Published October 2015 | Version v1
Journal article

Progress on DEMO blanket attachment concept with keys and pins

Description

Highlights: • DEMO blanket attachment system with keys and pins (without using bolts). • Blanket segments are preloaded by progressively designed springs. • Blanket back plate flexibility has a major impact on spring design. • Mechanical analysis of other components indicates no unresolvable issues. • Thermal analysis indicates acceptable temperatures for the support system. - Abstract: The blanket attachment has to cope with gravity, thermal and electromagnetic loads, also it has to be installed and serviced by remote handling. Pre-stressed components suffer from stress relaxation in irradiated environments such as DEMO. To circumvent this problem pre-stressed component should be either avoided or shielded, and where possible keys and pins should be used. This strategy has been proposed for the DEMO multi-module segments (MMS). The blanket segments are held by two tapered keys each, designed to allow thermal expansions while providing contact with the vacuum vessel and to resist the poloidal and radial moments the latter being dominant at 9.1 MNm inboard and 15 MNm outboard. On the top of the blanket segment there is a pin which provides vertical support. At the bottom another vertical support has to lock them in position after installation and manage the pre-load on the segments. The pre-load is required to deal with the electromagnetic loads during disruption. This is provided by a set of springs, which require shielding as they are preloaded. These are sized to cope with the force (3 MN inboard, 1.4 MN outboard) due to halo currents and the toroidal moment which can reverse. Calculations show that the flexibility of the blanket segment itself plays a significant role in defining the required support system. The blanket segment acts as a preloaded spring and it has to be part of the attachment design as well.

Availability note (English)

Available from http://dx.doi.org/10.1016/j.fusengdes.2015.04.020

Additional details

Identifiers

DOI
10.1016/j.fusengdes.2015.04.020;
PII
S0920-3796(15)00249-5;

Publishing Information

Journal Title
Fusion Engineering and Design
Journal Volume
98-99
Journal Page Range
p. 1674-1677
ISSN
0920-3796
CODEN
FEDEEE

Conference

Title
28. symposium on fusion technology
Acronym
SOFT-28
Dates
29 Sep - 3 Oct 2014
Place
San Sebastian (Spain)

INIS

Country of Publication
Netherlands
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
48006683
Subject category
S42: ENGINEERING; S70: PLASMA PHYSICS AND FUSION TECHNOLOGY;
Resource subtype / Literary indicator
Conference
Descriptors DEI
CONTAINERS; FASTENERS; FLEXIBILITY; GRAVITATION; HEATING LOAD; PLATES; REMOTE HANDLING; SHIELDING; SPRINGS; STRESS RELAXATION; THERMAL ANALYSIS; THERMAL EXPANSION; TOKAMAK DEVICES; VACUUM SYSTEMS
Descriptors DEC
CLOSED PLASMA DEVICES; EXPANSION; MACHINE PARTS; MECHANICAL PROPERTIES; RELAXATION; TENSILE PROPERTIES; THERMONUCLEAR DEVICES

Optional Information

Copyright
Copyright (c) 2015 Elsevier Science B.V., Amsterdam, The Netherlands, All rights reserved.