GE G6F00HFH6CM8FP6PU6CWXX F110 Engine Variant (F-14 Tomcat Configuration)
GE G6F00HFH6CM8FP6PU6CWXX F110 Engine Variant (F-14 Tomcat Configuration)
Manufacturer: General Electric
Product No.: G6F00HFH6CM8FP6PU6CWXX
Condition:1000 in stock
Product Type: F110 Engine Variant (F-14 Tomcat Configuration)
Product Origin: USA
Payment: T/T, Western Union
Weight: 1000g
Shipping port: Xiamen
Warranty: 12 months
- 24/7 Support
- 30-Day Returns
- Fast Shipping
Product Details
| Parameter | Details |
|---|---|
| Manufacturer | General Electric |
| Model/Part Number | G6F00HFH6CM8FP6PU6CWXX |
| Description | F110 Engine Variant (F-14 Tomcat Configuration) |
Product Overview
| Parameter | Details |
|---|---|
| Part Number | G6F00HFH6CM8FP6PU6CWXX |
| Product Name | F110-GE-400 Turbofan Engine |
| Application | Propulsion system for the Grumman F-14 Tomcat fighter aircraft, providing twin-engine power for high-performance supersonic flight and carrier operations |
| Compatibility | Grumman F-14A/B/D Tomcat variants; supports afterburning for combat maneuvers and supercruise capabilities |
| Function | Twin-spool low-bypass turbofan with afterburner, delivering high thrust-to-weight ratio for agile fighter performance and extended range |
Functional Specifications
| Parameter | Details |
|---|---|
| Engine Type | Afterburning low-bypass turbofan |
| Thrust (Dry) | 17,600 lbf (78 kN) |
| Thrust (Afterburner) | 28,200 lbf (125 kN) |
| Bypass Ratio | 0.85:1 |
| Length | 17.2 ft (5.24 m) |
| Diameter | 46.5 in (1.18 m) |
| Dry Weight | 3,920 lb (1,778 kg) |
| Overall Pressure Ratio | 28:1 |
| Turbine Inlet Temperature | 2,600°F (1,427°C) |
| Fuel Type | JP-5 (naval standard), JP-8 compatible |
| Maintenance Interval | 1,500 flight hours |
| Special Features | Digital electronic engine control (DEEC), variable stator vanes for surge protection, thrust vectoring compatibility |
| Standards Compliance | MIL-STD-5007, FAA certification, NATO STANAG |
Product Description
Product Details
| Parameter | Details |
|---|---|
| Manufacturer | General Electric |
| Model/Part Number | G6F00HFH6CM8FP6PU6CWXX |
| Description | F110 Engine Variant (F-14 Tomcat Configuration) |
Product Overview
| Parameter | Details |
|---|---|
| Part Number | G6F00HFH6CM8FP6PU6CWXX |
| Product Name | F110-GE-400 Turbofan Engine |
| Application | Propulsion system for the Grumman F-14 Tomcat fighter aircraft, providing twin-engine power for high-performance supersonic flight and carrier operations |
| Compatibility | Grumman F-14A/B/D Tomcat variants; supports afterburning for combat maneuvers and supercruise capabilities |
| Function | Twin-spool low-bypass turbofan with afterburner, delivering high thrust-to-weight ratio for agile fighter performance and extended range |
Functional Specifications
| Parameter | Details |
|---|---|
| Engine Type | Afterburning low-bypass turbofan |
| Thrust (Dry) | 17,600 lbf (78 kN) |
| Thrust (Afterburner) | 28,200 lbf (125 kN) |
| Bypass Ratio | 0.85:1 |
| Length | 17.2 ft (5.24 m) |
| Diameter | 46.5 in (1.18 m) |
| Dry Weight | 3,920 lb (1,778 kg) |
| Overall Pressure Ratio | 28:1 |
| Turbine Inlet Temperature | 2,600°F (1,427°C) |
| Fuel Type | JP-5 (naval standard), JP-8 compatible |
| Maintenance Interval | 1,500 flight hours |
| Special Features | Digital electronic engine control (DEEC), variable stator vanes for surge protection, thrust vectoring compatibility |
| Standards Compliance | MIL-STD-5007, FAA certification, NATO STANAG |