Patent ID: 11970275
Assignee: ISRAEL AEROSPACE INDUSTRIES LTD.
Field: Transport (Mechanical engineering)
Classification: CPC B | IPC B

Claim 17:
18. The method according to claim 16, wherein each one of said port wing and said starboard wing comprises a flap arrangement and an aileron arrangement, and including one of the following:
wherein in step (C) a respective first set of secondary electrical propulsion units of each said first plurality of secondary electrical propulsion units is coupled to the respective port wing or starboard wing such as to provide corresponding jet flows directly to the full flap arrangement of the respective said port wing or starboard wing, and a respective second set of secondary electrical propulsion units each of each said first plurality of secondary electrical propulsion units is coupled to the respective port wing or starboard wing such as to provide corresponding jet flows directly to the aileron arrangement of the respective said port wing or starboard wing;
wherein in step (C) a respective first set of secondary electrical propulsion units of each said first plurality of secondary electrical propulsion units is coupled to the respective port wing or starboard wing such as to provide corresponding jet flows directly only to the full flap arrangement of the respective said port wing or starboard wing;
wherein each one of said port wing and said starboard wing comprises a flap arrangement and an aileron arrangement, and wherein in step (C) a respective first set of secondary electrical propulsion units of each said first plurality of secondary electrical propulsion units is coupled to the respective port wing or starboard wing such as to provide corresponding jet flows directly only to a portion of said flap arrangement of the respective said port wing or starboard wing; or
wherein each one of said port wing and said starboard wing comprises a flap arrangement and an aileron arrangement, and wherein in step (C) a respective first set of secondary electrical propulsion units of each said first plurality of secondary electrical propulsion units is coupled to the respective port wing or starboard wing such as to provide corresponding jet flows directly only to a portion of said flap arrangement of the respective said port wing or starboard wing, and, wherein in step (C) said secondary electrical propulsion units of each said first plurality are laterally distributed over a portion of the length of the respective said port wing or starboard wing.