NL88777C - - Google Patents

Info

Publication number
NL88777C
NL88777C NL88777DA NL88777C NL 88777 C NL88777 C NL 88777C NL 88777D A NL88777D A NL 88777DA NL 88777 C NL88777 C NL 88777C
Authority
NL
Netherlands
Application number
Publication date
Application granted granted Critical
Publication of NL88777C publication Critical patent/NL88777C/xx

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • B64C27/33Rotors having flexing arms

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
NL88777D NL88777C (en:Method)

Publications (1)

Publication Number Publication Date
NL88777C true NL88777C (en:Method) 1900-01-01

Family

ID=1833711

Family Applications (1)

Application Number Title Priority Date Filing Date
NL88777D NL88777C (en:Method)

Country Status (1)

Country Link
NL (1) NL88777C (en:Method)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2397979A1 (fr) * 1977-07-22 1979-02-16 Messerschmitt Boelkow Blohm Rotor sans articulation de battement ni de trainee
EP2949579A1 (en) * 2014-05-28 2015-12-02 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Flexbeam unit with at least one twisted flexbeam element

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2397979A1 (fr) * 1977-07-22 1979-02-16 Messerschmitt Boelkow Blohm Rotor sans articulation de battement ni de trainee
EP2949579A1 (en) * 2014-05-28 2015-12-02 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Flexbeam unit with at least one twisted flexbeam element
US10005552B2 (en) 2014-05-28 2018-06-26 Airbus Helicopters Deutschland GmbH Flexbeam unit with at least one twisted flexbeam element

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