PL361221A1 - Skrzydło samolotu - Google Patents

Skrzydło samolotu

Info

Publication number
PL361221A1
PL361221A1 PL03361221A PL36122103A PL361221A1 PL 361221 A1 PL361221 A1 PL 361221A1 PL 03361221 A PL03361221 A PL 03361221A PL 36122103 A PL36122103 A PL 36122103A PL 361221 A1 PL361221 A1 PL 361221A1
Authority
PL
Poland
Prior art keywords
aircraft wing
wing
aircraft
Prior art date
Application number
PL03361221A
Other languages
English (en)
Other versions
PL202380B1 (pl
Inventor
Włodzimierz Gnarowski
Wojciech Kania
Anna Gnarowska
Original Assignee
Instytut Lotnictwa
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 Instytut Lotnictwa filed Critical Instytut Lotnictwa
Priority to PL361221A priority Critical patent/PL202380B1/pl
Priority to US10/564,168 priority patent/US20060175469A1/en
Priority to EP04748878A priority patent/EP1646559A1/en
Priority to PCT/PL2004/000054 priority patent/WO2005005251A1/en
Priority to CA002555880A priority patent/CA2555880A1/en
Priority to BRPI0411950-9A priority patent/BRPI0411950A/pt
Publication of PL361221A1 publication Critical patent/PL361221A1/pl
Publication of PL202380B1 publication Critical patent/PL202380B1/pl

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B64C9/20—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by multiple flaps
    • 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
    • Y02T50/30—Wing lift efficiency

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)
  • Power-Operated Mechanisms For Wings (AREA)
  • Toys (AREA)
PL361221A 2003-07-11 2003-07-11 Skrzydło samolotu PL202380B1 (pl)

Priority Applications (6)

Application Number Priority Date Filing Date Title
PL361221A PL202380B1 (pl) 2003-07-11 2003-07-11 Skrzydło samolotu
US10/564,168 US20060175469A1 (en) 2003-07-11 2004-07-09 Wing of aircraft
EP04748878A EP1646559A1 (en) 2003-07-11 2004-07-09 Wing of aircraft
PCT/PL2004/000054 WO2005005251A1 (en) 2003-07-11 2004-07-09 Wing of aircraft
CA002555880A CA2555880A1 (en) 2003-07-11 2004-07-09 Wing of an aircraft
BRPI0411950-9A BRPI0411950A (pt) 2003-07-11 2004-07-09 asa de aeronave

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL361221A PL202380B1 (pl) 2003-07-11 2003-07-11 Skrzydło samolotu

Publications (2)

Publication Number Publication Date
PL361221A1 true PL361221A1 (pl) 2005-01-24
PL202380B1 PL202380B1 (pl) 2009-06-30

Family

ID=34057048

Family Applications (1)

Application Number Title Priority Date Filing Date
PL361221A PL202380B1 (pl) 2003-07-11 2003-07-11 Skrzydło samolotu

Country Status (6)

Country Link
US (1) US20060175469A1 (pl)
EP (1) EP1646559A1 (pl)
BR (1) BRPI0411950A (pl)
CA (1) CA2555880A1 (pl)
PL (1) PL202380B1 (pl)
WO (1) WO2005005251A1 (pl)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2746151B1 (en) 2012-12-19 2017-04-12 Airbus Operations GmbH Flap system for an aircraft, method for adjusting the lift of an aircraft and aircraft comprising a main wing and at least one flap system
JP6440293B2 (ja) * 2014-06-13 2018-12-19 国立研究開発法人宇宙航空研究開発機構 モーフィング翼
CN109515686B (zh) * 2018-11-07 2021-09-21 西安航空学院 一种自适应后缘机动襟翼机构
CN109515687B (zh) * 2018-11-07 2021-09-21 西安航空学院 基于油气弹簧的自适应后缘机动襟翼机构
US11447233B2 (en) * 2019-08-26 2022-09-20 The Boeing Company Low load shear out auxiliary support joint
CN116443242B (zh) * 2022-11-29 2025-11-14 南京航空航天大学 一种基于气压传动且用于直升机格尼襟翼的驱动装置

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE748146C (de) * 1937-10-29 1944-10-27 Joseph Ksoll Flugzeugtragfluegel
US4471928A (en) * 1980-08-13 1984-09-18 The Boeing Company Extendible airfoil track assembly
DE3527497A1 (de) * 1985-07-31 1987-02-12 Airbus Gmbh Tragfluegel mit ausfahrbarer klappe und veraenderbarer woelbung
US5651513A (en) * 1995-03-01 1997-07-29 Northrop Grumman Corporation Linear flap drive system
US5711496A (en) * 1995-06-30 1998-01-27 Nusbaum; Steve R. STOL aircraft and wing slat actuating mechanism for same

Also Published As

Publication number Publication date
US20060175469A1 (en) 2006-08-10
EP1646559A1 (en) 2006-04-19
BRPI0411950A (pt) 2006-08-29
WO2005005251A1 (en) 2005-01-20
PL202380B1 (pl) 2009-06-30
WO2005005251B1 (en) 2005-03-17
CA2555880A1 (en) 2005-01-20

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