Our stock is changing, please contact us directly for specific inventory and pricing. Runners and Museum cutaways/display pieces, large and small.
Teledyne CAE J402
We have Teledyne CAE J402 Engines in Stock
Specifications (J402-CA-400)
General characteristics
- Type: Turbojet
- Length: 29 in (74 cm)
- Diameter: 12.5 in (32 cm)
- Dry weight: 101.5 lb (46 kg)
Components
- Compressor: Single stage axial compressor single stage centrifugal compressor
- Combustors: Annular
- Turbine: Single stage high pressure turbine
Performance
- Maximum thrust: 660 lbf (2.9 kN)
- Overall pressure ratio: 5.6:1
- Fuel consumption: 1.2 lb/lbf-hr
- Thrust-to-Weight Ratio=: 6.5:1
Boeing T50
Boeing T50 Turbine Engines in Stock
MANUFACTURER: Boeing
DESIGNATION (Military): T50-BO-12.
ENGINE TYPE: Turboshaft. Dual-Shaft.
COMPRESSOR TYPE: Two-stage (axial and centrifugal), single-entry compressor.
TURBINE TYPE: Single stage, axial-flow turbine.
COMBUSTOR TYPE:Two reverse-flow combustion chambers.
POWER (take-off) RATING: 365 shp at 59°F.
BASIC DRY WEIGHT: 267 lbs.
APPLICATION: Navy Model QH-50D Drone.
JFS-100
JFS-100 Engines for Sale.
Allied Signa Garret l JFS 100
Model JFS 100-13 Gas Turbine Engine
Model and type
JFS 100-13. Turboshaft, ( free turbine), The gas generator incorporates a 1-stage centrifugal compressor, annular combustor,1-stage axial flow turbine. The power turbine incorporates an axial flow turbine wheel assembly, a planetary reduction gear system an over running clutch system.
Compressor
Air inlet in front of unit. Single stage radial outflow, Single-entry impeller mounted on main shaft supported in 2 ball bearings. air mass flow 1.6 Ib/sec/72,500 rpm.
Combustor
Annular fuel manifold assembly, and five simplex fuel nozzles.
Turbine (Gas generator)
Hollow nozzle vanes.1-stage axial flow turbine. Maximum temperature 1850 F (1000)C.
Turbine (power)
Axial flow free turbine wheel attached to main gear train pinion and reduction gear.
Exhaust
Fixed area single outlet, exhausted downward.
Power take-off
Reduction gearbox at rear of unit. Output shaft 3,000 rpm.
Fuel system
Allied-signal-integral fuel system. pump, governor, internal relief valve, and flow control.
Ignition System
Bendix air-gap, ignition system. 1 igniter.
Lubrication
Sump type, Pressurized system.
Width and height
11.9 in and 12.0 in
Length
22.0 in
Weight
82.0 Ib
Power weight
1.09 shp/Ib
Fuel spec
Kerosene, or Jet-A
Fuel consumption
1.3 Ib/shp-hr
Oil spec; consumption
MIL-L-7808: 0.02phr
Rating
90 shp @ 60,400 power turbine rpm.
Boeing 502
Boeing 502 Engines currently in stock.
Manufacturer: The Boeing Co., Commercial Airplane Division, Turbine Program
Model: 502-6
Type: Turboshaft
Power: 160 bhp normal maximum (continuous)
Air Compressor: Single stage, centrifugal
Burners: Two: through-flow type
Turbine Stages: Two: compressor and output turbines
Compressor Turbine Speed: 36,500 rpm normal maximum (continuous)
Compressor Turbine Rotation: Counterclockwise, viewed from shaft end
Overspeed Limit: 3,210 to 3,290 rpm output shaft speed
Fuel: Kerosene or Jet-A
Oil: MIL-L-7808 OR MIL-L-23699
Electrical System: 24 Vdc
Weight: 200+ lbs (252 lbs stated in manual)
Dimensions: 43″L x 23″W x 23″H
Operating Limits:
Condition Minimum Normal Maximum
Turbine RPM Cranking 4,000 rpm 5,000 rpm 5,000 rpm
Idling 14,500 rpm 15,000 rpm 15,000 rpm
Rated Speed —– —– 36,500 rpm
Momentary —– —– 37,500 rpm
Turbine Oil Pres. Rated Speed 35 psi 50 psi 70 psi
Auto. Shutdown 18 psi 20 psi 20 psi
Fuel Pressure Starting 50 psi 100 psi 200 psi
Rated Speed —– 350 psi 500 psi
Idling Speed 10 psi 10-50 psi 50 psi
Exhaust Temp. Continuous —– 1150F(621C) 1225F(663C)
Auto. Shutdown —– 1300F(704C)
View more by category: Rotax GTS (1), JFS-100 (1), Boeing 502 (1), CAE-J402 (1), Boeing T-50 (1). .