jet engine systems
TRANSCRIPT
J85 ENGINEJ85 ENGINE
INTRODUCTIONINTRODUCTION
A General Electric J85-5
Type Turbojet
National origin United States
Manufacturer General Electric
First run 1950s
Variants General Electric CJ610
Developed into General Electric CF700
Specs:
Thrust 2680 lbs
Weight 600 lbs
Compressor 8 Stage Axial
Turbine 2 Stage Axial
ApplicationT-38 Jet Trainer, F-5 Tiger II,A-37 (non-afterburning)
Max RPM 16,550
J85 ENGINE MAIN PARTSJ85 ENGINE MAIN PARTS
FRONT FRAME
1- IGV (inlet guide vanes)2- IGV CRANKS3- 1ST.BEARING4- DOME ASSY
COMPRESSOR CASING
COMPRESSOR ROTOR
1- GEAR BOX2- 2ND.BEARING
MAIN FRAME
SHAFT
COMBUSTION SECTION
1- INNER CASING2- OUTER CASING3- LINERS (12)4- FUEL NOZZLES (12)5- MAIN IGNITER PLUG
TURBINE SECTION
1- TURBINE CASINGS (2)2- TURBINE ROTOR3- TURBINE STATOR
DIFFUSER SECTION
1- DIFFUSER LINER2- EXHAUST CONE3- FLAME HOLDER4- A/B FUEL SPRAY BARS5- A/B IGNITER PLUG
EXHAUST SECTION
1- CASING2- LINER3- VARIABLE EXHAUSTNOZZLE4- ACTUATORS
THANK YOU FORTHANK YOU FORLISTENINGLISTENING
Özkan EYİLİKBİLİRÖzkan EYİLİKBİLİRChief Master Sgt.Chief Master Sgt.Jet Engine InstructorJet Engine Instructor..