DE3569711D1 - Nacelle and wing assembly - Google Patents

Nacelle and wing assembly

Info

Publication number
DE3569711D1
DE3569711D1 DE8585201285T DE3569711T DE3569711D1 DE 3569711 D1 DE3569711 D1 DE 3569711D1 DE 8585201285 T DE8585201285 T DE 8585201285T DE 3569711 T DE3569711 T DE 3569711T DE 3569711 D1 DE3569711 D1 DE 3569711D1
Authority
DE
Germany
Prior art keywords
nacelle
wing assembly
wing
assembly
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.)
Expired
Application number
DE8585201285T
Other languages
English (en)
Inventor
Mark I Goldhammer
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.)
Boeing Co
Original Assignee
Boeing Co
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=24759470&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE3569711(D1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of DE3569711D1 publication Critical patent/DE3569711D1/de
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C7/00—Structures or fairings not otherwise provided for
    • B64C7/02—Nacelles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/02—Power-plant nacelles, fairings, or cowlings associated with wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Wind Motors (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
DE8585201285T 1984-12-28 1985-08-08 Nacelle and wing assembly Expired DE3569711D1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US68720084A 1984-12-28 1984-12-28

Publications (1)

Publication Number Publication Date
DE3569711D1 true DE3569711D1 (en) 1989-06-01

Family

ID=24759470

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8585201285T Expired DE3569711D1 (en) 1984-12-28 1985-08-08 Nacelle and wing assembly

Country Status (2)

Country Link
EP (1) EP0186220B1 (de)
DE (1) DE3569711D1 (de)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3917970A1 (de) * 1988-06-17 1989-12-21 Gen Electric An der tragflaeche befestigtes, mantelloses geblaesetriebwerk
CN103612746B (zh) 2013-10-24 2016-09-21 中国商用飞机有限责任公司 翼吊布局飞机中吊挂的整流罩结构

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4449683A (en) * 1979-01-03 1984-05-22 The Boeing Company Aerodynamically contoured, low drag wing engine and engine nacelle combination
US4314681A (en) * 1979-08-31 1982-02-09 General Electric Company Drag-reducing component
EP0111785A1 (de) * 1982-12-20 1984-06-27 The Boeing Company Mit Laminarströmung und kleinem stossbedingtem Widerstandsprofil

Also Published As

Publication number Publication date
EP0186220A3 (en) 1986-08-13
EP0186220A2 (de) 1986-07-02
EP0186220B1 (de) 1989-04-26

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Legal Events

Date Code Title Description
8363 Opposition against the patent
8365 Fully valid after opposition proceedings
8320 Willingness to grant licences declared (paragraph 23)