-contained power station powered by diesel generator set equipped with additional flywheel and disconnect clutch with automatic control members, additional flywheel is mounted on separate shaft which is connected with diesel-generator set by means of disconnect clutch. Preparatory operation is carried out to set power station into operation with subsequent overcoming of short-time starting resistances from consumer. Additional flywheel is connected to shut down diesel generator set by means of disconnect clutch. Power station is started under no load, and its coming to rated speed is detected by readings of generator shaft speed pickups. Load is connected and intensity of generator shaft speed drop is checked. Information is automatically transmitted to controller wherefrom, at termination of generator speed drop, signal is transmitted to disconnect clutch, and rotating additional flywheel is disconnected from diesel generator set, thus changing the set for accelerated mode of restoration of initial rated speed.

EFFECT: provision of power saving operation at stable conditions for overcoming designed resistance torque and short-time overloads exceeding capabilities of chosen supply source.

1 dwg

FIELD: electromechanical engineering.

SUBSTANCE: proposed generator primarily designed to supply with power borehole instrument of face telemetering system in the course of boring has internal stator and rotor; the latter mounts turbine in its front part that has casing carrying rectangular- or trapezoidal-section helical blades. These blades are free to vary their angle of lift depending on conditions of borehole washing with drilling fluid. Blades may be made of flexible material and have two parts of which one part is joined with turbine casing and other (loose) part is free to bend in transverse plane. In addition, blades may have variable stiffness in cross-sectional area and variable height of cross-section profile; loose parts of blades may be joined with ring. Blade turn limiter responding to maximal discharge of drilling fluid may be provided on the turbine casing.

EFFECT: enhanced operating reliability and extended variation range of drilling fluid discharge through generator turbine.

7 cl, 2 dwg

Turbodrill turbine // 2269631

FIELD: oil and gas well drilling equipment, particularly axial flow turbine of multistage turbodrill.

SUBSTANCE: turbodrill turbine comprises stator with blade ring and inner rim, rotor with blade ring and hub. Design angles of stator flow inlet and outlet directions α2 and α1 and rotor flow inlet and outlet directions β2 and β1 are related by theoretical correlations with peripheral velocity determined in idle and optimal (shock-free) mode of turbine operation. Stator and rotor blade ring blades defining above design angles as distinct from prior art turbines are formed so that shock-free regime of flow around the stator and the rotor is realized at different peripheral velocities, wherein above shock-free regime of stator flow-around is performed in retardation mode, shock-free regime of rotor flow-around is performed in runaway mode thereof. Above stator and rotor angles are correlated as α12≤π/2 and β21≤π/2 (in the case of positive reactive turbine) and β12≤π/2 (for negative reactive turbine). The stator rim has surface of lesser diameter having conoid shape and converging towards lower cross-section thereof so that minimal annular gap defined by rotor hub is 0.05-0.3, preferably 0.1-0.2 of radial stator blade height and inner blade ring surface of lesser diameter has conoid shape and is converged to upper section so that radial rotor blade height ratio in lower and upper sections is equal to 0.7 - 0.95.

EFFECT: increased axial support resistance along with increased performance.

5 cl, 8 dwg

FIELD: engines and pumps.

SUBSTANCE: invention can be used as a hydraulic turbine for producing electric power, as a pneumatic and hydraulic turbine making a drive in heading machines, as well as in drilling gas and oil holes. Twin rotor stepping turbine incorporates an asynchronous reduction gear. Inner (5) and outer (6) rotors are fitted aligned on the aligned shafts, the outer and inter rotor vanes entering their inter-vane space to come into contact with the inner rotor outer surface and the outer rotor inner surface, respectively, so as to turn the said rotors in turn one way through the designed angle from the acting working clearance which allows filling the rotors' inter-vane space via the slide valves fitted on the turbine inner and outer rotors. Note that the aforesaid rotors are rigidly linked with the aforesaid inner and outer aligned shafts of the asynchronous variable gear ratio reduction gear to allow asynchronous one-way rotation of the twin turbine inner and outer rotors.

EFFECT: smaller turbine overall sizes and higher output.

5 dwg

Turboalternator // 2404370

FIELD: engines and pumps.

SUBSTANCE: proposed turboalternator comprises outer stator arranged in tight casing, upper fairing and inner rotor fitted on turboalternator shaft. The latter runs in rolling bearings arranged on both sides of the rotor. Said shaft is furnished with two extra seals. Said tight casing is filled with lubricant-coolant. It comprises two stationary pistonless compensators that do not revolve with the shaft. First compensator is arranged inside turboalternator housing nut and filled with lubricant-coolant. Second compensator is arranged in shell that covers the turboalternator tight housing. First seal separates inner space of the said first compensator from outer fluid (drill fluid), while second seal separates first compensator inner space filled with lubricant-coolant from turboalternator tight housing, also filled with lubricant-coolant.

EFFECT: notable reduced abrasive wear, ruling out turbulent flow origination, longer life and higher reliability.

1 cl, 1 dwg

FIELD: oil and gas industry.

SUBSTANCE: invention is related to power supply system of borehole surface system assembly. The power supply system of a borehole surface system assembly contains at least one primary engine interconnected to fuel source supplying the primary engine and containing at least one heat source, at least one pump driven by the primary engine interconnected to at least one borehole and at least one fluid used in the borehole and at least one auxiliary system interconnected to the heat source from at least one primary engine. At that the auxiliary system contains a heat exchanger designed to transfer heat from the heat source to the fluid in order to separate one part of the fluid from the other part in at least one borehole.

EFFECT: improving efficiency, flexibility and productivity of the power supply system of a borehole surface system assembly.

20 cl, 5 dwg

FIELD: oil and gas industry.

SUBSTANCE: generator, external stator placed in as sealed body, internal rotor installed at the generator shaft with roller bearings in sealed cavity filled with a lubricant coolant and sealing components. At that the generator sealed body is divided into three sealed loops - electrical, kinematic and protective ones. Electric loop of the stator is equipped with an independent compensating diaphragm and filled with cooling liquid and separated from the kinematic loop by a screen made of non-magnet material. Kinematic loop of the bearings is filled with lubricant and separated by a system of cup-type seals and inner diaphragm from the protective loop of an end sealing compensator filled with lubricant in the volume limited by the outside diaphragm. The electrical loop is filled with dielectric cooling liquid without excessive pressure; the kinematic is filled with dielectric cooling liquid without excessive pressure; protective is filled with dielectric cooling liquid under excessive pressure. Besides, the protective loop may be filled with lubricant having higher viscosity and higher boundary tension in comparison with lubricant in the kinematic loop. Zero point of the stator windings is coupled to the body through a plugging contact. The filling system for the protective and kinematic loops has a valve spindle to switch between the filled loops at vacuuming and filling of lubricant. Rigidity of diaphragms in the electric and kinematic loops is higher than the same in the protective loop.

EFFECT: improving reliability of the generator and reducing labour intensity during repair and maintenance operations.

6 cl, 1 dwg

FIELD: mining.

SUBSTANCE: group of inventions is related to drilling, i.e. to rotary drilling hydraulic drives installed in borehole. Assembly of hydraulic downhole motor comprises screw motor having near end and far end and comprising stator and rotor. Stator comprises metal case, first elastomer material arranged in metal case, and first rigid material, arranged radially and directed inward from and at least partially covering first elastomer material. Rotor contains metal core, second elastomer material, located around metal core, and second rigid material arranged around second elastomer material. Stator first rigid material contacts rotor second rigid material.

EFFECT: enabling limiting of rotor geometric center displacement trajectory.

12 cl, 21 dwg

FIELD: electricity.

SUBSTANCE: invention relates to turbine for transmission of electric data from one end of turbine to other end. Turbine (100) has first end (101) and second end (103). Ends (101) and (103) are opposite to each other. Turbine (100) comprises housing (104), shaft (102) located in centre of housing (104), engine (106), having a plurality of rotors, stators and bearings arranged between shaft (102) and housing (104), at least one non-conducting insulator, providing electrical insulation of shaft (102) and housing (104) from each other. Engine (106) is located between first end (101) and second end (103) of turbine (100). Non-conducting insulator is located between housing (104) and a plurality of rotors, stators and bearings or is located between shaft (102) and a plurality of rotors, stators and bearings.

EFFECT: invention is aimed providing transmission of electric data signals.

20 cl, 12 dwg

Up!