fbpx
Wikipedia

Walter M602

The Walter M602 is a turboprop aircraft engine produced by Walter Aircraft Engines of the Czech Republic, used on the Let L-610.

M602
M602 on display at the Kbely Aviation Museum
Type Turboprop
National origin Czech Republic
Manufacturer Walter Aircraft Engines
First run 25 February 1986.[1]
Major applications Let L-610

Applications edit

Specification edit

Data from Jane's All the World's Aircraft 2005–2006[2][3]

General characteristics

  • Type: Three-spool turboprop engine
  • Length: 2565 mm (M602A), 2285 mm (M602B)
  • Diameter: 753 mm
  • Dry weight: 570 kg (M602A), 480 kg (M602B)

Components

  • Compressor: 2-spool centrifugal compressor
  • Combustors: Annular combustion chamber[1]
  • Turbine: 1-stage HP axial turbine (with internally cooled blades), 1-stage axial IP compressor, 2-stage LP axial power turbine
  • Fuel type: Aviation kerosene
  • Oil system: pressure spray

Performance

  • Maximum power output: 1,360 kW (1,820 hp) (M602A), maximum continuous 1,200 kW (1,600 hp),[1] 1,500 kW (2,000 hp) (M602B)
  • Overall pressure ratio: 12[1]
  • Air mass flow: 7.33 kg (16.2 lb)/s
  • Turbine inlet temperature: 1388K[1]
  • Fuel consumption: 0.330 kg/kWh (0.543 lb/(hp⋅h))[1]
  • Power-to-weight ratio: 2.39 kW/kg (M602A), 3.13 kW/kg (M602B)

See also edit

Related lists

References edit

  1. ^ a b c d e f "Turbovrtulový motor M602" (in Czech).
  2. ^ Jane's All the World's Aircraft. 2005–2006. p. 847.
  3. ^ "CREDITABLE COMMUTER" (PDF). Flight International: 24–30. 28 February 1990. Retrieved 14 December 2015.

walter, m602, turboprop, aircraft, engine, produced, walter, aircraft, engines, czech, republic, used, m602, m602, display, kbely, aviation, museum, type, turboprop, national, origin, czech, republic, manufacturer, walter, aircraft, engines, first, february, 1. The Walter M602 is a turboprop aircraft engine produced by Walter Aircraft Engines of the Czech Republic used on the Let L 610 M602 M602 on display at the Kbely Aviation Museum Type Turboprop National origin Czech Republic Manufacturer Walter Aircraft Engines First run 25 February 1986 1 Major applications Let L 610 Contents 1 Applications 2 Specification 2 1 General characteristics 2 2 Components 2 3 Performance 3 See also 4 ReferencesApplications editLet L 610Specification editData from Jane s All the World s Aircraft 2005 2006 2 3 General characteristics Type Three spool turboprop engine Length 2565 mm M602A 2285 mm M602B Diameter 753 mm Dry weight 570 kg M602A 480 kg M602B Components Compressor 2 spool centrifugal compressor Combustors Annular combustion chamber 1 Turbine 1 stage HP axial turbine with internally cooled blades 1 stage axial IP compressor 2 stage LP axial power turbine Fuel type Aviation kerosene Oil system pressure spray Performance Maximum power output 1 360 kW 1 820 hp M602A maximum continuous 1 200 kW 1 600 hp 1 1 500 kW 2 000 hp M602B Overall pressure ratio 12 1 Air mass flow 7 33 kg 16 2 lb s Turbine inlet temperature 1388K 1 Fuel consumption 0 330 kg kWh 0 543 lb hp h 1 Power to weight ratio 2 39 kW kg M602A 3 13 kW kg M602B See also editRelated lists List of aircraft enginesReferences edit nbsp Wikimedia Commons has media related to Walter M602 a b c d e f Turbovrtulovy motor M602 in Czech Jane s All the World s Aircraft 2005 2006 p 847 CREDITABLE COMMUTER PDF Flight International 24 30 28 February 1990 Retrieved 14 December 2015 Retrieved from https en wikipedia org w index php title Walter M602 amp oldid 1102340817, wikipedia, wiki, book, books, library,

article

, read, download, free, free download, mp3, video, mp4, 3gp, jpg, jpeg, gif, png, picture, music, song, movie, book, game, games.