BSI Engineering’s aviation projects include creating two combustor test cells for gas turbine engines. This one is rated to 120 lb/s of 1500°F at 1000 psia.
Combustor Test Cell 2
- Design of new facility to test gas turbine combustors (single cup, sector, and full annular rigs)
- 120 lb/s of 1500°F at 1000 psia combustion air
- Spool and isometric drawings for combustion air pipe
- Pipe support details
- Support steel design
- Both natural gas heaters and electric heaters in the combustion air lines
- Booster compressors
Contact Us for Aviation or Turbine Engine Projects
Look at our other aviation project here.
BSI Engineering brings decades of expertise and experience to the aviation and turbine engine industries. Contact our team or call our Cincinnati headquarters at (513) 201-3100 for more information.Contact Us