NL16887C - - Google Patents

Info

Publication number
NL16887C
NL16887C NL16887DA NL16887C NL 16887 C NL16887 C NL 16887C NL 16887D A NL16887D A NL 16887DA NL 16887 C NL16887 C NL 16887C
Authority
NL
Netherlands
Application number
Publication of NL16887C publication Critical patent/NL16887C/xx

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/82Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
NL16887D NL16887C (de)

Publications (1)

Publication Number Publication Date
NL16887C true NL16887C (de)

Family

ID=1784653

Family Applications (1)

Application Number Title Priority Date Filing Date
NL16887D NL16887C (de)

Country Status (1)

Country Link
NL (1) NL16887C (de)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2409917A1 (de) * 2010-07-20 2012-01-25 Eurocopter Verfahren und Luftfahrzeug mit Drehfahrwerk, das mit einem Stabilisationsmittel zur Minimierung des attitude hump -Phänomens ausgestattet ist
EP2878536A1 (de) * 2013-11-29 2015-06-03 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Erweiterter Steigungsstabilisator
USD1040728S1 (en) 2021-05-18 2024-09-03 Leonardo S.P.A. Helicopter
USD1041386S1 (en) 2021-05-18 2024-09-10 Leonardo S.P.A. Helicopter toy

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2409917A1 (de) * 2010-07-20 2012-01-25 Eurocopter Verfahren und Luftfahrzeug mit Drehfahrwerk, das mit einem Stabilisationsmittel zur Minimierung des attitude hump -Phänomens ausgestattet ist
FR2962972A1 (fr) * 2010-07-20 2012-01-27 Eurocopter France Procede et aeronef a voilure tournante muni d'un moyen de stabilisation minimisant le phenomene de bosse d'assiette
EP2878536A1 (de) * 2013-11-29 2015-06-03 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Erweiterter Steigungsstabilisator
US9381995B2 (en) 2013-11-29 2016-07-05 Airbus Helicopters Deutschland GmbH Advanced pitch stabilizer
USD1040728S1 (en) 2021-05-18 2024-09-03 Leonardo S.P.A. Helicopter
USD1041386S1 (en) 2021-05-18 2024-09-10 Leonardo S.P.A. Helicopter toy

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NL16887C (de)