FIELD: power engineering.
SUBSTANCE: shell is fully or partially made of a composite material with a ceramic matrix containing fibres of silicon carbide (SiC) as reinforcement of the matrix and a phase-to-phase layer between the matrix and fibres. The matrix contains at least one carbide selected from titanium carbide (TiC), zirconium carbide (ZrC) or triple carbide of titanium-silicon (Ti3SiC2). The method to manufacture a shell of nuclear fuel includes, in particular, manufacturing of a fibre pre-mould, application of a phase-to-phase layer on it with chemical steam infiltration, application of the matrix.
EFFECT: reliable mechanical retention of products of nuclear fuel fission inside a shell during radiation, at the same time optimal transfer of heat energy to coolant is provided.
2 cl, 2 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF FABRICATING COMPOSITE PARTS BY LOW MELTING POINT IMPREGNATION | 2014 |
|
RU2668431C2 |
MULTI-LAYER COMPOSITE FUEL COATING SYSTEM WITH HIGH TEMPERATURE AIR TIGHTNESS AND RESISTANCE TO NON-STANDARD SITUATIONS | 2016 |
|
RU2743178C2 |
COMPOSITE MATERIAL (VARIANTS) AND METHOD OR PREPARING THEREOF, METHOD OF TREATING FIBROUS SEMI-FINISHED PRODUCT (VARIANTS) | 1997 |
|
RU2176628C2 |
MULTILAYER COMPOSITE FUEL COATING SYSTEM WITH HIGH-TEMPERATURE TIGHTNESS AND STABILITY TO EMERGENCY SITUATIONS | 2016 |
|
RU2732465C2 |
AIRCRAFT ENGINE OUTLET CONE AND REAR HOUSING | 2013 |
|
RU2625421C2 |
METHOD OF MAKING PART FROM COMPOSITE MATERIAL WITH CERAMIC MATRIX | 2017 |
|
RU2728791C2 |
FUEL ELEMENT WITH COMPOSITE PROTECTIVE COATING | 2019 |
|
RU2740701C2 |
DEVELOPED SIC-SIC COMPOSITE AND MONOLITHIC LAYERED SIC STRUCTURES | 2017 |
|
RU2720579C1 |
METHOD FOR SURFACING PART MADE OF COMPOSITE WITH CERAMIC MATRIX | 2009 |
|
RU2520108C2 |
METHOD FOR MANUFACTURING A CERAMIC MULTILAYER TUBE FOR THE SHELL OF A FUEL ELEMENT OF A NUCLEAR POWER PLANT | 2020 |
|
RU2762000C1 |
Authors
Dates
2014-01-10—Published
2009-09-18—Filed