FIELD: equipment for turbodrilling of oil and gas wells. SUBSTANCE: turbodrill turbine pressure stage consists of stator pressure stage hub and stator blade ring having internal rim, rotor pressure stage consisting of hub and rotor blade ring having external rim, radii centers conjugating undercut-outlet edges of blades on surface external back side of their profiles with minimal sizes of radii outlining on external-back size of zone of maximum thickness of blade profiles of stator and rotor blade rings and located on or below line determining undercut of outlet edges. EFFECT: reduced labour input of turbine manufacture and higher turbine operate reliability. 3 dwg
Title | Year | Author | Number |
---|---|---|---|
VORTEX PRESSURE STAGE OF TURBO-DRILL TURBINE | 2003 |
|
RU2236534C1 |
TURBODRILL TURBINE | 2004 |
|
RU2269631C1 |
PRESSURE STAGE OF TURBINE OF TURBO-DRILL | 2000 |
|
RU2174584C1 |
TURBODRILL-REDUCTION GEAR | 2002 |
|
RU2198994C1 |
TURBINE OF TURBODRILL | 2009 |
|
RU2403366C1 |
LOW-PRESSURE COMPRESSOR OF GAS TURBINE ENGINE OF AVIATION TYPE | 2016 |
|
RU2614708C1 |
LOW-PRESSURE COMPRESSOR OF GAS TURBINE ENGINE OF AVIATION TYPE | 2016 |
|
RU2614709C1 |
BALL BEARING | 2002 |
|
RU2224867C1 |
SHOCK ABSORBING SPINDLE | 2002 |
|
RU2224865C1 |
TURBODRILL TURBINE | 2006 |
|
RU2322563C1 |
Authors
Dates
2003-06-10—Published
2002-10-01—Filed