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, , , . , , .

q-1/T , , : .

, . , , , . , , ... 30%. 5-10 ... 40%. ... , , 30% 40%.

.. [1], , , : 50 , 3 , 300 , 8 , 6,3 / (1,5 /).

... 30% 6,4%, 31,1 / . ... 40% 7,6%, 43,6 / . , , , , 2,7%.

183 . 127 .

100 / 30% 5,4 , 40% - 6,0 .

.. [1] 13-16%.

, , , .

: , ... , 30%, , ... 40%. ... , , 9% 16%. , .. [1].

, , , , . , .

. ... 9%, 12,1%, ... 16%, 13,4%. , 2,7%, 350% 390%, .

... 9% 16% , , 250 241 .

, .

, , ... , ... , .

, ?

, ... 30% 6,4%.

, , , , , , , . (), .

, . , , , , . [4,5]. , , .

4 , , . , . , , .

 
 

, . , , - , . , , , . , , 60.000 30 [5].

, , , . , , , .

, , - , . , . , , , , .

, , . , , .

.

. , , [6]. 20%. , , , [7].

. , , .

. , , , .

, .

.

q-1/T , 5

 
 

, , ... 16%. , , 4, , 1. ... .

q-1/T , . (195 ) , . , . , , , . , , .

q-1/T , , , .

 
 

Q-1/T , . , 5 .

, , , . , . .

, . 6 T-S . 1,2,4,5,6,7,9,1 9,8,6,5,4,3,9. 6 9,8,6,5,4,3,9, , .

, , , , . , , . , , 3,4,5,6,7,9 , . , D, 3,4,5,6,7,9 (1 D).

6 8,6,7. 8-6, 6-7, 7-8. , . , , . , . 8,6,7 .

, .. . , 30- , .

.

, , , .

, ... 30%, 183 , , 2,7% 6,4%. 16,9%.

... 16% , 390%.

, , , .

.

 

1. . ( ) . . , 1966 . . 52.

2. .. , .. . . // , 1, 2011 .

3. ... (q-1/T) . // , 2, 2004 .

4. Ja. Wurm, J. A.Kinast, T.R.Roose, W.R.Staats. Stirling and Vuilleumier Heat Pump. New York. McGraw-Hill, Inc. 1990. 252 p.

5. Jeffrey G. Schreiber. Developmental Considerations on the Free-Piston Stirling Power Convertor for Use in Space.// American Institute of Aeronautics and Astronautics, AIAA20064015.

6. Scott Backhaus, Greg Swift. New varieties of thermoacoustic engines// Los Alamos National LaboratoryLA-UR-02-2721, 9th International Congress on Sound and Vibration, July 2002,

7. Chen Guobang, Tang Ke & Jin Tao. Advances in thermoacoustic engine and its application to pulse tube refrigeration//Chinese Science Bulletin 2004 Vol. 49 No. 13 1319 p.1328 (Cryogenics Laboratory, Zhejiang University, Hangzhou 310027, China)

 

 





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