Kuznetsov TV-2

From Wikipedia, the free encyclopedia
Jump to navigation Jump to search
TV-2
TypeTurboprop
National originSoviet Union
ManufacturerKuybyshev Engine Design Bureau
First run1951[1]
Major applicationsTupolev Tu-91[2]
Developed fromTV-022
Developed into2TV-2F
TV-12/NK-12

The Kuznetsov TV-2 was a turboprop engine, designed by the Kuybyshev Engine Design Bureau.

Applications

[edit | edit source]
TV-2F
Antonov An-8 (proposed)
Tupolev '101' (project)
Tupolev '102' (project)
Tupolev Tu-118 (project)
TV-2M
Tupolev Tu-91 (prototype only)
TV-2T
Antonov An-8 (proposed)

Specifications (TV-2F)

[edit | edit source]

Data from engine.aviaport.ru[3]

General characteristics

  • Type: Turboprop engine
  • Length:
  • Diameter:
  • Dry weight:

Components

Performance

  • Maximum power output:
    • 6,250 hp (4,660 kW)[3] at takeoff
    • 2,550 hp (1,900 kW)[3] in cruise
  • Overall pressure ratio: 5.8[3]
  • Air mass flow:
    • 30 kg/s (66 lb/s) at takeoff
    • 10.6 kg/s (23 lb/s) in cruise
  • Turbine inlet temperature: 1,150 K (880 °C; 1,610 °F)[3]
  • Specific fuel consumption:
    • 0.294 kg/(hp⋅h) at takeoff
    • 0.218 kg/(hp⋅h)[3] in cruise

See also

[edit | edit source]

Comparable engines

Related lists

References

[edit | edit source]
  1. ^ Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
  2. ^ Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
  3. ^ a b c d e f g h Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).