Case
Study
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Emirates Air Line
(London Cable Car)
-
Multi-award
winning first urban
cable car for the United Kingdom
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Category 3 design
check
of main steel towers to Eurocodes
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Design of cable
car stations and adjacent compression towers
The Emirates Air Line is the UK's first
urban cable car and one of the latest crossings of the River Thames in London. The
1.1km long crossing connects the Royal Greenwich peninsula to the
Royal Victoria Dock and forms
part of a long term regeneration plan for East London. The Design and
Build contract was awarded by Transport for London to main contractor Mace.
Structural design was shared between Buro Happold, who were responsible for the design
of the three main towers, and URS (now AECOM), who designed the stations and
adjacent compression towers. AECOM also carried out a Category 3 check of the
design of the main towers using LUSAS Civil & Structural analysis software
and LUSAS consultancy services to assist with this task.
Overview
The height and positioning of the
three main towers were dictated by a number of site
constraints. The main South and North towers had to be tall enough
to provide sufficient navigational clearance to the suspended
gondolas for shipping. Ideally, the South Tower would have been
positioned out of the river, but the development plot for the South
Station was fixed, and very close to the river. This meant that the
tower's positioning was governed by the steepest practical ascent
rate for the system resulting in it being located in the river just outside of
the shipping lane. The North Tower is land-based and sited to
accommodate the
curved route of a potential future tunnel
across the river at the same location as the cable car. The height of the North Intermediate tower
was restricted by it being on the flight path from London City
airport and its longitudinal position was dictated by the presence of the existing Docklands light rail
line and road network.
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Cable car
location and profile |
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Royal Victoria
Dock as viewed from Emirates Air Line with London City Airport in
the distance |
Main Towers
The 450 tonne South and North main towers each stand over 85m in height. They are formed from four, 40mm thick, steel plated ribbons that are doubly-curved and twist in an anti-clockwise direction as they rise in height. These ribbons, in turn, are stiffened internally by helical braces, formed from Circular Hollow Sections (CHS) faced with a steel plate, that twist in an opposing direction to the ribbons. Both towers taper from 10m diameter at their base, remain circular in cross-section until, at a height of around 53m, they become elliptical prior to being capped with a collar section. Then, they split and flare into two separate arms to carry the structural frame that supports the cable car yoke structure. In the narrow mid-section of each tower five torsion rings, fitted in addition to the helical steel, provide additional resistance to twisting forces. Two main ribbon to helix connection types are used in each tower. Near the base of the tower the length of the helix CHS that sits behind the ribbon is boxed out with steel plates. Further up the tower a large diameter CHS drum onto which the bracing members are fixed is used instead, with horizontal splice plates being used at any bolted joints. The smaller, 320 tonne, North Intermediate tower is similar in design to the taller main towers but has a 5.67m diameter footprint and stands just 60m in height. The towers were fabricated in segments then welded together to form larger sub-components that were lifted into position and bolted together.
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Base of South
Tower |
Top of South
Tower |
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Location of North Tower |
Modelling
methodology
As a consequence of their structural
configuration the towers are flexible torsionally. They rely on the moment fixity of the ribbon and helix connections to
restrict the rotational displacement of the top of each tower to the
0.003 radian
rotation limit specified by Doppelmayr, the cable car
installers. As part of its
comprehensive overall design check, AECOM carried out a global
analysis of the towers to check for compliance with overall
deflection limits at the Serviceability Limit State. For the tower
analysis a LUSAS
geometry model was created via a
tailored IGES import. It was not viable to use
shell elements to represent all the structural components in the tower
in detail, so the upper arms of the head, the ribbons and the helix connection stiffeners were modelled using
thick shells, and thick beam elements represented the helix
CHS and all other
members. To ensure that the behaviour of the tower would be captured
correctly when the ribbon and helix connections were modelled in
this way detailed localised calibration studies were carried out
for the two basic connection types used.
James Rowe, Technical
Director, AECOM
said: "Results from connection models made exclusively
from shell
elements were
compared to those from comparable nodes on the same connections modelled
with shells and beams. This allowed the plate thicknesses for
the joints on the global model to be artificially adjusted to ensure
the connections on the global model were of the correct stiffness."
He continues: "Ensuring that the LUSAS tower models correctly
represented the ribbon to helix connections was a key step towards
us verifying the original structural design as part of the Category 3 check,
and ultimately confirming its adequacy to EC3."
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Beam and shell
element sensitivity model
of a can-type ribbon/helix connection
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Shell
element sensitivity model
of a can-type ribbon/helix connection
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Beam and shell element
sensitivity model
of a plated ribbon/helix connection
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Shell element
sensitivity model
of a plated ribbon/helix connection
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Global beam and
shell model of
tower
showing selected key parts
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Sensitivity modelling of connections
and global modelling of tower
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Modelling and
analysis
Models of each tower were built in
LUSAS and similar analyses and checks were carried out for each. In
modelling the South Tower around 130 multi-varying cross-section
properties needed to be
defined and assigned to the model geometry. In addition to the connection sensitivity studies
previously described, mesh sensitivity analyses for the whole tower
derived an optimum number of beam and shell elements for the
accuracy required and for the numerous analyses
that needed to be carried out.
Eigenvalue frequency analyses took account of the stiffnesses of the
substructures and included significant lumped masses (3 x 12.1 tonnes
in the case of the South Tower) that represented the weight of cable car support
systems applied to the support frame at the top of the towers. From these analyses it was seen that,
for each tower, the first mode shape was
orthogonal to the run of the cables, the second was generally an
in-plane mode, and the
third was a torsional mode. By performing a global linear buckling
analysis on the tower for the most adverse design load combination
it was found that a second order analysis was not required. However, a geometrically
nonlinear analysis was also performed to confirm this and showed a minimal increase in deformations in comparison to the linear analysis undertaken.
Loading for the towers consisted of
three main components: cable car loading to the top of each tower;
direct wind loading on the tower surfaces and other wind induced
loads (to BS EN 1991-1-4:2005 and NA); and temperature loading from
direct sun irradiation (to BS EN 1991-1-5:2003).
Wind loading actions were of particular
interest and required wind tunnel testing and detailed analytical
evaluation to assess potential flutter, vortex shedding, galloping and
buffeting effects. Accidental loadings
considered derailment of the cable cars; deropement of the cable;
loss of support to a ribbon at base level, and fire - which involved checking the stress and buckling in the structure for localised reduced
Young’s modulus and Yield stress.
To assist with the ULS and SLS checks
on the towers, numerous project-specific VB scripts were developed for
use with LUSAS to allow for slicing through the model to create
results for multiple loadcases; for
enveloping shell stresses; and for the calculation of modal rotational inertia for torsional modes of vibration.
The large number, variety
and complex arrangement of the loadings meant that many combinations
and design cases needed to be considered. VB scripting was employed
here too, automating the creation of over 700 load combinations and envelopes.
Use of the scripts in conjunction with other results from the vast
range of LUSAS analyses undertaken allowed stresses in the ribbons,
stiffeners, diaphragms and welds to
be obtained and verified.
Representative
results plots
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Wind
loading in X-direction |
Deformed
shape (exaggerated) from rope (cable) loading |
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Thermal strain
on ribbons |
Stress in
ribbons from full spectrum envelope |
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Stress
in ribbon stiffeners |
Stress in collar
stiffeners |
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Stress
in head arms |
Stress
in head stiffeners |
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Modelling of the North and South
Stations and
adjacent compression towers was also carried out by
AECOM using LUSAS. Details of
the
analyses undertaken are beyond the scope of this case study.
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North terminal
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South
terminal
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South
terminal concrete modelling |
South
terminal steelwork modelling |
In summary
Emirates Air Line gets its name from the
Emirates airline who substantially part-sponsored its construction. Its 34 gondolas have the capacity to carry up
to 2,500 people per hour in each direction. It opened to the public in July 2012 after
a rapid 15 month design
and construction period.
Project team
- Main Contractor: Mace
- Architect: Aedas Architects
- Consulting Engineers: Buro Happold
/ URS (now AECOM)
- Steelwork Fabricator: Watson Steel
Structures Ltd.
- Piling/Foundations: Soletanche Bachy
- Cable car installation: Doppelmayr
Awards
"The use and
assistance of LUSAS in conjunction with our own substantial in-house
expertise allowed us to carry out a challenging Category 3
design check on a very unusual structure within a very tight
timescale"
James Rowe, Technical
Director, AECOM
Find out more
Other LUSAS Civil &
Structural case studies:
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