FIELD: foundry.
SUBSTANCE: gating system comprises casting bowl (2), vertical pipe (3), distributor (4) arranged at lower end of vertical pipe, and at least one sprue channel system (5, 5', 5"), connected to at least two molds (7). Runner channels system comprises gating channel (51, 151, 251), first section (51a, 151a, 251a) of which is located in first direction (A) from distributor (4) and two second sections (51b, 151b, 251b) are located in second direction (B), note here that every second section is arranged at first section outlet and communicated with first section via adapter 52, 152, 252. Each mold (7) is connected to second section (51b, 151b, 251b) of sprue channel. Damping channel (54, 154, 254) extends the first section of the sprue channel and has first end (54a, 154a, 254a) communicating with adapter (52, 152, 252), and second end (54b, 154b, 254b) made closed. Damping channel allows to slow down the first metal jet and to weaken the hydraulic impact.
EFFECT: excluding ingress of non-metallic inclusions in casting mold.
10 cl, 5 dwg
Title | Year | Author | Number |
---|---|---|---|
CASTING MOULD FOR PRODUCTION OF MONOCRYSTALLINE VANE BY CASTING, INSTALLATION AND METHOD OF MANUFACTURING, USING CASTING MOULD | 2017 |
|
RU2730827C2 |
BLADE EQUIPPED WITH SHELVES CONTAINING INSERTS | 2016 |
|
RU2699857C2 |
CASTING MOLD FOR MONOCRYSTALLINE CASTING | 2015 |
|
RU2686163C2 |
ROD FOR CASTING AN AIRCRAFT PART | 2019 |
|
RU2772561C2 |
GAS TURBINE ENGINE BLADE EQUIPPED WITH A COOLING SYSTEM AND METHOD OF MANUFACTURING SUCH BLADE BY CASTING USING SMELTED WAX MODELS | 2020 |
|
RU2800619C2 |
MECHANISED TOOL | 2010 |
|
RU2483864C2 |
PREFORM AND ONE-PIECE BLADE FOR GAS TURBINE ENGINE | 2013 |
|
RU2653823C2 |
CENTER RUNNER UNIT | 2003 |
|
RU2297303C2 |
IMPROVED METHOD FOR MANUFACTURING SHELL MOULD FOR PRODUCTION BY LOST-WAX CASTING OF BLADED ELEMENTS OF AN AIRCRAFT TURBINE ENGINE | 2015 |
|
RU2685614C2 |
WHEEL FOR SEED BURYING SYSTEM | 2020 |
|
RU2811098C2 |
Authors
Dates
2020-09-18—Published
2017-05-10—Filed