|
Engine
Research Building (ERB):
Turbine Facilities - SE-17
Wave Rotor Experiment Test Facility
SE-17
Facility Description
The SE-17 Wave Rotor Experiment Test Facility combines the functions
of a compressor and turbine in one unit. Instead of using blades
to add or remove energy from the flow, it uses compression and expansion
waves, traveling in passages on the rotor. It is intended to be
used as a "turbocharger" for gas turbine engines, boosting
the compression ratio. Air from the engine compressor would enter
the wave rotor, and be compressed by waves to about three times
its original pressure. Exiting the wave rotor, it would then pass
to a combustor, and be heated. Returning to the wave rotor, it would
lose pressure in expansion waves, providing the energy required
to compress the incoming air in the process. The advantage of a
wave rotor is that the rotor "sees" both cold and hot
gases, and reaches a temperature somewhat between the two, whereas
in a gas turbine engine the turbine "sees" the hot gas
from the combustor directly, and attains a temperature close to
that of the gas leaving the combustor. In a conventional combustor,
the gas leaving the combustor is a lower pressure than the entering
air. The gas leaving the wave rotor is at higher pressure that the
entering air. As a result, calculations have shown that the engine
incorporating the wave rotor may have a specific power up to 19%
higher than the base engine, with specific fuel consumption about
15% lower.
SE-17
Special Features
The performance of thermal engines usually depends on temperature
ratios rather than absolute values. Operating at reduced inlet temperatures
allows reasonable high temperatures for a given temperature ratio.
This is true for the wave rotor, and SE-17 is equipped with a chilled
air supply at -60°F. Heating of the compressed air is performed
by a 350 kW electric heater. The exhaust gases are sent to the altitude
exhaust system. Most of the data are pressure readings, which are
processed by an electronic scanning system, and stored in Escort.
Temperatures are read by thermocouples, with the readings also stored
in Escort.
SE-17
Facility Capabilities |
| Parameter |
Operating
value |
| Inlet
air pressure |
40
psig/10 psig |
| Inlet
air temperature |
-40
to 200 °F |
| Inlet
airflow |
2
lb/s |
| Altitude
exhaust |
26
in. hg |
| Rotor
speed |
2000-12000
r/min |
| Heater |
330kW
1200 °F |
| SE-17 System Instrumentation |
| System |
Number and Type |
| ESP |
320 Ports of +/- 45 PSID
Barometric Ref |
| Escort |
192 Channels
132 Available to the Customer |
| Thermocouples |
94 Type K
2 Type T |
|