FIELD: machine building.
SUBSTANCE: invention relates to simulation of at least part of bathtub (2) of turbine blade (1). Disclosed is a simulation method, characterized in that it includes, using data processing equipment (11) means (10), steps of: (a) parameterising volume (V) displaying said portion of bathtub (2) as a collection of sections (20) extending from support transverse surface (S) of blade (1), wherein blade (1) physically comprises sections (20), and each section (20): is connected to elementary surface (Si) selected from plurality of elementary surfaces (Si), forming separation of at least part of said support transverse surface (S); and is determined by section height relative to said support surface (S); (b) determining optimized values of sections heights relative to a given aerodynamic and/or thermal criterion; (c) at interface (13) of said equipment (10) reproduce determined thus values.
EFFECT: technical result consists in enabling analysis of various geometry of blades with reduced use of computer resources.
14 cl, 6 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF SIMULATION OF AXIALLY SYMMETRIC SURFACE | 2014 |
|
RU2670380C2 |
METHOD FOR MODELLING PART, IN PARTICULAR TURBINE BLADE | 2014 |
|
RU2665216C2 |
TURBOMACHINE COMPONENT OR COLLECTION OF COMPONENTS AND ASSOCIATED TURBOMACHINE | 2014 |
|
RU2666933C1 |
METHOD FOR MODELLING NON-STREAMLINED PROPELLER BLADE | 2014 |
|
RU2670330C2 |
METHOD AND DEVICE FOR ELECTROLYTIC DEPOSITION OF COATING | 2010 |
|
RU2567143C2 |
TURBOMACHINE COMPONENT WITH NON-AXISYMMETRIC SURFACE | 2014 |
|
RU2672990C1 |
TURBOMACHINE COMPONENT WITH NON-AXISYMMETRIC SURFACE | 2014 |
|
RU2675980C2 |
OPTIMISATION OF CYCLE FATIGUE OR CYCLE AND HIGH-CYCLE FATIGUE TEST BENCH | 2014 |
|
RU2665186C2 |
METHOD OF RESTORING ONE-PIECE BLADED DISK AND TEST PIECE (VERSIONS) | 2006 |
|
RU2397329C2 |
METHOD OF HARD TO WELD MATERIALS PRODUCTION | 2017 |
|
RU2742963C1 |
Authors
Dates
2019-07-23—Published
2015-07-10—Filed