收藏切换
Effective Power and Power Recovery of Aviation Piston Engine
收藏切换
PDF
Zhan-yong WEN, Ya-ming TIAN, Peng-hui SUN, Wei-dong ZHAO
Science Technology and Engineering | 2025, 25(16) : 6760 - 6765
Less
收藏切换
Science Technology and Engineering | 2025, 25(16): 6760-6765
Papers·Energy and Power Engineering
Effective Power and Power Recovery of Aviation Piston Engine
Full
Zhan-yong WEN, Ya-ming TIAN, Peng-hui SUN, Wei-dong ZHAO
Affiliations
  • CH UAV Science & Technology Co. , Ltd. , China Academy of Aerospace Aerodynamics, Beijing 100074, China
Published: 2025-06-08 doi: 10.12404/j.issn.1671-1815.2404769
Outline
收藏切换

A calculation method of effective power based on heat transfer mathematical simulation of intercooling system was proposed for an aviation piston engine, and the heat transfer simulation model of the intercooling system was developed with VB language. The validity of the simulation model was verified by the test data. The results show that the errors between the simulation values and the test values of the intercooler cold side outlet temperature and the hot side outlet temperature are within 1.5%. Using the simulation model, the influence of fan air flow on the effective power of the aviation piston engine was studied, and the air effective power recovery was studied. The results show that with the increase of fan air volume, the amplification of fan power increases, while the amplification of engine power decreases. Under the combined effect of the two, the effective power of the engine first increases and then decreases with the increase of fan air volume. For the aviation piston engine studied, when the fan air volume is 1 400 m3/h, the effective power of the engine reaches the maximum, which is 101.6 kW. When the flight altitude is below 2 000 m, the engine effective power recovery coefficient increases slightly with the increase of flight altitude, and when the flight altitude is above 2 000 m, the engine effective power decreases significantly with the increase of flight altitude. Under the condition of 50 ℃ at sea level, the effective power recovery coefficient of the engine at 7 000 m is only 92.2%.

aviation piston engine  /  intercooling system  /  electric fan  /  surge tank temperature  /  effective power
Zhan-yong WEN, Ya-ming TIAN, Peng-hui SUN, Wei-dong ZHAO. Effective Power and Power Recovery of Aviation Piston Engine[J]. Science Technology and Engineering, 2025 , 25 (16) : 6760 -6765 . DOI: 10.12404/j.issn.1671-1815.2404769
Year 2025 volume 25 Issue 16
PDF
414
171
Cite this Article
BibTeX
Article Info
doi: 10.12404/j.issn.1671-1815.2404769
  • Receive Date:2024-06-25
  • Online Date:2025-07-09
  • Published:2025-06-08
Article Data
Affiliations
History
  • Received:2024-06-25
  • Revised:2025-03-07
Funding
Affiliations
    CH UAV Science & Technology Co. , Ltd. , China Academy of Aerospace Aerodynamics, Beijing 100074, China
References
Share
https://castjournals.cast.org.cn/joweb/kxjsygc/EN/10.12404/j.issn.1671-1815.2404769
Share to
QR

Scan QR to access full text

Cite this article
BibTeX
Citations
表12种不同金属材料的力学参数

Family
属数
Number of
genus
种数
Number of
species
占总种数比例
Percentage of
total species (%)

Genus
种数
Number of
species
占总种数比例
Percentage of total
species (%)
鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
关闭全屏
  • BibTeX
  • EndNote
  • RefWorks
  • TxT