General Electric CF700

From Wikipedia, the free encyclopedia
Jump to navigation Jump to search
CF700
File:General Electric CF700 on Dassault Falcon 20 N921ML.jpg
A Dassault Falcon 20 nacelle with its distinctive bypass intake
TypeTurbofan
National originUnited States
ManufacturerGeneral Electric
First run1960s
Major applicationsDassault Falcon 20
North American Sabreliner
Developed fromGeneral Electric CJ610

The General Electric CF700 (military designation TF37) is an aft-fan turbofan development of the CJ610 turbojet. The fan blades are an extension of the low-pressure turbine blades.

Variants

[edit | edit source]
CF700-2B
Baseline aft-fan CJ610 variant rated at 4,200 lbf (19,000 N) for take-off
CF700-2V
The 2B modified for continuous vertical operation on the Lunar Landing Research Vehicle (LLRV) and Lunar Landing Training Vehicle (LLTV)
TF37-GE-1
Military version of the CF700-2V on the Boeing Model 853-21 Quiet Bird

Applications

[edit | edit source]

Specifications (CF700)

[edit | edit source]

Data from [1][2]

General characteristics

  • Type: Two-spool aft-fan turbofan
  • Length: 75.5 in (1,918 mm)
  • Diameter: 33 in (838 mm)
  • Dry weight: 735 lb (333.4 kg) with optional thrust reverser

Components

  • Compressor: 8 stage high pressure compressor + 1 stage fan directly driven by the free LP turbine
  • Turbine: 2 stage high pressure turbine, 1 stage low pressure turbine
  • Fuel type: Aviation kerosene

Performance

See also

[edit | edit source]

Related development

Comparable engines

Related lists

References

[edit | edit source]
  1. ^ Model CF700. GE AE Website Archived 2010-01-16 at the Wayback Machine. Accessed 2 Nov 2009.
  2. ^ Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
  • Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
  • Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
[edit | edit source]