Abstract
This paper aims to obtain the thermodynamic characteristics of the air system control device sealing part in different compressor bleed air and ambient temperature. On the basis of considering the main factors affecting the heat exchange process and simplifying the physical model of the air system control device, the thermodynamic model of air system control device is established based on the basic theory of laminar flow heat transfer and heat conduction theory. Then the piston motion characteristics and the thermodynamic characteristics of the air system control device seal are simulated. The simulation results show that the valve actuation dynamic time of piston is about 0.13 s in the actual working conditions, and the temperature effect on the dynamic response of the piston rod is only 5 ms when the inlet air temperature at 300℃ and 370℃. The maximum temperature of the air system control device sealing part is not more than 290℃ under long time working condition of compressor air entraining. The highest temperature of the sealing part can reach up to 340℃ when the air flow temperature reaches the limit temperature of 370℃, and the longest duration working temperature limit is not more than 14 s. Therefore, the selection of control device sealing material should consider the work characteristic of instantaneous temperature limit.
| Original language | English |
|---|---|
| Pages (from-to) | 517-526 |
| Number of pages | 10 |
| Journal | Transactions of Nanjing University of Aeronautics and Astronautics |
| Volume | 36 |
| Issue number | 3 |
| DOIs | |
| State | Published - 1 Jun 2019 |
Keywords
- Aeroengine
- Air bleed control device
- Air system
- Thermodynamic analysis