3456905

Information

• Patent Grant
• 3456905

• References
• Source

• Patent Number

  3,456,905

• Date Filed

  Not available

• Date Issued

  Tuesday, July 22, 1969
  55 years ago

• CPC

  • B64C30/00 - Supersonic-type aircraft
  • B64C1/0009 - Aerodynamic aspects
  • B64C3/54 - Varying in area
  • B64C5/12 - for retraction against or within fuselage or nacelle
  • B64C17/00 - Aircraft stabilisation not otherwise provided for
  • B64C23/06 - by generating vortices
  • B64C2001/0045 - Fuselages characterised by special shapes
  • B64C2700/6219 - by auxiliary fixed or movable surfaces or other special devices, or surfaces acting as parachutes
  • Y02T50/162 - Wing tip vortex reduction

• US Classifications

  • 244 - Aeronautics and astronautics