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Revision 1.8 by carlo, Thu May 21 10:26:25 2009 UTC

# Line 1 | Line 1
1   \section{Integration Procedures}
2   \label{sec:Procedures}
3 < TIB and TID have different integration procedures, each one being optimised
3 > The TIB and TID have different integration procedures, each one being optimised
4   for the geometry and the best installation and test logical sequence.
5   In this section the steps done to assembly a TIB shell and a TID
6   ring will be described also mentioning the tests performed in between and
# Line 31 | Line 31 | A picture of a Layer 4 mechanical struct
31   \begin{center}
32    \includegraphics[width=0.85\textwidth]{Figs/bench.pdf}
33   \end{center}
34 < \caption{A shell carbon fiber structure mounted on the integration bench. The cooling pipes
35 < and ledges of inner part of the shell are visible.}
34 > \caption{A shell carbon fiber structure mounted on the integration bench.
35 > The cooling pipes
36 > and ledges of inner part of the shell are visible. Stickers, containing
37 > bar codes to identify the strings, are temporary fixed on the structure.}
38   \label{fig:bench}       % Give a unique label
39   \end{figure}
40  
# Line 121 | Line 123 | that comes with the correct address CCUM
123   \begin{center}
124    \includegraphics[width=0.60\textwidth]{Figs/mc_detail_full.png}
125   \end{center}
126 < \caption{A symplified detail of the $r\phi$ section of TIB L3
125 <  mechanical drawing.}
126 > \caption{A symplified $r\phi$ view of TIB L3 as seen from the front-flange.}
127   \label{fig:l3detail}       % Give a unique label
128   \end{figure}
129  
130  
131   \subsubsection{Module Mounting}\label{sect:tibmodules}
132 < Both single modules and double sided module assemblies are mounted on the shell by hand.
132 > %Both single modules and double sided module assemblies are mounted on the shell by hand.
133   The module  is supported below the front-end
134 < hybrid and on the opposite side by two ledges support that precisely
135 < define the module position and act as heat sink
136 < %for the front-end hybrid and the sensor generated power
137 < being in contact with the cooling pipes.
134 > hybrid and on the opposite side by two aluminum ledges that precisely
135 > define its position and, being in contact with the cooling pipes,
136 > act as heat sink.
137 > %for the front-end hybrid and the sensor generated power
138   The shape of the ledges is different for the single sided modules and
139   for the double-sided module assemblies. In the latter case the
140 < ``stereo'' module sits on the structure upside-down and the ledge
141 < below the hybrid has a milled slot to ensure enough room to the
140 > ``stereo'' module sits on the structure upside-down and the hybrid ledge
141 > has a milled slot to leave enough room for the
142   front-end hybrid. The ledge on the opposite side has two different
143   shapes reflecting the two orientations of the ``stereo'' modules.
144   Each ledge has two M1 threaded holes. One is concentric with a 2mm
145   diameter socket.
146   The module features one precision pin on both short sides that fits
147 < into the socket (Fig. \ref{fig:insets} c). The milling of the socket and the glueing of the
148 < ledge onto the shell is done by using the same reference, i.e. the
149 < ledge edges, so to ensure an accurate positioning.
147 > into the socket (Fig. \ref{fig:inserts} c).
148 > The milling of the socket and the glueing of the
149 > ledge onto the shell are both done by using the same reference, i.e. the
150 > precisely machined ledge edges, so to ensure an accurate positioning.
151   The module pin at the hybrid side is glued onto the module frame. The
152   one at the opposite side, however, fits into an 'U'-shaped
153 < slot a design that allows for movements along the module long side. In
154 < a device that will be affected to huge temperature changes, this is an
155 < essential feature to compensate for thermal variations while ensuring
156 < mechanical precision.
153 > slot a design that allows for movements along the module long side.
154 > With such a constraint it is always possible to easily screw down the module
155 > regardless of the small construction tolerances on the relative position
156 > of the four holes set.
157 > %In a device that will be affected to huge temperature changes, this is an
158 > %essential feature to compensate for thermal variations while ensuring
159 > %mechanical precision.
160  
161   Before mounting a module on the shell the structure is rotated to place
162 < the corresponding string in a confortable and horizontal
163 < position. Then the module inventory database is queried for an
162 > the corresponding string in a horizontal position to ease the following
163 > operations.
164 > FIXME: Introdurre l'inventory database prima delle procedure d'integrazione,
165 > in modo da poterlo nominare qui, e anche prima quando si parla del montaggio
166 > di MC e AOH.
167 > Then the module inventory database is queried for an
168   appropriate module. The answer depends on module type and availability
169   at the integration centre and on the module depletion
170   voltage (see par.~\ref{sec:biasandvdepl}). \\
# Line 171 | Line 180 | a considarable fraction of the time spen
180   The single sided module or the double side modules assembly is mounted
181   on the structure by hand. It is first leaned onto the ledges and then is
182   gently slit until the pin at the hybrid side enters into the precision
183 < socket. Now can only the rotation around the pin axis is possible.
183 > socket. At this stage only a rotation around the pin axis is possible.
184   The mounting is completed by inserting in the corresponding precision
185   socket the T-shaped aluminum pin placed in the U-shaped slot
186 < (Fig. \ref{fig:insets} b) located on the frame short side opposite to
186 > (Fig. \ref{fig:inserts} b) located on the frame short side opposite to
187   the hybrid. The module is finally tighetned by the four M1 screws by
188   using a limited-torque screw driver.
189  
190   \begin{figure}[tbh]
191   \centering
192   \includegraphics[width=.7\textwidth]{Figs/collage.pdf}
193 < \caption{TIB single-sided module insets:
193 > \caption{TIB single-sided module inserts:
194   \textbf{a:} The U-shaped slot glued on the carbon fiber module frame;
195   \textbf{b:} the T-shaped pin inserted in the slot (seen from below);
196   \textbf{c:} front-end hybrid side precision insertion pin (seen from below).}
197 < \label{fig:insets}
197 > \label{fig:inserts}
198   \end{figure}
199  
200   The clearance between the module most fragile parts (bondings)
201 < and the other surrounding structures when the operation is performed (cooling pipes and ledges of the
202 < adjacent strings and modules already mounted) are, in case of single-sided modules,
201 > and the other surrounding structures when the operation is performed
202 > (cooling pipes and ledges of the
203 > adjacent strings and modules already mounted) are, in case of single-sided
204 > modules,
205   sufficiently large for a safe operation. For the double-sided module
206 < assemblies the cleareances are much reduced, of the order or less than a millimeter.
206 > assemblies the cleareances are much reduced being
207 > of the order or less than a millimeter.
208   In this case, to ease the mounting, a simple mechanical guidance
209   template has been designed to further reduce the risk of possible
210   accidental damage of the microbonds or the sensor.
211 + This template is temporary mounted using the ledges of the adjacent string
212 + and prevents the  module to move into positions where its bondings
213 + can touch the mechanics. When the module is safely screwed into position
214 + the template is removed.
215  
216   Once a module or a double sided assembly is mounted its basic
217   functionality is tested by feeding low voltages and checking I$^2$C
218   communications with the various devices present on the hybrid, the CCU
219   on the mother cable and the AOH. This also allows the module identity
220 < to be certified by using the DCU hardware ID.
221 < Once a string of three or six modules is completed the I$^2$C
220 > to be certified by reading the DCU hardware ID.
221 > Once a string  is completed the I$^2$C
222   communications are checked again and a pedestal and noise run is taken
223 < with a HV bias at 400V. For the tests complete description see
223 > with a bias voltage of 400V. For the tests complete description see
224   section~\ref{sec:Tests}.
225  
226   \subsubsection{Control Ring Installation}
227 < The control electronics that supervises the control ring, i.e. the
228 < DOHM boards and in case the AUXs, are located on a carbon fiber skin
229 < are mounted on the shell external surface just above the modules by carbon fiber pillars and aluminum supports (Fig. \ref{fig:dohm}).
230 < A thin aluminum foil has been glued on the skin and electrically grounded
227 > The control electronics that supervises the control ring
228 > (DOHM and AUX boards) are located on a carbon fiber skin which is
229 > mounted on the shell external surface, just above the modules,
230 > by carbon fiber pillars and aluminum supports (Fig. \ref{fig:dohm}).
231 > A thin aluminum foil has been glued on the carbon fiber
232 > skin and electrically grounded
233   to reduce possible interference between the logical control signals and
234   the module analog electronics. All mother cables are then connected to
235 < the DOHM (and AUX) ports by using a set of appropriately terminated
235 > the DOHM (and AUX) ports by using a set of appropriately shaped
236   flat-cables that have been preprared before, on the empty structure,
237 < by using dummy replicas of the DOHS/AUX boards and mother cables.
237 > by using dummy replicas of the DOHM/AUX boards and mother cables.
238  
239 < Each shell needs of three to six Control Rings, generally
240 < differing also withinh the same shell with respect to the number of
239 > Each shell is equipped by three to six Control Rings, generally
240 > differing also within the same shell with respect to the number of
241   served strings and the geographical distribution of these strings
242   into the shell.
243   For example, Layer 1 and 2, which are equipped with
244   double sided modules, have control rings of 3 to 5
245 < strings, while Layer three and four have 13 to 15 single sided strings.\\
245 > strings, while Layer 3 and 4 have 13 to 15 single sided strings.\\
246   \begin{figure}[!htb]
247   \begin{center}
248    \includegraphics[width=0.60\textwidth]{Figs/dohm.pdf}
249   \end{center}
250   \caption{A Layer 3 control ring circuitry during the cable preparation
251 <  witha DOHM and an AUX (the smaller board) with control ring cables
252 <  connected the mother cable heads (not visible).}
251 >  with a DOHM and an AUX (the smaller board) with control ring cables
252 >  connected to the mother cable heads (not visible).}
253   \label{fig:dohm}       % Give a unique label
254   \end{figure}
255  
# Line 243 | Line 261 | Each control cable path has been optimiz
261   very limited room available for services.
262   For layer three and four the part of the control cables
263   which is not protected by the carbon fiber plate
264 < is shielded using a thin Aluminum foil.\\
264 > is shielded using a thin aluminum foil.\\
265   The $4 \times 2$ optical fibers, which connect the two DOH to the FEC,
266 < are cerefully routed and protected at the flange. In fact the
266 > are carefully routed and protected at the flange.
267 > This is a critical point because it is true that the
268   redundancy architecture allows the ring to work also if the connection
269   to the master DOH fails, but the price to pay if both DOH connections
270 < fail is of the order of 1-2\% of the entire TIB.\\
270 > fail is of the lost of 1-2\% of the entire system.\\
271   The DOHM cabling is completed by the power cable, very similar to the
272 < mother cable 'medusas', and by the wiring of two PT1000 temperature
272 > mother cable 'medusas', and by the wiring of two PT1000~\cite{ref:pt1000}
273 > temperature
274   probes per control ring that comes already glued on the cooling manifolds.
275   The four probe wires are in fact routed through the DOHM via the Control
276   Ring power cable up to the power supply racks where the interlock
277   boards are also located. The four-wire resistance measurement
278   of the PT1000 is necessary to avoid the contribution of the
279   40 meter long power cable.
280 < Also a humidity meter is hosted on the DOHM board; it is read out
281 < through dedicated wires on the Control Ring power cable.
280 > Also a hygrometer (HMX2000~\cite{ref:hmx}) is hosted on the DOHM board; it is read out
281 > through dedicated wires on the Control Ring power cable. These sensors
282 > are used to monitor the TIB/TID enviromental conditions even
283 > without the tracker read-out switched on.
284  
285 < A thinner carbon fiber skin is used as a protecting cover. Electrical
285 > A thinner carbon fiber skin is used as a protecting and shielding
286 > cover of the control ring circutry. Also in this case electrical
287   shielding is ensured by an aluminum foil glued to the cover and
288 < grounded (Fig. \ref{fig:dohml1}). Finally the control ring is tested (see section \ref{sec:Tests}).\\ .
288 > grounded (Fig. \ref{fig:dohml1}).
289 > When completely installed
290 > the control ring is tested.
291 > A complete debug, including the control of the redundancy, is done
292 > at this level to spot possible malfunctioning which are relatively easy
293 > to repare at the integration centers. For a complete test description
294 > see section \ref{sec:Tests}\\ .
295  
296   \begin{figure}[tbh]
297   \centering
298   \includegraphics[width=.7\textwidth]{Figs/L1DOHM.pdf}
299   \caption{A Layer 1 completed with its control rings. The DOHM and cable area is covered with
300 < aa aluminum shielded carbon fiber plate.}
300 > an aluminum shielded carbon fiber plate.}
301   \label{fig:dohml1}
302   \end{figure}
303  
# Line 304 | Line 333 | assembly of rings into a disk.  Weight??
333    \includegraphics[width=0.7\textwidth]{Figs/R1-back.pdf}
334   %  \includegraphics[width=0.49\textwidth]{Figs/R3-front.pdf}
335   \end{center}
336 < \caption{ The TID integration crown  holding R1 rings in front (top) and back (bottom) positions.}
336 > \caption{ The TID integration crown  holding R1 rings in front (top)
337 > and back (bottom) positions. FIXME (Carlo): secondo me ne basta una, cosi'
338 > si salva un po' di spazio.}
339   \label{fig:ringbench}       % Give a unique label
340   \end{figure}
341   Once a new ring structure arrived, it was mounted on an integration crown. In order to identify easily the mother cable positions
# Line 402 | Line 433 | Disk assembly proceed for R1 on a R3, th
433    \includegraphics[height=0.6\textwidth]{Figs/DISK.pdf}
434   \end{center}
435   \caption{Disk assembled.}
436 < \label{fig:tidassembly}       % Give a unique label
436 > \label{fig:tidassembled}       % Give a unique label
437   \end{figure}
438  
439  
# Line 430 | Line 461 | It also contains a subset of the test da
461   devices and their functional status (good, broken, mounted, dismounted, etc...).\\
462   Along with module tests results also an important number is stored for each module:
463   the hardware identifier of the DCU chip
464 < embedded with the module (or DcuHardId). This code can be retrieved during data acquisition,
464 > embedded with the module.% (or DcuHardId).
465 > This code can be retrieved during data acquisition,
466   allowing for an unambiguous identification of a module.\\
467   A TIB/TID specific key was defined to store the location of mounted devices (named Geographical
468   Identifier, or GeoId): it is a string
469 < composed of numerical fields separated by dots, as described in Table~\ref{tab:geoids}.
469 > composed of numerical fields separated by dots.
470 > %, as described in Table~\ref{tab:geoids}.
471   Bar code stickers with the GeoId are glued on the mechanical structure
472 < before the integration starts (Fig. \ref{fig:stickers}).
440 <
441 < \begin{figure}[t]
442 < \centering
443 < \includegraphics[width=.6\textwidth]{Figs/stickers.pdf}
444 < \caption{An empty shell with the bar code stickers identifying the strings.}
445 < \label{fig:stickers}
446 < \end{figure}
472 > before the integration starts (Fig. \ref{fig:bench}).
473  
474 < The first 7 numbers in a GeoId identify the string to which a device belongs, while the last
475 < part of this code represents the physical location where the device is placed.
476 <
477 < \begin{table}[h!]
478 < \begin{center}
479 < \begin{tabular}{l|ccc}
480 <    & 1               & 2     & free value  \\
481 <    \hline
482 <  a & TIB             & TID              &             \\
483 <  b & Forward ($z>0$) & Backward ($z<0$) &             \\
484 <  c & Up ($y>0$)      & Down ($y<0$)     &             \\
485 <  d &                 &                  & Layer \#    \\
486 <  e & Inner           & Outer            &             \\
487 <  f &                 &                  & Manifold \# \\
488 <  g &                 &                  & String \#   \\
489 < \end{tabular}
490 < \caption[smallcaption]
491 < {A generic $a.b.c.d.e.f.g$ GeoId identifies a string and  must be interpreted according
492 < to this table. For example of GeoId 1.1.2.4.1.3.2 identifies the second string, of the
493 < third manifold placed in the inner surface of the Layer 4 Down Forward TIB shell.}
494 < \label{tab:geoids}
495 < \end{center}
496 < \end{table}
474 > %\begin{figure}[t]
475 > %\centering
476 > %\includegraphics[width=.6\textwidth]{Figs/stickers.pdf}
477 > %\caption{An empty shell with the bar code stickers identifying the strings.}
478 > %\label{fig:stickers}
479 > %\end{figure}
480 >
481 > The first 7 numbers in a GeoId identify the string to which a device belongs,
482 > while the last
483 > part of this code represents the physical location where the device is placed
484 > in that particular string.
485 >
486 > %\begin{table}[h!]
487 > %\begin{center}
488 > %\begin{tabular}{l|ccc}
489 > %    & 1               & 2     & free value  \\
490 > %    \hline
491 > %  a & TIB             & TID              &             \\
492 > %  b & Forward ($z>0$) & Backward ($z<0$) &             \\
493 > %  c & Up ($y>0$)      & Down ($y<0$)     &             \\
494 > % d &                 &                  & Layer \#    \\
495 > %  e & Inner           & Outer            &             \\
496 > %  f &                 &                  & Manifold \# \\
497 > %  g &                 &                  & String \#   \\
498 > %\end{tabular}
499 > %\caption[smallcaption]
500 > %{A generic $a.b.c.d.e.f.g$ GeoId identifies a string and  must be interpreted according
501 > %to this table. For example of GeoId 1.1.2.4.1.3.2 identifies the second string, of the
502 > %third manifold placed in the inner surface of the Layer 4 Down Forward TIB shell.}
503 > %\label{tab:geoids}
504 > %\end{center}
505 > %\end{table}
506  
507   %The first number identifies TIB (1) against TID (2),
508   %the second number marks the forward part (1) vs. the backward (2). Hence TIB and TID codes become

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