, , , . , , .
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)