Westinghouse J30

{{Short description|American pioneering jet aircraft engine}}

{{Use dmy dates|date=March 2023}}

{{Use American English|date=March 2023}}

{{Infobox aircraft begin

|name = J30

|image = File:Westinghouse J30 NAN8-47.jpg

|caption =

}}

{{Infobox aircraft engine

|type= Turbojet

|national origin = United States

|manufacturer= Westinghouse Aviation Gas Turbine Division

|first run= 19 March 1943

|major applications= FH Phantom

|number built =

|developed from =

|variants with their own articles =

|developed into = Westinghouse J32
Westinghouse J34

}}

The Westinghouse J30, initially known as the Westinghouse 19XB, was a turbojet engine developed by Westinghouse Electric Corporation. It was the first American-designed turbojet to run, and only the second axial-flow turbojet to run outside Germany (after the British Metropolitan-Vickers F.2).Gunston, p. 240-241

A simple and robust unit with six-stage compressor, annular combustor, and single-stage turbine, it initially gave 1,200 pounds of thrust but improved to 1,600 in production versions. Its first flight was under a FG Corsair in January 1944. It was developed into the smaller J32, and the successful Westinghouse J34, an enlarged version which produced 3,000 pounds of thrust.

Variants

;19A:Prototypes and initial production, boost engines{{Citation needed|date=April 2020}}

;19B:Increased mass flow version delivering {{convert|1,400|lbf|kN|abbr=on|2}} at 18,000 rpm at sea level, added gearbox to allow engine to be a prime driver{{Citation needed|date=April 2020}}

;19XB-2B:Company designation for WE-20.{{cite book |last=Wilkinson |first=Paul H. |title=Aircraft engines of the World 1950 |year=1950 |publisher=Sir Isaac Pitman & Sons Ltd. |location=London |edition=11th |pages=60–61}}

;XJ30-WE-7: {{convert|1,600|lbf|kN|abbr=on}} for Northrop X-4{{Citation needed|date=April 2020}}

;XJ30-WE-8: originally designated J43{{Cite web|url=http://www.designation-systems.net/usmilav/engines.html#_Turbine4668|title = Designations of U.S. Military Aero Engines}}

;XJ30-WE-9: {{convert|1,600|lbf|kN|abbr=on}} for Northrop X-4{{Citation needed|date=April 2020}}

;J30-WE-20: production engines delivering {{convert|1,600|lbf|kN|abbr=on}} thrust, Internal model 19XB-2B{{Citation needed|date=April 2020}}

Applications

Specifications (Westinghouse 19A)

{{jetspecs

|ref={{cite book|last=Wilkinson|first=Paul H.|title=Aircraft Engines of the world 1946|year=1946|publisher=Sir Isaac Pitman & Sons|location=London|pages=278–281}}

|type=Axial flow turbojet

|length={{convert|100|in|mm|abbr=on|1}}, 19B {{convert|104.5|in|mm|abbr=on|1}}

|diameter={{convert|19|in|mm|abbr=on|1}}

|weight={{convert|830|lb|kg|abbr=on|1}}, 19B {{convert|809|lb|kg|abbr=on|1}}

|compressor=6-stage axial

|combustion=Annular stainless steel

|turbine=Single-stage axial

|fueltype=100/130 gasoline

|oilsystem=pressure spray at {{convert|40|psi|kPa|abbr=on|1}} dry sump, 60 S.U. secs (10.2 cSt) (AN-0-6A) grade oil

|power=

|thrust= {{convert|1,360|lbf|kN|abbr=on|2}} at 18,000 rpm at sea level, 19B {{convert|1,400|lbf|kN|abbr=on|2}} at 18,000 rpm at sea level

|compression=3:1

|bypass=

|aircon={{convert|26.5|lb/s|kg/s|abbr=on|2}} at 17,000 rpm, 19B {{convert|30|lb/s|kg/s|abbr=on|2}} at 18,000 rpm

|turbinetemp= {{convert|1,500|°F|°C|abbr=on|0}}

|fuelcon=

|specfuelcon={{convert|1.35|tsfc|si tsfc}}, 19B {{convert|1.28|tsfc|si tsfc}}

|power/weight=

|thrust/weight=1.639, 19B 1.724

  • Normal thrust, static: {{convert|1,160|lbf|kN|abbr=on|2}} at 18,000 rpm at sea level, 19B {{convert|1,170|lbf|kN|abbr=on|2}} at 17,000 rpm at sea level
  • Military thrust, flight: {{convert|660|lbf|kN|abbr=on|2}} at 17,200 rpm at altitude, 19B {{convert|525|lbf|kN|abbr=on|2}} at 18,000 rpm at altitude
  • Normal thrust, flight: {{convert|570|lbf|kN|abbr=on|2}} at 16,260 rpm at altitude, 19B {{convert|465|lbf|kN|abbr=on|2}} at 17,000 rpm at altitude

}}

See also

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|similar engines=

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Notes

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References

  • {{cite book |last= Gunston |first= Bill |title= World Encyclopedia of Aero Engines, 5th Edition |year= 2006 |publisher= Sutton Publishing Limited |location= Phoenix Mill, Gloucestershire, England, UK |isbn= 0-7509-4479-X |pages= 240–241 }}
  • {{cite book|last=Wilkinson|first=Paul H.|title=Aircraft Engines of the world 1946|year=1946|publisher=Sir Isaac Pitman & Sons|location=London|pages=278–281}}
  • {{cite book|last=Christiansen|first=Paul J. |title=Early Westinghouse Axial Turbojets|year=2019|publisher=Bleeg Publishing|location=Olney, Maryland|pages=360–361}}