Detector Services

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Table of Figures

Figure 1 - Gas system schematic 6

Figure 2 - A half-rack space is used for the gas control implementation. 7

Figure 3 - Gas system half rack ready for installation 8

Figure 4 - Cathode pad half-cylinder. Pairs of cooling pipes are visible 9

Figure 5 - Water cooling system during test. 9

Figure 6 - Model and 3D-printed realization of the dry-air manifold, very similar to the manifolds for the water cooling system. 12

Figure 7 - Overall water cooling system 13

Figure 8 - Temperature Monitor Board 14

Figure 9 - End plate view of the layout of the different electronics boards & HV connections 15

Figure 10 – Unpotted Anode Wire Card and Board with HV distribution 17

Figure 11 - Anode wire pins and Field wire pins under yellow cover 17

Figure 12 – New Anode Wire card with 16 potted HV capacitors, gold crimp pin Mill-max socket to the anode wire 18

Figure 13 - Anode wire pre-amp power distribution & 16 channel temperature boards 19

Figure 14 - Overall Low voltage distribution for anode wires and cathode pads 21

Figure 15 - High Voltage & Grounding scheme for the rTPC 22

Figure 16- Alpha-g rTPC rack organization 23

Introduction

This document is to describe the different services for the rTPC detector. 3 main sections cover the Gas system, the Water cooling system and the Power distribution.

References and related Documents

A dedicated TRIUMF Wiki site gathers all documentations for the rTPC detector system and equipment. Gas system, cooling water system and power distribution can be found there.

Gas system

The gas system as described below includes the entire gas infrastructure required to deliver gas to the detector, monitor and control the gas flow into the detector. It also includes the necessary equipment to notify any change from the nominal gas flow or gas mixture ratio delivered to the detector.

This type of mixed gas system is well understood by the Triumf detector group staff and no issue in its realization is expected.

This system is a stand-alone infrastructure assembled and delivered to CERN. It will be placed in the Alpha-g experimental area floor. The delivery of the different gases to the experimental area is under the responsibility of the Gas handling group from CERN.

The gas delivery system for the radial TPC (rTPC) is to provide Ar/CO2 gas mixture between 90/10 to 50/50 depending on the user requirements. This system does not recycle the gas as the environmental impact of either gas is minimal and the operation cost versus a recycling system would not be economic.

In the event of an additional quenching gas requirement, the overall gas system will have to be reconsidered and possible recycling system envisaged.

A simple gas mixer using digital flow meters will provide the precise mixture dialed by hand in the control system.

During the prototype phase, an ad-hoc gas system will be put in place. A portable gas system is available for such a test.

Specifications

Parameter	Value
Gas mixture	Ar/CO2 (90/10..50/50)
Gas flow requirements	0.3l/min (50%), 0.3l/min (50%)
Detector gas Volume	0.18m3
Flushing time	5h @ 600cc/min
Flow rate	100 to 300 cc/minute

Operation

This gas system is quite simple as it takes 2 or 3 (spare) gas supplies and mixes them in a manifold before delivery to the rTPC detector. Necessary valves for purging lines and by-passing the detector are foreseen. The individual in-flows are controlled by gas dedicated mass flow controllers (MFC-x). The return flow is measured for leak assessment. An additional manometer monitors the internal detector pressure for evaluation of the electron drift characteristics.

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Figure 1 - Gas system schematic

The main flow controller and monitoring is performed by industrial devices from MKS. We added analog flowmeters on each gas line to provide a quick visual inspection of the gas mixing system.

This system will be hooked to the CERN AD-Gas facility. The CERN gas delivers gas through 2 switchable packs of 12 bottles for each gas.

The gas exhaust is evacuated to the exterior of the experimental area with an elevation of about 8m.

Figure 2 - A half-rack space is used for the gas control implementation.

Figure 3 - Gas system half rack ready for installation

Water cooling system

The outer surface of the detector has an arrangement of 8x8 electronics boards handling the readout of the cathode pads. These boards require operating at a controlled temperature to prevent heat build-up at the surface of the detector and improving the reliability of the system. In order to do so, 8 independent water pipe loops running from the bottom-up and down in the longitudinal axis of the detector are in a thermal contact to 8 successive readout boards. From the bottom, a pair of water hoses connect to 2 custom 3D-printed manifolds supplying the water feed and return to the 8 water loops.

These 8 loops are run in parallel to a negative pressure water cooling system. This negative pressure system is to ensure that no water leak will damage the electronics even during possible pipe or delivery hose breakage.

Figure 4 - Cathode pad half-cylinder. Pairs of cooling pipes are visible

Figure 5 - Water cooling system during test.

Specifications

Parameters	Values
Number of parallel water loops	8
Copper pipe OD/ID	¼” / 4.7mm
Length of one loop (on the rTPC)	4.6m
Water speed per loop	…
Pressure drop per loop	…
Power extraction per water loop	8x15W= 120W
Total cooling power	1KW
Inlet water temperature	16..20 degC (to be confirmed)
Outlet water temperature	20..24 degC
Total water flow	3..6 l/minute

Operation

The Pressure PID (proportional/integral/differential controller), PID2, monitors the air pressure in the vacuum vessel. When the pressure rises above a trigger value (perhaps 350mbar) it activates the aspirator vacuum pump to bring the pressure down to maintain a long time averaged pressure (say 300mbar).

This vacuum is then used to draw water through the detector into the vessel, from the Open Tank. The vacuum vessel's water level is monitored by PID1, using a differential pressure transducer measuring the weight of the water column by the difference between the air pressure in the top of the vessel and the water pressure at the bottom of the vessel. PID1 provides a variable signal to the Proportional Solenoid Valve, which varies the flow through the return loop around the (fixed flow) water pump, and thus changing the overall flow of water from the vacuum vessel to keep the water level in the vessel constant despite water being constantly drawn in by the vacuum. The water pulled from the vacuum vessel is pushed through the filter and into the Open Tank, completing the circulation.

Cooling is accomplished in the water pump leg of the system, as coolant pulled from the vacuum vessel passes through a heat exchanger coupled to CERN’s cooling water supply on its way to the pump. The rate that water flows through the system can be determined by many obstacles in the loop, but ideally it should be dominated by the position of the main Throttle Valve. Other valves should generally be set either fully open of fully closed, except for the Proportional Valve, whose position responds to the setting of the Throttle Valve.

Data outputs: there are five data outputs planned. The two process variables, the vacuum vessel absolute pressure, and differential water column pressure, will be sent to the Detector DAQ system. As well, the total flow rate is monitored by the flow meter, whose output is sent to the DAQ system. This data is not used by the circulation system itself. Likewise, the back pressure on the water filter is only sent to the DAQ system to indicate if the filter may need changing, and the temperature of the open tank is monitored and sent to the DAQ system, but currently there is no plan to use it in a temperature control feedback. The temperature of CERN's cooling water supply is not yet known, but we expect we can set the heat exchanger to run at a rate to hold the system temperature near 20°C without feedback control.

For the negative pressure to work effectively to prevent leaks, the water pressure in the detector ought to be down at least to half an atmosphere. With the detector cooling tubes 8x 4.6m of parallel 4.7mm ID copper tubes (2.3m down then 2.3 back-ups), and the supply using (perhaps 6m, 3 to the detector then 3 back) 9.7mm ID (=1/2" OD) poly tubing, the flow will need to be somewhat greater than the required 3 l/min in order to maintain that degree of vacuum in the detector, unless the Throttle Valve is placed upstream of the detector near the Open Tank, or an additional constriction is added in that region.

The water pump leg of the circuit residing in the water cooling/gas rack is placed far enough from the fringe field of the superconducting magnet to prevent disruptive effects on the solenoid valves and electric motors. Therefore the main 1/2" poly line to and from the water pump and its flow loop will add a pressure drop which is estimated at 0.4atm for a 10m line at 6 l/min (9.7mmID), which is within our requirements. As mentioned earlier, the splitting (and reassembly) of the line to the 8 cooling lines close to detector will be accomplished with the use of 2 separate manifolds equipped with temperature sensors for constant in/out global water temperature monitoring.

Figure 6 - Model and 3D-printed realization of the dry-air manifold, very similar to the manifolds for the water cooling system.

Currently, PVC valves with "true union" couplings are planned to be provided around the water pump to permit it to be swapped out from the system for servicing and a valved bypass to the water filter is provided for the same purpose to allow easily changing filter elements with the system running. True union valves are generally only available to 1/2NPT and larger, so an adapter fitting is required. The vacuum pump for the system is a small (2 x 5 x 7.5cm) cascaded dual Venturi aspirator, which is operated with site air, switched with two simultaneously operated normally closed solenoid valves, one for the site air, and one for the vessel vacuum input. If the system is leak free, the vacuum in the vessel should only be degraded by the dissolved air absorbed in the Open Tank and extracted in the vacuum vessel, which from past experience might mean running for under a minute every six hours or so.

The wetted surfaces of this system will be mainly PVC and Polyethylene for the valves, tubing and vessels, plus brass fittings, and the copper cooling tubes, and the surfaces of the heat exchanger, which will most likely be stainless steel. It may be possible to devise an equivalent of a bellows communicating with the Open Tank, so that it is only virtually open, thus sealing the cooling water from contaminants, which may allow us to run with just distilled water plus a strip of silver as a biocide (although I'm not sure if the mix of metals, copper plus stainless, may not interfere with the function of the silver, which is mostly used in computer cooling systems which are copper and plastic only). Otherwise, we will need a biocide and corrosion inhibitor. We have the latter, tolyltriazole, but the biocide is problematic. They tend to be short-lived; for systems which are open to atmosphere, typical industrial practice is chlorination, regularly refreshed, which builds up NaCl as it degrades, making the coolant corrosive. For T2K in Japan, we used the (human-nontoxic) "Germall", which has a two-year lifetime, after which when its effectiveness decays it turns into food, which is the case for any solute that is not actively biocidal. Eventually, any such additives build up and require the coolant to be flushed and replaced. Silver is a lovely method, but only works for extended periods with a sealed system which remains deoxygenated. My research so far has not turned up a good candidate which does not entail recurring changes of the coolant.

Power: the system needs to be able to run on European 220VAC power, but also operate here for testing purposes. The PIDs (Omega CN76160s) will accept both; for the rest of the system, I will have an a universal 90-240VAC input to 24VDC (5A) supply which will drive all the other components, including the pump, which will be a brushless 24VDC centrifugal pump, 1 - 1.5A range. The whole system will run about 125W.

Information on the temperature and flow rate of the CERN cooling water system will be provided later but we don’t anticipate any major issues about the sizing of the heat exchanger.

Figure 7 - Overall water cooling system

Temperature Measurement

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Figure 8 Temperature Monitor Board

The water temperature is read by the Temperature Monitor Board (TEMPB). Thermistors located inside the manifold connect to a 16 bit ADC on the TEMPB which is read out by a Raspberry Pi mounted on board. In a similar manner the air system temperature is read with sensors in the air manifold. The TEMPB can provide temperature readout of 32 thermistors which connect to terminal blocks. The channels can also be readout differentially providing up to 16 channels for thermocouples. An on board thermistor allows for cold junction compensation. The board is powered via USB on the Raspberry Pi.

Power distribution

This section covers the different voltages and power requirements for the operation of the rTPC. This includes:

1. High Voltage for the rTPC electron drift and amplification operation
2. Low Voltage to the Anode wire frontend electronics
3. Low Voltage to the Barrel Scintillator frontend electronics
4. Low Voltage to the Cathode Pads electronics
5. Grounding scheme of the overall rTPC

The provision of power to the different components of the detector is distributed from the top end plate of the rTPC.

Figure 9 - End plate view of the layout of the different electronics boards & HV connections

High Voltage for the rTPC

Three main components of the rTPC require High Voltage

• Main cathode wall (Negative ~5KV)
• Field wires (Negative ~ few hundred volts)
• Anode wires (Positive ~3.2KV )

These voltages are provided by a Quad High Voltage unit from CAEN. Three independent cables will be fed to the top of the rTPC.

High Voltage provision to the bottom endplate HV ring is taken from the central cathode near the bottom endplate.

The Field wire voltage is connected to all the field wire crimp-pins through a dedicated socket chain inserted on each of the crimp-pin on the top and bottom endplates. The field wires themselves interconnect the high voltage between the top and bottom pins.

The High Voltage for the anode wires is delivered to the Anode Wire Card (AWC) which will distribute it to its 16 wires, Figure 11. There are 16 AWC cards covering each end of the anode wires. All the top and bottom 32 AWC are connected serially. The anode wires themselves interconnect the high voltage between the top and bottom pins.

The anode wires pre-amplifiers boards (AWB) are sitting on the top of the Anode Wire Card (AWC) Figure 10. As the wire is powered by the HV, each anode wire has a high Voltage decoupling capacitor to isolate the pre-amp stage from the HV. This circuit resides on the AWC. The AWB will see the AC coupled anode signal only. With a new design of the AWC Figure 12, the decoupling capacitors are potted in epoxy to ensure proper isolation of the HV toward the surrounding circuit as well to prevent corona discharge due to relative humidity of the surrounding.

Figure 10 – Unpotted Anode Wire Card and Board with HV distribution

Figure 11 - Anode wire pins and Field wire pins under yellow cover

Figure 12 – New Anode Wire card with 16 potted HV capacitors, gold crimp pin Mill-max socket to the anode wire

Power distribution to the Anode wire frontend electronics

The AWB pre-amp board requires 2 voltages (+5V, -5V) which are fed through dedicated cable connections to each of the AWB. There are 16 AWB per end of the rTPC, therefore, 16 individual cable bundle will be reaching the top and another 16 the bottom of the rTPC. The cable bundle is to also provide the power return lines to the Power Supply.

The PL508 Low Voltage power Supply from Wiener will provide the main power source for all the 32 pre-amplifiers. A dedicated connection breakout board with current monitoring capability splits the source power to the 2 x 16 necessary connections to the Anode wire boards. Based on a RaspeberryPi card, a 16 power distribution board is already implemented for the prototype. This board has extra 4 channels of temperature monitoring which can be used later on. In the same process we produce a similar board for 16 channel of NTC, RTC temperature monitoring. They will be used for overall detector and cooling system monitoring.

Component	+5V Supply	-5V Supply
Anode Pre-amp	1.5W (0.3A)	1.5W (0.3A)

Figure 13 - Anode wire pre-amp power distribution & 16 channel temperature boards

Power distribution to the Barrel Scintillator frontend electronics

Similar to the Anode wire pre-amplifier voltage distribution scheme, the Barrel Scintillators will require several low voltages for power and control. The Barrel Scintillator Boards (BSB) are mounted on both ends of the Scintillator bar with the same segmentation as the Anode wires i.e.: 16 BSB per end. The design of the electronic chain for the barrel scintillator is not fully designed yet.

The SiPM sensors require a bias voltage of the order of 28V. This voltage will be provided through the same mean as the low voltage power. Expected threshold voltage for the local signal level discriminator is also foreseen.

Low Voltage to the Cathode Pads electronics

The cathode pads electronics mounted on the external cylinder surface is composed of the analog frontend and the digital conversion electronics. Two voltages are required (+5.3V, +2.3V). The delivery is done through dedicated “power bar” running the full length of the rTPC. A set of 3 bars covers the 8 axial cathode pad electronics boards. 8 of them cover the circumference of the rTPC.

Component	+5.3V Supply	+2.3V Supply
Padwing board	10W (1.8A)	2W (0.8A)

Overall the low power supplies are provided by a PL508-3U with 8 modules of either single or dual channels from Wiener.

Figure 14 - Overall Low voltage distribution for anode wires and cathode pads

Grounding scheme of the overall rTPC

The grounding scheme challenge in this setup is the far distance between the 2 end of the rTPC (2.3m) and the lack of accessibility to the bottom of the detector. The proposal is to use a Copper sheet mounted on the inner surface of the inner cylinder. This ground path will connect the 2 endplates to the High Voltage return. All the pre-amps will merge their ground to this central ground.

Additional ground lugs have been included in the Anode wire pre-amplifier boards to strengthen the ground as each anode wire is readout out from both end. This may be used once the full detector is assembled to address possible ground loop issues.

Safety and Hazard considerations

Gas

The Ar and CO2 do not require special health safety system. The detector will be operated in the ventilated hall of the AD building at CERN.

Gas flow, detector gas pressure, and gas inlet temperature are constantly monitored and can trigger adequate response for shutdown or closure of the gas system for safety purpose.

Cooling water

The water cooling system operates in negative pressure mode preventing any water leak to flood the detector outer surface. In addition water flow and inlet/outlet temperature are constantly monitored to allow fast response to off range parameter in order to shut down the electronics. The cooling water system requires a primary cooling tap water loop from the AD building. Water quality, water flow and water temperature are not under our responsibility. This aspect will be dealt during the initial phase of the rTPC commissioning at CERN.

Power distribution

All electronics voltages are below 48V. No special safety circuits are envisaged.

The high-voltage circuit is fully protected outside the detector. The access to the high-voltage on the detector is restricted to the two end-plates. Interlock scheme will be put in place to ensure the shutdown of the HV in case of manual access to the detector itself.

The LV (Low Voltage) power units are also interlocked to prevent false powering sequence which can damage the downstream electronics modules.

Figure 16- Alpha-g rTPC rack organization