DE3617398A1 - Hubschrauber - Google Patents

Hubschrauber

Info

Publication number
DE3617398A1
DE3617398A1 DE19863617398 DE3617398A DE3617398A1 DE 3617398 A1 DE3617398 A1 DE 3617398A1 DE 19863617398 DE19863617398 DE 19863617398 DE 3617398 A DE3617398 A DE 3617398A DE 3617398 A1 DE3617398 A1 DE 3617398A1
Authority
DE
Germany
Prior art keywords
fuselage
helicopter
section
tail
fin
Prior art date
Legal status (The legal status 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 status listed.)
Withdrawn
Application number
DE19863617398
Other languages
German (de)
English (en)
Inventor
Dante Ballerio
Santino Pancotti
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Agusta SpA
Original Assignee
Costruzioni Aeronautiche Giovanni Augusta SpA
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 Costruzioni Aeronautiche Giovanni Augusta SpA filed Critical Costruzioni Aeronautiche Giovanni Augusta SpA
Publication of DE3617398A1 publication Critical patent/DE3617398A1/de
Withdrawn legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0045—Fuselages characterised by special shapes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C2025/325—Alighting gear characterised by elements which contact the ground or similar surface  specially adapted for helicopters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
DE19863617398 1985-05-30 1986-05-23 Hubschrauber Withdrawn DE3617398A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT8553439U IT8553439V0 (it) 1985-05-30 1985-05-30 Elicottero

Publications (1)

Publication Number Publication Date
DE3617398A1 true DE3617398A1 (de) 1987-12-03

Family

ID=11282772

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19863617398 Withdrawn DE3617398A1 (de) 1985-05-30 1986-05-23 Hubschrauber

Country Status (6)

Country Link
US (1) US4809930A (enExample)
JP (1) JPS6244800U (enExample)
DE (1) DE3617398A1 (enExample)
FR (1) FR2582615B1 (enExample)
GB (1) GB2175867B (enExample)
IT (1) IT8553439V0 (enExample)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5209430A (en) * 1991-11-07 1993-05-11 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Helicopter low-speed yaw control
USD357894S (en) 1993-09-20 1995-05-02 Bell Helicopter Textron Inc. Helicopter
USD363054S (en) 1994-08-30 1995-10-10 Bell Helicopter Textron Inc. Helicopter
USD375077S (en) 1995-01-24 1996-10-29 Bell Helicopter Textron Inc. Helicopter
USD388048S (en) * 1996-05-13 1997-12-23 Bell Helicopter Textron Inc. Helicopter
US6352220B1 (en) 2000-06-02 2002-03-05 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Helicopter tail boom with venting for alleviation and control of tail boom aerodynamic loads and method thereof
RU2246426C1 (ru) * 2003-07-21 2005-02-20 Открытое акционерное общество "Казанский вертолетный завод" Вертолет
RU2245821C1 (ru) * 2003-07-21 2005-02-10 Открытое акционерное общество "Казанский вертолётный завод" Система компенсации реактивного момента несущего винта одновинтового вертолёта
ITTO20040118A1 (it) * 2004-02-27 2004-05-27 Agusta Spa Elicottero
CN100398398C (zh) * 2006-04-29 2008-07-02 刘昌喆 伞面旋翼轨迹的直升机
DE602008006532D1 (de) * 2008-05-22 2011-06-09 Agusta Spa Drehmomentausgleichs-Heckrotorblatt für Hubschrauber
DE102008058029B3 (de) * 2008-11-18 2010-01-07 Deutsches Zentrum für Luft- und Raumfahrt e.V. Hubschrauber
FR3013677B1 (fr) * 2013-11-27 2015-12-04 Eurocopter France Carenage de sommet d'un giravion comportant un profil en goutte d'eau tronque dote d'un bossage a surface perturbee
CH710657A1 (de) * 2015-01-28 2016-07-29 Marenco Swisshelicopter Ag Hubschrauberkabine.
FR3054690B1 (fr) 2016-07-28 2021-10-22 Airbus Helicopters Procede d'optimisation des sections d'une poutre de queue destinee a un aeronef a voilure tournante

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3131892A (en) * 1962-06-11 1964-05-05 Eltra Corp Door latch assembly
FR1511006A (fr) * 1966-12-13 1968-01-26 Sud Aviation Dispositif directionnel et propulsif pour hélicoptère
US3544047A (en) * 1968-02-23 1970-12-01 Boeing Co Download reduction apparatus
US4103848A (en) * 1977-03-08 1978-08-01 United Technologies Corporation Variable incidence helicopter stabilator and fail safe actuator
US4306837A (en) * 1979-04-24 1981-12-22 Textron, Inc. Bearingless tail rotor for helicopters
US4544047A (en) * 1980-09-08 1985-10-01 American Standard Inc. Spring-applied, air-released, slack-adjusting parking brake
DE3371771D1 (en) * 1982-07-05 1987-07-02 Westland Plc Helicopter

Also Published As

Publication number Publication date
GB2175867B (en) 1988-09-28
GB8612764D0 (en) 1986-07-02
US4809930A (en) 1989-03-07
JPS6244800U (enExample) 1987-03-18
FR2582615A1 (fr) 1986-12-05
FR2582615B1 (fr) 1989-08-11
IT8553439V0 (it) 1985-05-30
GB2175867A (en) 1986-12-10

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Legal Events

Date Code Title Description
8127 New person/name/address of the applicant

Owner name: AGUSTA S.P.A., CASCINA COSTA DI SAMARATE, VARESE,

8128 New person/name/address of the agent

Representative=s name: ZENZ, J., DIPL.-ING., 4300 ESSEN HELBER, F., DIPL.

8141 Disposal/no request for examination