3525486

Information

• Patent Grant
• 3525486

• References
• Source

• Patent Number

  3,525,486

• Date Filed

  Not available

• Date Issued

  Tuesday, August 25, 1970
  54 years ago

• CPC

  • B64C23/06 - by generating vortices
  • B64C2700/6271 - by fluid flow around the aircraft
  • B64D2033/0226 - comprising boundary layer control means
  • Y02T50/162 - Wing tip vortex reduction

• US Classifications

  • 244 - Aeronautics and astronautics