Williams FJ44
Template:Short description Template:Primary
| FJ44 | |
|---|---|
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| A Williams FJ44-3ATW turbofan engine | |
| Type | Turbofan |
| National origin | United States |
| Manufacturer | Williams International |
| First run | 1985[1] |
| Major applications | Beechcraft Premier I Cessna CitationJet Piper PiperJet Altaire Saab 105 Grob G180 SPn Pilatus PC-24 |
| Developed into | Williams FJ33 |
The Williams FJ44 is a family of small, two-spool, turbofan engines produced by Williams International for the light business jet market. Until the recent boom in the very light jet market, the FJ44 was one of the smallest turbofans available for civilian applications. Although a Williams design, Rolls-Royce was brought into the project at an early stage to design, develop, and manufacture an air-cooled high-pressure (HP) turbine for the engine. The FJ44 first flew on July 12, 1988 on the Scaled Composites/Beechcraft Triumph aircraft.
The Williams FJ33 is a newer, smaller engine based on the basic FJ44 design.
Development
Production started in 1992 with the Script error: No such module "convert". thrust FJ44-1A. The FJ44-1C is derated to Script error: No such module "convert".. The uprated to Script error: No such module "convert". FJ44-2A was introduced in 1997. The Script error: No such module "convert". thrust FJ44-3A was introduced in 2004. In 2005, a new low end version, the FJ44-1AP, was introduced, with a Script error: No such module "convert". takeoff thrust. Released in 2007 was the new Script error: No such module "convert". thrust FJ44-4. In 2010 this engine was in use on the Cessna CJ4, and since 2018 also on the new Pilatus PC-24.
Design
The FJ44-1A has a single stage blisk fan plus a single intermediate pressure (IP) booster stage, both driven by a 2 stage low pressure (LP) turbine, and supercharging a single stage centrifugal high pressure (HP) compressor, driven by a single stage uncooled high pressure (HP) turbine. The combustor is an impingement cooled annular design. Fuel is delivered to the combustor through an unusual rotating fuel nozzle system, rather than the standard fuel-air mixers or vapourisers. The bypass duct runs the full length of the engine. The FJ44-2A has two additional booster compressor stages.
Variants
- FJ44-1A
- Script error: No such module "convert". thrust, production started in 1992, Script error: No such module "convert". diameter fan, SFC at full thrust at SLS, ISA is understood to be 0.456 lb/(hr lbf),
- FJ44-1AP
- Script error: No such module "convert". takeoff thrust, introduced in 2005, 5% better specific fuel consumption, lower internal temperatures, similar to the -1A with a higher pressure ratio fan, a new combustor and LP turbine, a new full length bypass duct/exhaust mixer and a dual channel FADEC.[2]
- FJ44-1C
- Script error: No such module "convert". thrust, derated version of the FJ44-1A, SFC of Script error: No such module "convert"..[3][4]
- FJ44-2A
- Script error: No such module "convert". thrust, introduced in 1997, larger Script error: No such module "convert". diameter fan, with two additional booster stages to increase core flow, centrifugal compressor throttled-back aerodynamically to a lower HPC pressure ratio than the -1, exhaust mixer and a fuel electronic control unit.[5]
- FJ44-2C
- Script error: No such module "convert". thrust, similar to the -2A with an integrated hydromechanical fuel control unit.
- FJ44-3A
- Script error: No such module "convert". thrust, 2004 introduction, similar to the -2A with a larger fan and dual channel FADEC unit.[6]
- FJ44-3A-24
- Script error: No such module "convert". thrust, derated -3A.
- FJ44-3AP
- Script error: No such module "convert". thrust.[7]
- FJ44-4A
- Script error: No such module "convert". thrust, released in 2007, hi-tech fan of larger diameter than the -3 unit.[8] Used on the Cessna CJ4 and the Pilatus PC-24.
- FJ44-4C
- 3,450 lbf (15.3kN) thrust. Used on the upcoming Honda HA-480 Echelon.[9][10]
- FJ44-4M
- Williams-Rolls F129
- Military designation for the derated FJ44-1C with Script error: No such module "convert". thrust.
Applications
| Variant | Application | Type | Deliveries |
|---|---|---|---|
| FJ44-1[12] | Cessna CitationJet CJ1/CJ1+/M2 | Business jet | 1993- |
| SAAB Sk60 | Jet trainer | re-engine | |
| FJ44-2[13] | Beechcraft Premier 1A | Business jet | 2001-2012 |
| Cessna CitationJet CJ2 | Business jet | 2000-2005 | |
| Cessna Citation 501SP | Business jet | re-engineTemplate:Efn | |
| Cessna Citation 550 | Business jet | re-engineTemplate:Efn | |
| Scaled Composites Proteus | Experimental | 1998 | |
| Syberjet SJ30 | Business jet | 2007-2009 | |
| Learjet 25 | Business jet | re-engineTemplate:Efn | |
| Virgin Atlantic GlobalFlyer | Experimental | 2005 | |
| FJ44-3[14] | Cessna CitationJet CJ2+/CJ3+ | Business jet | 2004- |
| Cessna Citation 550 | Business jet | re-engineTemplate:Efn | |
| Nextant 400XTi | Business jet | re-engine | |
| FJ44-4[15] | Cessna CitationJet CJ4 | Business jet | 2010- |
| Hawker 400XPR | Business jet | re-engine | |
| Pilatus PC-24 | Business jet | 2018- | |
| FJ44-4M | Aero L-39 Skyfox | Jet trainer Light attack aircraft |
2022- |
| FJ44-4M-34 | Alenia Aermacchi M-345 | Jet trainer | 2018- |
| not deliveredScript error: No such module "Unsubst". | Cessna 526 CitationJetTemplate:Efn | Jet trainer | 2 prototypes |
| Eviation Jets EV-20 Vantage Jet | Business jet | 1 prototype | |
| Grob G180 SPn | Business jet | 4 prototypes | |
| Hawker 200 | Business jet | Cancelled | |
| Lockheed Martin Polecat | Drone | Crashed | |
| Lockheed Martin RQ-3 DarkStar | Drone | Cancelled | |
| Piper PA-47 PiperJet/Altaire | Business jet | 1 prototype | |
| Scaled Composites Triumph | Business jet | 1 prototype |
Specifications
| Variant | FJ44-1AP[17] | FJ44-2[18] | FJ44-3[19] | FJ44-4[20] |
|---|---|---|---|---|
| Configuration | Twin-spool turbofan with 1-stage fan and annular combustor | |||
| LP compressor | 1-stage axial | 3-stage axial | ||
| HP compressor | 1-stage centrifugal | |||
| Turbine | 1-stage HP, 2-stage LP | |||
| Thrust | Template:Cvt | Template:Cvt | Template:Cvt | Template:Cvt |
| Weight | Template:Cvt | Template:Cvt | Template:Cvt | Template:Cvt |
| Length | Template:Cvt | Template:Cvt | Template:Cvt | Template:Cvt |
| Diameter | Template:Cvt | Template:Cvt | Template:Cvt | Template:Cvt |
See also
Related development
Related lists
References
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- ↑ Script error: No such module "citation/CS1".
- ↑ FJ44-1AP Template:Webarchive at www.williams-int.com, Accessed 2006-05-07
- ↑ FJ44-1 Template:Webarchive at www.williams-int.com, Accessed 2006-05-07
- ↑ FJ44 for military trainer aircraft Template:Webarchive at defence.rolls-royce.com Template:Webarchive, Accessed 2006-05-07
- ↑ FJ44-2 at www.williams-int.com, Accessed 2006-05-07
- ↑ FJ44-3 Template:Webarchive at www.williams-int.com, Accessed 2006-05-07
- ↑ Williams Fanjet Family, Accessed 2020-02-20
- ↑ FJ44-4 Template:Webarchive at www.williams-int.com, Accessed 2010-03-12
- ↑ Script error: No such module "citation/CS1".
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Notes
External links
Template:Williams aeroengines Template:US military gas turbine aeroengines Template:Swedish military gas turbine aeroengines