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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/82—Rotorcraft; 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)
Publications (1)
Publication Number | Publication Date |
---|---|
NL16887C true NL16887C (ko) |
Family
ID=1784653
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
NL16887D NL16887C (ko) |
Country Status (1)
Country | Link |
---|---|
NL (1) | NL16887C (ko) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2409917A1 (fr) * | 2010-07-20 | 2012-01-25 | Eurocopter | Procédé et aéronef à voilure tournante muni d'un moyen de stabilisation minimisant le phénoméne de bosse d'assiette |
EP2878536A1 (en) * | 2013-11-29 | 2015-06-03 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Advanced pitch stabilizer |
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0
- NL NL16887D patent/NL16887C/xx active
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2409917A1 (fr) * | 2010-07-20 | 2012-01-25 | Eurocopter | Procédé et aéronef à voilure tournante muni d'un moyen de stabilisation minimisant le phénoméne de bosse d'assiette |
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 (en) * | 2013-11-29 | 2015-06-03 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Advanced pitch stabilizer |
US9381995B2 (en) | 2013-11-29 | 2016-07-05 | Airbus Helicopters Deutschland GmbH | Advanced pitch stabilizer |
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NL16887C (ko) |