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Williams FJ33

The Williams FJ33 is an American family of turbofan jet engines intended for use in very light jet aircraft. The FJ33 is a scaled-down version of the FJ44 engine. The FJ33-5A is the latest version certified in June 2016.[2]

FJ33
Type Turbofan
National origin United States
Manufacturer Williams International
First run 1998 [1]
Major applications Cirrus Vision SF50
Diamond D-Jet
Developed from Williams FJ44

Design

Engine configuration is a single stage fan, with booster stage, driven by a two-stage LP turbine, supercharging a centrifugal HP compressor, driven by a single stage HP turbine.[3] An annular combustor is featured.

The FJ33 has a dry weight of less than 300 lb (140 kg), overall diameter of 18.36 in (466 mm), 38.43 in (976 mm) overall length, and produces between 1,000 lbf (4,400 N) and 1,800 lbf (8,000 N) static thrust. Specific fuel consumption at 1,200 lbf (5,300 N) thrust (SLS, ISA) is understood to be 0.486 lb/(lbf⋅h) (13.8 g/(kN⋅s)).

Variants

  • FJ33-1
  • FJ33-2
  • FJ33-3
  • FJ33-4-A11
  • FJ33-4
  • FJ33-4-17M
  • FJ33-4-18M
  • FJ33-4A-19
  • FJ33-5A
  • Jahesh-700

Iranian Reverse engineered variant serving as high endurance UAV powerplant.[4][5]

Applications

Specifications (FJ33-5A)

General characteristics

  • Type: turbofan
  • Length: 38.43 in (976 mm)
  • Diameter: 18.36 in (466 mm),
  • Dry weight: less than 300 lb (140 kg)

Components

  • Compressor:

Performance

See also

Related development

Related lists

References

  1. ^ "P&WC unveils light jet study". Flight International. 28 October 1998.
  2. ^ "Williams International FJ33-5A Turbofan FAA-Certified". 8 June 2016. Retrieved 10 June 2016.
  3. ^ https://sistemas.anac.gov.br/certificacao/Produtos/Espec/EM-9303-05i.pdf[bare URL PDF]
  4. ^ "Iran Flaunts New Missile and Jet Engine Technology". The Washington Institute. Retrieved 2022-06-10.
  5. ^ "Iran's 1st turbofan engine: Jahesh-700". iranpress.com. Retrieved 2022-06-10.

External links

  • Williams Product Information FJ33
  • List of jets designed to use FJ33

williams, fj33, this, article, relies, excessively, references, primary, sources, please, improve, this, article, adding, secondary, tertiary, sources, find, sources, news, newspapers, books, scholar, jstor, november, 2021, learn, when, remove, this, template,. This article relies excessively on references to primary sources Please improve this article by adding secondary or tertiary sources Find sources Williams FJ33 news newspapers books scholar JSTOR November 2021 Learn how and when to remove this template message The Williams FJ33 is an American family of turbofan jet engines intended for use in very light jet aircraft The FJ33 is a scaled down version of the FJ44 engine The FJ33 5A is the latest version certified in June 2016 2 FJ33Type TurbofanNational origin United StatesManufacturer Williams InternationalFirst run 1998 1 Major applications Cirrus Vision SF50 Diamond D JetDeveloped from Williams FJ44 Contents 1 Design 2 Variants 3 Applications 4 Specifications FJ33 5A 4 1 General characteristics 4 2 Components 4 3 Performance 5 See also 6 References 7 External linksDesign EditEngine configuration is a single stage fan with booster stage driven by a two stage LP turbine supercharging a centrifugal HP compressor driven by a single stage HP turbine 3 An annular combustor is featured The FJ33 has a dry weight of less than 300 lb 140 kg overall diameter of 18 36 in 466 mm 38 43 in 976 mm overall length and produces between 1 000 lbf 4 400 N and 1 800 lbf 8 000 N static thrust Specific fuel consumption at 1 200 lbf 5 300 N thrust SLS ISA is understood to be 0 486 lb lbf h 13 8 g kN s Variants EditFJ33 1 FJ33 2 FJ33 3 FJ33 4 A11 FJ33 4 FJ33 4 17M FJ33 4 18M FJ33 4A 19 FJ33 5A Jahesh 700Iranian Reverse engineered variant serving as high endurance UAV powerplant 4 5 Applications EditAdam A700 ATG Javelin Cirrus Vision SF50 Diamond D Jet Epic Elite Flaris LAR01 Spectrum S 33 Independence Sport Jet II Eclipse 700Specifications FJ33 5A EditGeneral characteristics Type turbofan Length 38 43 in 976 mm Diameter 18 36 in 466 mm Dry weight less than 300 lb 140 kg Components Compressor Performance Maximum thrust 1 846 lbf 8 21 kN Specific fuel consumption 0 486 lb lbf h 13 77 g kN s Thrust to weight ratio 6See also EditRelated development Williams EJ22 Williams FJ44Related lists List of aircraft enginesReferences Edit P amp WC unveils light jet study Flight International 28 October 1998 Williams International FJ33 5A Turbofan FAA Certified 8 June 2016 Retrieved 10 June 2016 https sistemas anac gov br certificacao Produtos Espec EM 9303 05i pdf bare URL PDF Iran Flaunts New Missile and Jet Engine Technology The Washington Institute Retrieved 2022 06 10 Iran s 1st turbofan engine Jahesh 700 iranpress com Retrieved 2022 06 10 External links Edit Wikimedia Commons has media related to Williams FJ33 Williams Product Information FJ33 List of jets designed to use FJ33 Retrieved from https en wikipedia org w index php title Williams FJ33 amp oldid 1092479602, wikipedia, wiki, book, books, library,

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