GB2071396A - Structural shells - Google Patents
Structural shells Download PDFInfo
- Publication number
- GB2071396A GB2071396A GB8007462A GB8007462A GB2071396A GB 2071396 A GB2071396 A GB 2071396A GB 8007462 A GB8007462 A GB 8007462A GB 8007462 A GB8007462 A GB 8007462A GB 2071396 A GB2071396 A GB 2071396A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shell
- load
- local
- protuberances
- structural
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
Classifications
-
- G—PHYSICS
- G21—NUCLEAR PHYSICS; NUCLEAR ENGINEERING
- G21C—NUCLEAR REACTORS
- G21C5/00—Moderator or core structure; Selection of materials for use as moderator
- G21C5/02—Details
- G21C5/10—Means for supporting the complete structure
-
- G—PHYSICS
- G21—NUCLEAR PHYSICS; NUCLEAR ENGINEERING
- G21C—NUCLEAR REACTORS
- G21C13/00—Pressure vessels; Containment vessels; Containment in general
- G21C13/08—Vessels characterised by the material; Selection of materials for pressure vessels
- G21C13/087—Metallic vessels
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E30/00—Energy generation of nuclear origin
- Y02E30/30—Nuclear fission reactors
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Plasma & Fusion (AREA)
- General Engineering & Computer Science (AREA)
- High Energy & Nuclear Physics (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
A structural shell for housing a nuclear reactor fuel assembly carried from the wall of the shell is pressurised and has outwardly directed pre-formed protuberances at the load-points. The preformed protuberances are of proportions generally similar to the notional deflections that would be caused by the load in a normal membrane wall. Bending moments local to the load points are reduced. <IMAGE>
Description
SPECIFICATION
Structural shells
This invention reiates generally to structural shells but is primarily directed to steel shells for housing loads carried from the wall thereof.
It is known that curved thin plates or membranes are well suited for carrying distributed loads such as occur in roof structures of buildings and pressure vessels. When curved thin plates or membranes are required to carry concentrated loads, deflections local to the load points or load lines can occur thereby inducing severe bending stresses. In conventional shells, the stresses are reduced to acceptable levels by increasing the thickness of the plate or membrane local to the load points or load lines, but it is an object of the invention to provide a structural shell wherein increased wall thicknesses are avoided.
According to the invention, a structural shell carrying a concentrated load from a wall thereof is pressurised and is profiled to include protuberances formed local to the load points or load lines, the protuberances being directed away from the load.
The protuberances, which preferably correspond generally in shape and proportions to the notional deflection that would be produced in a generally similar shell without protuberances under the same load conditions, reduce the local bending moment to a value lower than would be induced in the generally similar shell and pressure in the shell provides a bending moment of opposite sign to counteract the bending moment induced by the load.
The invention finds application in a nuclear reactor containment shell for housing a nuclear fuel assembly carried from a wall of the shell, wherein the shell is pressurised with an inert gas or liquid coolant and is provided with protuberances local to the load points or lines and directed outwardly of the shell.
In a preferred nuclear reactor construction the nuclear fuel assembly is carried by a skirt from a generally spherical region of the containment shell and a circumferential protuberance local to the load line consists in two opposed frusto-conical surfaces disposed tangentially to the spherical surface.
The invention will be more readily understood from the following description of the shells of two alternative nuclear reactor constructions which embody the invention, the embodiments being described by way of example only and with reference to the accompanying diagrammatic drawings Figs 1 and 2 which are fragmentary sectional views.
In Fig 1 a vessel designated 1 represents a generally cylindrical shell open at its upper end and having a hemispherical lower end. A nuclear reactor fuel assembly is carried on a skirt 2 from
the hemispherical region of the wall of the shell
and is submerged in liquid alkali metal coolant.
The region of the shell local to the circumferential
load line designated 'L' forms a protuberance to
the profile of the shell the protuberance being
directed outwardly and formed by two frusto
conical sections each of which is tangential to the
part spherical adjoining regions. In such a
construction the load of the fuel assembly is
resisted mainly by the hoop stress in the vessel
along the load line, but also by the bending stress
induced at the junction of the conical sections and
by the membrane stiffness of the protuberance.
Consideration of the geometry shows that the
membrane stiffness is greater than it would be in
the part spherical membrane of a conventional
shell (shown in broken line) so that the bending
moment is reduced correspondingly. The pressure
of the liquid metal on the conical sections provides
a bending moment of opposite sense to that of the
load so that the resultant bending stress is
reduced.
Fig 2 shows a section of a similar shell having
an open upper end and a generally hemispherical
lower and wherein the lower end is fabricated
from curved sections the intersection (designated
'I') of which is at a non-tangential point thereby
providing a protuberance extending about the
shell. The load line is arranged to coincide with the
intersection of the sections.
It should be noted that for the optimum
conditions a balance of the various parameters
affecting stresses is required and the vessel
geometry to be adopted will depend on the
prevailing conditions but nevertheless both the
described constructions provide an improved
structural shell wherein the stresses induced by a
concentrated load can be accommodated without the need for increased wall thickness local to the load line.
1. A structural shell carrying a concentrated load from a wall thereof, the shell being pressurised and profiled to include preformed protuberances local to the load points or load lines, the protuberances being directed away from the load.
2. A structural shell according to claim 1 the shell constituting a containment for a nuclear reactor fuel assembly which is carried from the wall of the shell, wherein the shell is pressurised with an inert gas or liquid coolant and is provided with preformed protuberances local to the load points or lines and directed outwardly of the shell.
3. A structural shell according to claim 2 wherein the nuclear fuel assembly is carried by a skirt from a generally spherical region of the containment shell and a preformed circumferential protuberance local to the load line consists in two opposed frusto-conical surfaces disposed
**WARNING** end of DESC field may overlap start of CLMS **.
Claims (4)
1. A structural shell carrying a concentrated load from a wall thereof, the shell being pressurised and profiled to include preformed protuberances local to the load points or load lines, the protuberances being directed away from the load.
2. A structural shell according to claim 1 the shell constituting a containment for a nuclear reactor fuel assembly which is carried from the wall of the shell, wherein the shell is pressurised with an inert gas or liquid coolant and is provided with preformed protuberances local to the load points or lines and directed outwardly of the shell.
3. A structural shell according to claim 2 wherein the nuclear fuel assembly is carried by a skirt from a generally spherical region of the containment shell and a preformed circumferential protuberance local to the load line consists in two opposed frusto-conical surfaces disposed tangentially to the spherical surface.
4. A structural shell substantially as hereinbefore described with reference to either
Figure 1 or Figure 2 of the accompanying drawings.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8007462A GB2071396A (en) | 1980-03-05 | 1980-03-05 | Structural shells |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8007462A GB2071396A (en) | 1980-03-05 | 1980-03-05 | Structural shells |
Publications (1)
Publication Number | Publication Date |
---|---|
GB2071396A true GB2071396A (en) | 1981-09-16 |
Family
ID=10511879
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8007462A Withdrawn GB2071396A (en) | 1980-03-05 | 1980-03-05 | Structural shells |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2071396A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2541811A1 (en) * | 1983-02-25 | 1984-08-31 | Novatome | NUCLEAR REACTOR TANK WITH QUICK NEUTRONS |
-
1980
- 1980-03-05 GB GB8007462A patent/GB2071396A/en not_active Withdrawn
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2541811A1 (en) * | 1983-02-25 | 1984-08-31 | Novatome | NUCLEAR REACTOR TANK WITH QUICK NEUTRONS |
EP0119125A1 (en) * | 1983-02-25 | 1984-09-19 | Novatome | Vessel of a fast breeder reactor |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |