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2. Axial fan design - Wikipedia

   en.wikipedia.org/wiki/Axial_fan_design

   An axial fan is a type of fan that causes gas to flow through it in an axial direction, parallel to the shaft about which the blades rotate. The flow is axial at entry and exit. The fan is designed to produce a pressure difference, and hence force, to cause a flow through the fan. Factors which determine the performance of the fan include the ...

3. Pratt & Whitney PW1000G - Wikipedia

   en.wikipedia.org/wiki/Pratt_&_Whitney_PW1000G

   Axial flow, 1 geared fan, 3 stage LPC, 8 stage HPC Axial flow, 1 geared fan, 2 stage LPC, 8 stage HPC Combustor: Talon-X Lean-Burn Combustor [126] Turbine: Axial flow, 2-stage HP, 3-stage LP Application A320neo family: Yakovlev MC-21: A220 family: E-Jet E2 190/195 X-66: E-Jet E2 175 SpaceJet M90/M100 Service entry 25 January 2016 Likely ...

4. Nidec - Wikipedia

   en.wikipedia.org/wiki/Nidec

   Acquired the axial-flow fan business from American company Torin Corporation, and established the locally incorporated company Nidec Torin Corporation in America. Started production of spindle motors for 3.5-inch hard disk device. 1988: October: The company listed its stock on the second section of the Osaka Stock Exchange, and the Kyoto Stock ...

5. Industrial fan - Wikipedia

   en.wikipedia.org/wiki/Industrial_fan

   Vaneaxial fans – These axial flow fans have a higher pressure capability due to the presence of static vanes. Variable pitch axial fans – The blades on these axial fans are manually adjustable to permit the blade angle to be changed. This allows operation over a much wider range of volume/pressure relationships.

6. Pratt & Whitney PW4000 - Wikipedia

   en.wikipedia.org/wiki/Pratt_&_Whitney_PW4000

   The Pratt & Whitney PW4000 is a family of dual-spool, axial-flow, high-bypass turbofan aircraft engines produced by Pratt & Whitney as the successor to the JT9D.It was first run in April 1984, was FAA certified in July 1986, and was introduced in June 1987.

7. General Electric GE9X - Wikipedia

   en.wikipedia.org/wiki/General_Electric_GE9X

   Dual rotor, axial flow, high bypass turbofan: Combustor Single annular Twin Annulus Premixing Swirler Control dual channel FADEC: Compressor: 1 fan, 3-stage LP, 11-stage HP Turbine: 2-stage HP, 6-stage LP Fan 134 in (3,404 mm) diameter, [26] 16 wide chord composite blades Length 224.0 in (5,690 mm) [Fan Spinner to TRF aft most flange] Width × ...