TURBINE BLADE Russian patent published in 2001 - IPC

Abstract RU 2173389 C2

FIELD: turbine blades. SUBSTANCE: turbine blade 1 has incident flow rate 8, running-off flow part 9 and opposite pressure side 10 and back 11 located between parts 8 and 9, and also wall structure 2 flowed around with fluid medium 18. Wall structure 2 has external wall 3 which surrounds member 16 for cooling fluid medium 6. Discharge member 16 has thickening part 14 directed toward internal space 21. Average thickness of external part 3 at least partially is less than 2.5 mm. EFFECT: higher intensity of cooling. 14 cl, 4 dwg

Similar patents RU2173389C2

Title Year Author Number
BLADE FOR GAS TURBINE, IMPLEMENTATION OF TURBINE BLADE AND PROCEDURE FOR TURBINE BLADE COOLING 2005
  • Bal'Dauf Shtefan
  • Khendler Mikhel'
  • Lerner Kristian
RU2393356C2
METHOD AND DEVICE FOR TANGENTIAL SHIFTING INNER COOLING AT FIXED BLADE OF NOZZLE 2009
  • Batler Dehvid
RU2518775C2
GAS TURBINE BLADE 2011
  • Bregman Vitalij
  • Petukhovskij Mikhail
RU2573085C2
TURBINE BLADE AND GAS TURBINE INCORPORATING THIS BLADE 2005
  • Bal'Dauf Shtefan
  • Bolms Khans-Tomas
  • Khendler Mikhel'
  • Lerner Kristian
RU2333364C2
TURBINE BLADE 2007
  • Akhmad Fati
RU2405940C1
GAS TURBINE WITH THERMAL PROTECTION AND CONTROL METHOD 2012
  • Daun Ehndrju
RU2537113C1
CLEARANCE PACKING MEMBER AND GAS-TURBINE UNIT 1996
  • Mirko Milazar
  • Fridkhel'M Tershjuren
  • Al'Fred Linert
RU2162556C2
TURBINE DESIGN AND METHOD TO COOL BAND INSTALLED NEAR TURBINE BLADE EDGE 2008
  • Maltson Dzhon Dehvid
RU2462600C2
ECCENTRIC CHAMFER AT ENTRY OF BRANCHES OF FLOW CHANNEL 2008
  • Moltson Dzhon Dehvid
RU2456459C2
APPARATUS FOR DETERMINING DISTANCE BETWEEN MOVING BLADE AND WALL OF MACHINE FOR CONVERTING FLOW KINETIC ENERGY TO MECHANICAL ENERGY SURROUNDING MOVING BLADE 2007
  • Bossel'Mann Tomas
  • Vill'Sh Mikhel'
RU2440555C2

RU 2 173 389 C2

Authors

Shojrlen Mikhel'

Khendler Mikhel'

Dates

2001-09-10Published

1998-02-20Filed