SU106746A1 - Turbine impeller for turbo-drill - Google Patents
Turbine impeller for turbo-drillInfo
- Publication number
- SU106746A1 SU106746A1 SU454921A SU454921DA SU106746A1 SU 106746 A1 SU106746 A1 SU 106746A1 SU 454921 A SU454921 A SU 454921A SU 454921D A SU454921D A SU 454921DA SU 106746 A1 SU106746 A1 SU 106746A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- turbo
- drill
- turbine impeller
- turbine
- blades
- Prior art date
Links
Landscapes
- Earth Drilling (AREA)
Description
Описываемое изобретение относитс к области ту-рби;шых рабочих колес дл турбобуров, примен емых дл бурени скважий.The described invention relates to the field of turbo-tubes, turbine drills used for drilling wells.
Известные конструкции забойных двигателей-турбобуров характеризуютс тем, что ирофил1и лопаток серийных, машин имеют цилиндрическую форму как у статора, так и у ротора, что вл етс причиной СИЛЬНОГО искажени формы междулопаточных каналов, ушир ющихс в вершииу лонаток. Така снижает к. п. д. ступени турбины.The known designs of downhole motor-turbo-drills are characterized by the fact that irofilia and blades are serial, the machines have a cylindrical shape both at the stator and at the rotor, which is the reason for the STRONG distortion of the shape of the inter-blade channels broadening at the top of the ribs. This reduces the efficiency of the turbine stage.
Описываемое изобретение устран ет этот недостаток.The described invention eliminates this disadvantage.
На чертеже изображен профиль предлагаемых лопаток турбины.The drawing shows the profile of the proposed turbine blades.
Лопатки / колеса турбины выполнены в виде дуговых отрезков кольца 2, по отношению к радиальному сечению которого дуговые отрезки имеют вогнутый по расчету желобообразный профиль 3, что обеспечивает в межлопаточных каналах посто нсиво осевой составл юш,ей скорости потока вдоль лопаток.The blades / turbine wheels are made in the form of arc segments of the ring 2, with respect to the radial section of which the arc segments have a concave-shaped trough-like profile 3, which ensures a constant axial component in the interscapular channels and its flow velocity along the blades.
Предмет изобретени Subject invention
Турбинное рабочее колесо дл турбобура, отличаюш,еес тем, что, с целью обеспечени а межлопаточных каналах посто нства осевой соста1вл юш,ей скорости потока вдоль лопаток, последние выполнены в виде дуговых отрезков желобообразного кольца.The turbine impeller for a turbodrill is distinguished by the fact that, in order to ensure that the interscapular channels are of axial stability, it has a flow velocity along the blades, the latter are made in the form of arc segments of a grooved ring.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU454921T | 1953-07-23 |
Publications (1)
Publication Number | Publication Date |
---|---|
SU106746A1 true SU106746A1 (en) | 1956-11-30 |
Family
ID=48380009
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU454921A SU106746A1 (en) | 1953-07-23 | 1953-07-23 | Turbine impeller for turbo-drill |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU106746A1 (en) |
-
1953
- 1953-07-23 SU SU454921A patent/SU106746A1/en active
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB626181A (en) | Improvements relating to axial flow turbomachines | |
FR2310481A1 (en) | Ultrahigh speed turbomolecular pump with electric motor - having cover with projecting cone circumferential ribs and blades acting as stators | |
GB1095830A (en) | Bladed rotor for a fluid flow machine such as a gas turbine engine | |
GB666536A (en) | Stator blades for a gas turbine | |
GB1217275A (en) | Gas turbine engine axial flow multi-stage compressor | |
US2446552A (en) | Compressor | |
GB1087514A (en) | Arrangement for damping vibration of steam-turbine blades | |
SU106746A1 (en) | Turbine impeller for turbo-drill | |
NL7708556A (en) | Turbine for compressible fluids - has two flow-paths after last stage but two created by circumferential baffles (NL 15.2.78) | |
SE8404989D0 (en) | synchronous | |
US743296A (en) | Centrifugal high-pressure pump. | |
GB1013835A (en) | Improvements in or relating to axial-flow turbines, compressors and exhausters | |
FR2271441A1 (en) | Magnetic flywheel suspension - has radially toothed magnetic rotor/stator interface | |
GB387766A (en) | Improvements in or relating to turbines and like rotary engines and pumps | |
SU658300A1 (en) | Turbomachine radial labyrinth packing | |
SU1927A1 (en) | Dual-rotation radial steam turbine | |
GB646728A (en) | Improvements in or relating to stator casings for turbines, compressors and like rotary bladed fluid flow machines | |
SU370362A1 (en) | AXIAL HYDRAULIC MACHINE | |
GB587509A (en) | Improvements relating to centrifugal compressors and pumps | |
SU779592A1 (en) | Turbomachine impeller | |
SU1019898A1 (en) | Turbomachine impeller | |
GB612573A (en) | Improvements in or relating to centrifugal pumps | |
SE7909725L (en) | LONG VETSKERING PUMPS AND COMPRESSORS | |
GB1010401A (en) | A new or improved housing arrangement for the shaft bearing of a gas turbine engine | |
US1714596A (en) | Steam-turbine construction |