3677501

Information

• Patent Grant
• 3677501

• References
• Source

• Patent Number

  3,677,501

• Date Filed

  Not available

• Date Issued

  Tuesday, July 18, 1972
  52 years ago

• CPC

  • B64D27/18 - within or attached to wing
  • F02K3/025 - the by-pass flow being at least partly used to create an independent thrust component
  • F02K3/04 - the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust
  • B64D2700/62956 - in jet propulsion aircraft

• US Classifications

  • 244 - Aeronautics and astronautics