FI20060858A0 - Ilma-aluksen kaarielementti, siipi, ohjainpinta sekä vakaaja - Google Patents

Ilma-aluksen kaarielementti, siipi, ohjainpinta sekä vakaaja

Info

Publication number
FI20060858A0
FI20060858A0 FI20060858A FI20060858A FI20060858A0 FI 20060858 A0 FI20060858 A0 FI 20060858A0 FI 20060858 A FI20060858 A FI 20060858A FI 20060858 A FI20060858 A FI 20060858A FI 20060858 A0 FI20060858 A0 FI 20060858A0
Authority
FI
Finland
Prior art keywords
wing
aircraft
stabilizer
control surface
arch element
Prior art date
Application number
FI20060858A
Other languages
English (en)
Swedish (sv)
Other versions
FI20060858A (fi
FI119726B (fi
Inventor
Juha Maekelae
Juha Halme
Lauri Halme
Mikko Hoffren
Original Assignee
Patria Aerostructures Oy
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 Patria Aerostructures Oy filed Critical Patria Aerostructures Oy
Priority to FI20060858A priority Critical patent/FI119726B/fi
Publication of FI20060858A0 publication Critical patent/FI20060858A0/fi
Priority to EP07823147.9A priority patent/EP2066563B1/en
Priority to PCT/FI2007/050510 priority patent/WO2008037847A1/en
Priority to US12/442,140 priority patent/US8245971B2/en
Priority to ES07823147.9T priority patent/ES2532596T3/es
Publication of FI20060858A publication Critical patent/FI20060858A/fi
Application granted granted Critical
Publication of FI119726B publication Critical patent/FI119726B/fi

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B64C3/187—Ribs
    • 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
    • B64C5/00—Stabilising surfaces

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Wind Motors (AREA)
FI20060858A 2006-09-26 2006-09-26 Ilma-aluksen kaarielementti, siipi, ohjainpinta sekä vakaaja FI119726B (fi)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FI20060858A FI119726B (fi) 2006-09-26 2006-09-26 Ilma-aluksen kaarielementti, siipi, ohjainpinta sekä vakaaja
EP07823147.9A EP2066563B1 (en) 2006-09-26 2007-09-25 Curved element, wing, control surface and stabilizer for aircraft
PCT/FI2007/050510 WO2008037847A1 (en) 2006-09-26 2007-09-25 Curved element, wing, control surface and stabilizer for aircraft
US12/442,140 US8245971B2 (en) 2006-09-26 2007-09-25 Curved element, wing, control surface and stabilizer for aircraft
ES07823147.9T ES2532596T3 (es) 2006-09-26 2007-09-25 Elemento curvo, ala, superficie de control y estabilizador para una aeronave

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FI20060858 2006-09-26
FI20060858A FI119726B (fi) 2006-09-26 2006-09-26 Ilma-aluksen kaarielementti, siipi, ohjainpinta sekä vakaaja

Publications (3)

Publication Number Publication Date
FI20060858A0 true FI20060858A0 (fi) 2006-09-26
FI20060858A FI20060858A (fi) 2008-05-22
FI119726B FI119726B (fi) 2009-02-27

Family

ID=37067181

Family Applications (1)

Application Number Title Priority Date Filing Date
FI20060858A FI119726B (fi) 2006-09-26 2006-09-26 Ilma-aluksen kaarielementti, siipi, ohjainpinta sekä vakaaja

Country Status (5)

Country Link
US (1) US8245971B2 (fi)
EP (1) EP2066563B1 (fi)
ES (1) ES2532596T3 (fi)
FI (1) FI119726B (fi)
WO (1) WO2008037847A1 (fi)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FI119726B (fi) * 2006-09-26 2009-02-27 Patria Aerostructures Oy Ilma-aluksen kaarielementti, siipi, ohjainpinta sekä vakaaja
DE102008059653B4 (de) * 2008-11-28 2015-07-09 Gkn Aerospace Services Ltd. Flächiges Bauteil eines Fluggerätes und Verfahren zu dessen Herstellung
GB0900494D0 (en) * 2009-01-14 2009-02-11 Airbus Uk Ltd Aerofoil Structure
GB0906157D0 (en) * 2009-04-09 2009-05-20 Airbus Uk Ltd Improved wing structure
DE102009060695A1 (de) 2009-12-29 2011-07-07 Airbus Operations GmbH, 21129 Flugzeugrumpf und Hautfeld
GB201020152D0 (en) * 2010-11-29 2011-01-12 Airbus Uk Ltd Aircraft panel structure and aircraft panel structure manufacturing method for alleviation of stress
TW201300651A (zh) * 2011-06-21 2013-01-01 zheng-xin Mei 減少流線形物體阻力的方法及其應用
GB201120707D0 (en) * 2011-12-01 2012-01-11 Airbus Operations Ltd Leading edge structure
CN103454102A (zh) * 2012-06-04 2013-12-18 北京宇航系统工程研究所 蒙皮加筋圆柱壳结构扭转等效刚度优化获取方法
JP6093192B2 (ja) * 2013-01-25 2017-03-08 三菱航空機株式会社 航空機の機体用パネル、航空機の翼
US9341207B2 (en) * 2013-07-30 2016-05-17 Gulfstream Aerospace Corporation Web component and method of making a web component
AT516211A1 (de) 2014-08-11 2016-03-15 Facc Ag Steuerflächenelement
EP3009344B1 (en) * 2014-10-16 2019-05-29 Airbus Operations GmbH Panel structure and associated method
US10196126B2 (en) 2015-04-07 2019-02-05 The Boeing Company Rib structure and method of forming thereof
ES2661888T3 (es) * 2015-05-05 2018-04-04 Airbus Operations, S.L. Plano de cola horizontal con una caja de torsión de nervaduras múltiples
US10427778B2 (en) * 2016-03-14 2019-10-01 The Boeing Company Heat shield assembly and method
US10315751B2 (en) * 2016-04-07 2019-06-11 The Boeing Company Stiffened beam assembly
US10220935B2 (en) * 2016-09-13 2019-03-05 The Boeing Company Open-channel stiffener
ES2800182T3 (es) * 2017-07-13 2020-12-28 Airbus Operations Sl Disposición estructural de caja para una aeronave y procedimiento de fabricación de la misma
EP3447280B1 (en) * 2017-08-21 2020-12-16 LM Wind Power International Technology II ApS A bulkhead unit, a wind turbine blade comprising the bulkhead unit, and methods of assembling and installing the bulkhead unit
GB2568654B (en) * 2017-09-27 2022-05-04 Gkn Aerospace Services Ltd Box rib
CN109263860A (zh) * 2018-11-19 2019-01-25 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种机翼翼梁及机翼
US11046420B2 (en) * 2019-10-23 2021-06-29 The Boeing Company Trailing edge flap having a waffle grid interior structure
RU2750508C1 (ru) * 2020-07-09 2021-06-29 Марлен Мелитонович Абрамишвили Стабилизатор винтового воздушного потока винтомоторного самолёта
US11780179B2 (en) 2021-09-02 2023-10-10 Rohr, Inc. Thermoplastic composite panel with corrugated peaks and troughs stiffening systems and methods

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US1875651A (en) * 1930-05-29 1932-09-06 William E Phelan Aerofoil section
US2329818A (en) * 1937-07-31 1943-09-21 Gen Motors Corp Photocell control
US2392818A (en) 1940-11-18 1946-01-15 Lockheed Aircraft Corp Double skin sheet metal structural element
US2395205A (en) * 1941-03-11 1946-02-19 Budd Edward G Mfg Co Aircraft structure
US2429144A (en) * 1941-03-26 1947-10-14 Budd Co Method of assembling aircraft structures
US2382950A (en) * 1942-09-14 1945-08-14 Budd Edward G Mfg Co Aircraft structure
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US4084029A (en) * 1977-07-25 1978-04-11 The Boeing Company Sine wave beam web and method of manufacture
US4230293A (en) * 1978-08-02 1980-10-28 Boeing Commercial Airplane Company Composite structure and method of making
US4452657A (en) * 1982-09-15 1984-06-05 The Boeing Company Composite integral web stiffening method
US5687538A (en) * 1995-02-14 1997-11-18 Super Stud Building Products, Inc. Floor joist with built-in truss-like stiffner
JPH10258463A (ja) 1997-03-19 1998-09-29 Fuji Heavy Ind Ltd 複合材の小骨およびその成形方法
DE19922295C1 (de) * 1999-05-14 2000-07-27 Eurocopter Deutschland Unterbodenstruktur einer Rumpfzelle eines Luftfahrzeuges
JP4526698B2 (ja) * 2000-12-22 2010-08-18 富士重工業株式会社 複合材成形品及びその製造方法
US20030226935A1 (en) 2001-11-02 2003-12-11 Garratt Matthew D. Structural members having improved resistance to fatigue crack growth
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GB0426944D0 (en) * 2004-12-08 2005-01-12 Airbus Uk Ltd A trussed structure
FI119726B (fi) * 2006-09-26 2009-02-27 Patria Aerostructures Oy Ilma-aluksen kaarielementti, siipi, ohjainpinta sekä vakaaja

Also Published As

Publication number Publication date
EP2066563A1 (en) 2009-06-10
ES2532596T3 (es) 2015-03-30
US20100181427A1 (en) 2010-07-22
FI20060858A (fi) 2008-05-22
FI119726B (fi) 2009-02-27
US8245971B2 (en) 2012-08-21
WO2008037847A1 (en) 2008-04-03
EP2066563B1 (en) 2015-01-07
EP2066563A4 (en) 2013-05-01

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