IT1392667B1 - Pala del rotore per un velivolo ad ala rotante - Google Patents

Pala del rotore per un velivolo ad ala rotante

Info

Publication number
IT1392667B1
IT1392667B1 ITMI2008A002254A ITMI20082254A IT1392667B1 IT 1392667 B1 IT1392667 B1 IT 1392667B1 IT MI2008A002254 A ITMI2008A002254 A IT MI2008A002254A IT MI20082254 A ITMI20082254 A IT MI20082254A IT 1392667 B1 IT1392667 B1 IT 1392667B1
Authority
IT
Italy
Prior art keywords
rotary aircraft
shovel
rotor
rotor shovel
aircraft
Prior art date
Application number
ITMI2008A002254A
Other languages
English (en)
Inventor
Valentin Kloeppel
Peter Janker
Original Assignee
Eurocopter Deutschland
Eads Deutschland Gmbh
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Eurocopter Deutschland, Eads Deutschland Gmbh filed Critical Eurocopter Deutschland
Publication of ITMI20082254A1 publication Critical patent/ITMI20082254A1/it
Application granted granted Critical
Publication of IT1392667B1 publication Critical patent/IT1392667B1/it

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B64C27/46—Blades
    • B64C27/463—Blade tips
ITMI2008A002254A 2007-12-20 2008-12-18 Pala del rotore per un velivolo ad ala rotante IT1392667B1 (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102007062490A DE102007062490B4 (de) 2007-12-20 2007-12-20 Rotorblatt für ein Drehflügelflugzeug

Publications (2)

Publication Number Publication Date
ITMI20082254A1 ITMI20082254A1 (it) 2009-06-21
IT1392667B1 true IT1392667B1 (it) 2012-03-16

Family

ID=40690727

Family Applications (1)

Application Number Title Priority Date Filing Date
ITMI2008A002254A IT1392667B1 (it) 2007-12-20 2008-12-18 Pala del rotore per un velivolo ad ala rotante

Country Status (3)

Country Link
US (1) US8152465B2 (it)
DE (1) DE102007062490B4 (it)
IT (1) IT1392667B1 (it)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8944365B2 (en) * 2010-09-09 2015-02-03 Groen Brothers Aviation, Inc. Mission-adaptive rotor blade
US9604722B1 (en) 2010-11-02 2017-03-28 Groen Aeronautics Corporation Mission-adaptive rotor blade
FR3005301B1 (fr) * 2013-05-03 2015-05-29 Eurocopter France Rotor carene d'aeronef, et giravion
FR3045564B1 (fr) 2015-12-21 2018-08-17 Airbus Helicopters Pale de rotor d'aeronef a geometrie adaptee pour l'amelioration acoustique lors de vols d'approche et l'amelioration des performances en vols stationnaire et d'avancement
FR3045565B1 (fr) 2015-12-21 2018-07-27 Airbus Helicopters Pale de rotor d'aeronef a geometrie adaptee pour l'ameloration acoustique lors d'un vol d'approche et l'amelioration des performances en vol d'avancement

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4324530A (en) * 1980-01-21 1982-04-13 United Technologies Corp. Helicopter blade with a tip having a selected combination of sweep, taper and anhedral to improve hover efficiency
FR2782307B1 (fr) * 1998-08-17 2000-10-13 Onera (Off Nat Aerospatiale) Procede pour la reduction du bruit d'interaction pales-tourbillons engendre par une voilure tournante
US6394397B1 (en) * 2000-12-06 2002-05-28 The Boeing Company Lifting surface with active variable tip member and method for influencing lifting surface behavior therewith

Also Published As

Publication number Publication date
DE102007062490B4 (de) 2011-07-28
ITMI20082254A1 (it) 2009-06-21
DE102007062490A1 (de) 2009-07-02
US20090169381A1 (en) 2009-07-02
US8152465B2 (en) 2012-04-10

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