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Estimation of the critical temperature ratio

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1 Estimation of the critical temperature ratio
for thermoacoustic engines based on adaptive control which maintains closed-loop system at stability limit Kazuaki Sakurai, Yasuhide Kobayashi and Noboru Yamada Nagaoka University of Technology (Japan)

2 Background TC TH Stack (Regenerator) Resonator Sound wave Thermoacoustic engines utilizing the thermoacoustic phenomena increase the efficiency on heat recovery It is important to know the critical temperature ratio (CTR) in thermoacoustic systems It is difficult to know it at the design stage when heat exchangers and stacks have complex structures

3 Power consumption of loudspeaker becomes minimum at CTR
Background In order to estimate CTR, we have proposed an experimental method The tube pressure amplitude is maintained to be a constant value by an open-loop control The open-loop control has a manual tuning of driving signal for loudspeaker Power consumption of loudspeaker becomes minimum at CTR

4 Background In order to estimate CTR, we have proposed an experimental method To carry out the open-loop control, it is necessary to previously measure the frequency responses at various temperature ratios The resonance frequency is calculated in order to set the driving frequency Labor saving of the measurement is desired

5 It will be shown that a relationship between the
Objective Propose an adaptive control system Increases the tube pressure amplitude till a reference value by destabilizing the closed-loop system in order to hold the critical point By using this method, there is no need to carry out the frequency responses, since the resonance frequencies are automatically determined by proposed control system It will be shown that a relationship between the adaptive gain and temperature ratio can be used an alternative method to estimate the CTR

6 Experimental apparatus
Standing-wave thermoacoustic engine D/A A/D PC PA loudspeaker TH TC Wspk sensor1 sensor2 core 1312 mm 565 164 502 p2 p1 u vi vs 360 ・ A loudspeaker and two pressure sensors are located ・ The thermoacoustic core is composed of a stack and two heat exchangers ・ The cold-side heat exchanger’s temperature TC is kept at room temperature

7 Experimental apparatus
Standing-wave thermoacoustic engine D/A A/D PC PA loudspeaker TH TC Wspk sensor1 sensor2 core 1312 mm 565 164 502 p2 p1 u vi vs 360 A preliminary experiment has been carried out to obtain a rough estimation of CTR It has been found that the CTR of the engine is approximately 1.3

8 Experiment method The driving signal of the loudspeaker (τ =11.5 ms )
The objective of the control system is to drive the loudspeaker with as small amplitude as possible in driving signal so that the amplitude of p2 matches to the reference value ・The reference value of p2 is set to 200 Pa. ・The heater temperature is adjusted so that TH / TC  varies from 1.00 to 1.35, 8 points with increment 0.05 The driving signal of the loudspeaker (τ =11.5 ms ) This is known as a phase-delay controller which has been conventionally used to suppress the thermoacoustic instabilities

9 ^ ^ ^ Experiment method |・| Block diagram of the control system
u e-sτ G(t) LPF PI π/2 |・| P2* - P2 ・The absolute value signal of p2 goes through to a low-pass filter and estimated pressure amplitude P2 is obtained ・The difference between P2 and the reference value P2*are sent to the PI controller G(t) ・The output of PI controller itself is used as the feedback gain G(t) At each setting of TH / TC, the steady-state feedback gain G is measured

10 ^ Result Time response G ex. TH / TC= 1.0 p2
As shown in blue line, the absolute value of the gain is increased so as to oscillate the engine p2 G Time(s) Pressure (Pa) Pressure (Pa),Gain It is automatically adjusted to achieve a constant pressure amplitude at the reference value

11 Result Time response ex. TH /TC= 1.0
Enlarged view of the time response of p2 in steady state It is observed that the pressure amplitude converges to 400 Pa which implies the steady-state oscillation 400 Pa Pressure (Pa) Time(s)

12 Result Feedback gain G Linear relationship is observed
【TH / TC < 1.3】 ・ Adjusted gain shows negative value ・ Loudspeaker acts to assist the sound wave generation 【TH / TC = 1.3】 ・ Gain is almost zero 【TH / TC = 1.35】 ・ Positive gain is observed ・ Loudspeaker acts to suppress the sound wave If we assume the linear relationship, it is possible to predict the CTR by performing measurement of gains for several points in the region below the CTR

13 Result Oscillation frequency
The oscillation frequency has been adjusted automatically It is confirmed that the oscillation frequency by adaptive control has the same tendency with frequency response experiment The frequency response experiment as in the conventional method can be omitted with this proposed method

14 Conclusion ・We proposed an adaptive control system which maintains
the tube pressure amplitude to be a reference value. The open-loop gain is automatically adjusted by destabilizing the system around the critical point. ・The results show that the pressure amplitude is successfully converged to the reference one. This implies the closed-loop stability of the proposed adaptive control system. ・The steady-state frequencies for various temperature ratios are automatically obtained in similar values by manual control. ・A linear relation between the adaptive gain and temperature ratio is also obtained, which provides an alternative method to estimate the CTR. 

15 Future work ・ Theoretical guarantee for the closed-loop
stability of the proposed adaptive   control system ・ Automatic adjustment of time delay in controller

16


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