1. Introduction
HPGe detectors are the laboratory standard for high-resolution gamma-ray spectroscopy and are used extensively in a wide range of application areas, such as environmental monitoring, medicine, geology and scientific research [
1]. In order to reduce the leakage of current-induced noise from thermal generation of charge carriers, HPGe detectors need to operate at a temperature range of 90~120 K. To achieve these temperatures, liquid nitrogen (LN2), a cryogen, was commonly used with a cryostat. However, cryogen use is confronted with several health risks and operational problems [
2]. Electromechanical cooling is an attractive choice, especially for portable HPGe detectors. Advances in Joule–Thomson technology coupled with HPGe detectors have been reported [
3]. Electromechanical cooling systems (cryocooler) have become common for HPGe detectors.
HPGe detector resolution is a measure of the width, specifically the full width at half maximum (FWHM), of a single energy peak, expressed in absolute keV. Better (lower FWHM value) resolution enables the system to more clearly separate the peaks within a spectrum. Mechanically cooled HPGe detector resolution performance is typically specified as degradation by some percentage compared to LN2 performance.
The cryocooler essentially needs pressure oscillation to generate low temperatures. Gas pressure oscillation intrinsically causes vibrations at the cold stage of the cryocooler. Mechanical vibrations inherent in EMC cause electrical noise induced at the preamplifier input and periodic changes of structural capacitances between the HPGe detector and components. The vibration alters the capacitances in input circuits of the preamplifier, causing electrical interference, and causing the detector performance to degrade.
Many technologies have been developed to reduce the micro-vibration induced by coolers [
4,
5,
6,
7,
8]. Riabzev et al. [
5] developed the ultra-low vibration cryogenic cooler by utilizing a combination of passive and active suppression techniques. The effectiveness of the techniques is mainly reflected in the axial direction of the cooler. Riabzev et al. [
6] proposed a multidimensional, triple-stage, passive vibration isolator on the cold tip of a small cryogenic cooler. The isolator is used to attenuate cold-tip vibration; however, vibration induced by the compressor inevitably passes to the cold tip when the compressor and cold finger are fixed in the same platform. Kwon et al. [
7] proposed an SMA blade isolator that ensures desirable vibration isolation performance, except in the gravitational axis, regardless of 1G and 0G conditions. The isolator has high stiffness in order to support the cooler in the gravitational axis. Thus, the isolator cannot isolate vibration in the gravitational axis. Kwon et al. [
8] proposed a multilayered blade isolator with double-sided adhesive tape, and this isolator can provide a constant vibration isolation capability irrespective of gravitational effects. Although the applicability and survivability of double-sided adhesive tapes were evaluated through qualification-level TV tests, the long-term stability and reliability of double-sided adhesive tape is unconvincing. Oh H U et al. [
4] proposed a passive isolation system named PLOVIS, and PLOVIS is used to isolate vibration from the cooler. However, the isolator requires an additional 1G compensation device to obtain an ideal micro-vibration isolation capability on the ground.
In this paper, a portable PTC, suitable for HPGe detectors, was developed. A split PTC was used to maintain the cryogenic temperature. The split PTC consisted of a linear compressor and cold head. Degradation of detector performance was suppressed in two ways. A portable pulse tube cryocooler (PTC) was expected to function as a low-vibration cryocooler. Due to the absence of moving components in the cold head, the split PTC could provide a cryogenic temperature with low vibration. Compressors are well-known sources of harmonic disturbance. In order to attenuate the vibration exported, a linear dual-piston compressor comprised a pair of back-to-back in-line pistons resonantly driven by linear “moving coil” motors, arranged to oppositely slide inside tightly matched cylinder liners. A flexible gas transfer line (a thin-walled copper tube of a small diameter) was installed to connect the linear compressor and cold head. The flexible gas transfer line isolated the detector vibration interference. Although producing quite acceptable vibration export for most applications, this vibration export was excessive for the HPGe detector. In order to attenuate cooler vibration further, a compressor vibration isolation kit (CVIK) and heat links [
9,
10,
11,
12] were implemented.
On account of the advantages of the simplicity and reliability of passive-type isolators, they have generally been employed to achieve the desired isolation performance. To attenuate the micro-vibration of the compressor, a compressor vibration isolation kit (CVIK) with eight sets of spring and damper isolators was implemented. Eight sets of damping spring dampers were divided into two groups and distributed evenly around the compressor. The right section of
Figure 1 shows a structural diagram. The compressor with the CVIK had the same isolation performance in any direction.
This paper evaluates the effectiveness of the CVIK and heat links. A micro-vibration test and HPGe energy resolution tests were performed. The results indicate that the passive isolation method can meet HPGe detector requirements.
2. Passive Isolation System Design
In this paper, the specifications for the low-vibration portable EMC system are displayed in
Table 1. A schematic illustration of the portable passive isolation PTC system is shown in
Figure 1. The compressor assembly was mainly composed of a compressor, spring isolators, housing for the compressor, and an “S” shape transfer line. The transfer line connected the cold flange with the compressor. The spring isolators attenuated base plate and cold head flange vibration. To attenuate detector interface (VR stage) vibration, copper heat links were used to connect the cold tip with detector interface. An FPR-supporting plate [
13] was mounted on a vacuum vessel flange to support the HPGe detector.
To reduce PTC mounting base plate vibration, a CVIK was installed between the compressor and the PTC-mounted interface. In order to ensure cooler multi-orientation operation, the CVIK included eight sets of spring and damper isolators to reduce the transmission of vibration from the compressor. The transmission of the vibration force η is defined as the ratio between the force at the mounted interface and the force exported by the compressor. For a linear single-degree-of-freedom spring and damper system, η is expressed as Equation (1).
Figure 2 demonstrates the physical model.
where ε is a damping ratio, λ is the ratio of vibrational frequency and natural frequency of the spring,
is the amplitude of vibration force after the vibration isolators,
is the amplitude of vibration force from the vibration source,
is vibration force amplitude,
is the isolation system vibration defection, and k is the axis stiffness of the CVIK.
In order to ensure
η ≤ 0.1, the CVIK design parameters are shown in
Table 2. The natural frequency of a compressor with the CVIK is less than 12.7 Hz. The axis stiffness of the CVIK is 16,000 N/m. The transfer line deflection is within 3.52 mm under the 2 g sine vibration load.
Figure 3 shows the transmissibility of the CVIK at different vibrational frequencies. The figure indicates that the transmissibility is 0.07 at the main frequency 64 Hz and that the CVIK has lower transmissibility at harmonic frequency. The requirement of the CVIK is not only to reduce vibration transmissibility but also to weaken the vibration displacement under the 2 g sine vibration load. According to function 2, the displacement of the compressor is 3.52 mm (which the copper transfer line tube can bear) when the PTC suffers from 2 g acceleration impact.
In this paper, the ultimate requirement was to reduce the vibration of the HPGe detector mounted interface. Especially, HPGe detectors need to extend cold tips because detectors require lead chamber shielding in use. The longer the copper cold tip, the greater the vibration of the detector interface.
The CVIK ensured the attenuation of the vibration of the compressor-mounted interface and the cold head flange. In order to further mitigate detector vibration, oxygen-free high-conductivity copper heat links and a glass fiber-reinforced-plastic supporting plate were used. The heat links consisted of several copper wires, each 0.5mm in diameter, which reduced the heat links’ spring constant. The detector interface was thermally connected to the cold tip by the heat links, and the HPGe detector was mounted on a vibration reduction stage. An FPR plate was used to support the detector. One end of the FPR plate was mounted on a vacuum vessel flange, and the other end supported the detector. Thus, detector vibration was obtained from the cold head flange and heat links. Additionally, we bent the transfer line into an “S” shape, which may have reduced the transfer line stiffness to decrease the compressor vibration transmissibility to the cold head flange. The advantage of the heat links was verified experimentally.
3. Evaluation Performance of the PTC Vibration Isolation System
The PTC vibration isolation system was evaluated both on the PTC and the HPGe detector. A three-dimensional dynamometer force sensor (Kistler 9257B) was used to measure compressor vibration [
14]. A PCB three-dimensional piezoelectric accelerometer (PCB 356B18) was installed to measure detector interface vibration acceleration. Meanwhile, detrimental effects of the PTC from mechanical vibration on spectrometric performance and detector signal noise were tested.
In order to evaluate CVIK performance, an isolation performance test on a Kistler 9257B table was executed.
Figure 4 shows the compressor isolation performance test configuration on the Kistler 9257B. The compressor with CVIK was mounted on the Kistler 9257B, and a cooler finger was rigidly fixed on other base plate on a sponge mat. The “S” shape copper transfer line may have affected the transmissibility of the cooler finger. The compressor vibration level was tested under the rigid connection and vibration isolation connection of the compressor. To provide a lightweight PTC system for the HPGe detector, the compressor and cold finger inevitably needed to be fixed to the same base plate. Thus, the vibration performance of the compressor with CVIK and cooler finger mounted in the same plate needed to be evaluated.
Figure 5 illustrates the vibration transmissibility of the CVIK. The compressor was driven by 64 Hz, 50 W AC. The percentages in the figure indicate the ratio of compressor vibration force with and without the CVIK. The vibration peak value of the rigid condition was less than 1 N, and the peak value of the isolation condition was less than 0.1 N. The figure indicates the vibration level without the CVIK was higher in harmonic frequency because the higher frequency modes were excited. CVIK transmissibility was less than 10% in higher-frequency modes. The main frequency vibration transmissibility was higher than theoretical calculation for some reason, such as the transfer line stiffness affecting CVIK nature frequency and gas reservoir vibration. However, the main frequency vibration force was smaller, which met the requirement of less than 0.2 N.
Figure 6 shows the isolation performance of the PTC when the compressor and cold finger were mounted on the same plate. The figure indicates that the vibration force of the PTC without an isolation system was up to 4 N, and the isolation performance was basically the same as the compressor.
Table 3 shows the experimental results for the root mean square value (Nrms) of the vibration force of the compressor, PTC, and cold finger with and without the CVIK obtained from the time domain profiles. Vibration RMS of the compressor with CVIK was less than 0.15 Nrms, and the transmissibility was less than 6%. The cooler vibration force RMS was unamplified after compressor vibration isolation. The RMS of the PTC with CVIK was less than 0.15 Nrms, and the transmissibility was less than 6%, which met the HPGe requirement of less than 0.2 Nrms.
In this section, we focus on the evaluation of detector mounting interface vibration attenuation by introducing heat sinks. Detector mounting interface vibration came from heat links and the FPR-supporting plate. Since the cold tip and detector mounting interface were hard to mount on the Kistler 9257B, a PCB three-dimensional piezoelectric accelerometer was chosen for evaluation of heat link vibration isolation performance.
Figure 7 shows an assembly drawing of the heat links and accelerometer mounting positions. Two measurement cases were performed under the CVIK: for case 1, the base plate, cold head flange and cold tip vibration acceleration were tested; for case 2, the accelerometer was moved to the detector mounting interface from the cold tip and the other two accelerometers stayed the same. The ratio of vibration acceleration of the detector mounting interface to vibration acceleration of the cold tip was used to evaluate the vibration isolation performance of the heat links. Base plate and cold head flange acceleration were used to monitor case 1 and case 2 in consistent test conditions.
Figure 8 shows the vibration isolation performance of heat links; the percentages were the ratio of detector mounting interface vibration to cold tip vibration. Vibration acceleration peak values of the detector mounting interface were less than 5 mg in main frequency and harmonic frequency. Heat links effectively attenuate the vibration in higher frequency modes.
Table 4 shows the different position and different measurement case time profile RMS test results. The detector interface vibration came from the heat links and the FPR-supporting plate.
Table 3 indicates that the detector vibration level was similar to the cold head flange. Thus, the transmissibility of the cold tip was very low, which indicates that heat links were effective in reducing the vibration transmission of the cold tip. The ratios of detector mounting interface to cold tip a
rms (root mean square of acceleration) were 26.8%, 15.6%, and74% in the x, y, and z axes. The detector vibration interface a
rms was less than 10 mg
rms, which met HPGe detector requirements.
To estimate the effect of mechanical vibrations from the PTC on detector energy resolution, the detector resolution and the detector signal spectrum characteristic were compared under the PTC switched on or off [
15]. The thermal inertia of the detector was large enough to allow tests to be taken over a period of 10 min, with little change in detector temperature.
Figure 9 illustrates that the detector signal noise was the same range from 0 Hz to 2000 Hz with the PT cooler switched on and switched off.
Figure 9 indicates that the vibration of the PTC basically provided no microphone noise for the detector signal. Thus, in this paper, the vibration isolation system of the PTC met the requirement of the HPGe detectors.
Figure 10 shows that detector FWHM energy resolutions of 1.31 keV and 1.98 keV were achieved at 122 keV and 1332 keV, respectively, with the cooler switched on.
Figure 11 indicates the resolution improved to 1.0 keV and 1.84 keV at 122 keV and 1332 keV, respectively, under the PTC switched off.
Table 5 summarizes the detector energy resolution under LN2, PT cooler on and PT cooler off conditions. Under the LN2 and PT cooler off conditions, the detector energy resolution was basically equal. The energy resolution degraded 2.5% and 8.3% at 1332 keV and 122 keV, respectively. Microphone noise and electromagnetic interference were introduced simultaneously when the cooler was on. Electromagnetic interference was the main reason for degrading detector energy resolution when the vibration isolation system and heat links were introduced to the PTC in this paper.