EP2504228A4 - FLYING DEVICE - Google Patents

FLYING DEVICE

Info

Publication number
EP2504228A4
EP2504228A4 EP10832704.0A EP10832704A EP2504228A4 EP 2504228 A4 EP2504228 A4 EP 2504228A4 EP 10832704 A EP10832704 A EP 10832704A EP 2504228 A4 EP2504228 A4 EP 2504228A4
Authority
EP
European Patent Office
Prior art keywords
flying apparatus
flying
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Withdrawn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
EP10832704.0A
Other languages
German (de)
English (en)
French (fr)
Other versions
EP2504228A1 (en
Inventor
Raimo Hirvinen
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of EP2504228A1 publication Critical patent/EP2504228A1/en
Publication of EP2504228A4 publication Critical patent/EP2504228A4/en
Withdrawn legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/38Adjustment of complete wings or parts thereof
    • B64C3/44Varying camber
    • B64C3/50Varying camber by leading or trailing edge flaps
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C23/00Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/06Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C37/00Convertible aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/10All-wing aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/12Canard-type aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C5/00Stabilising surfaces
    • B64C5/08Stabilising surfaces mounted on, or supported by, wings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/10Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Toys (AREA)
EP10832704.0A 2009-11-27 2010-11-26 FLYING DEVICE Withdrawn EP2504228A4 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FI20096253A FI122848B (fi) 2009-11-27 2009-11-27 Lentolaite
PCT/FI2010/050969 WO2011064456A1 (en) 2009-11-27 2010-11-26 Flying apparatus

Publications (2)

Publication Number Publication Date
EP2504228A1 EP2504228A1 (en) 2012-10-03
EP2504228A4 true EP2504228A4 (en) 2014-07-09

Family

ID=41395299

Family Applications (1)

Application Number Title Priority Date Filing Date
EP10832704.0A Withdrawn EP2504228A4 (en) 2009-11-27 2010-11-26 FLYING DEVICE

Country Status (3)

Country Link
EP (1) EP2504228A4 (fi)
FI (1) FI122848B (fi)
WO (1) WO2011064456A1 (fi)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111003169B (zh) * 2019-12-24 2023-07-21 中国航空工业集团公司西安飞机设计研究所 一种可实现短距起降飞翼

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4267990A (en) * 1977-11-17 1981-05-19 Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter Haftung Method for steering an aircraft
US4485992A (en) * 1981-09-10 1984-12-04 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Leading edge flap system for aircraft control augmentation
WO2000017046A1 (fi) * 1998-09-24 2000-03-30 Raimo Hirvinen Process for changing to maximum angle of attack of a profile

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4285482A (en) 1979-08-10 1981-08-25 The Boeing Company Wing leading edge high lift device
US4899284A (en) 1984-09-27 1990-02-06 The Boeing Company Wing lift/drag optimizing system
US4739957A (en) 1986-05-08 1988-04-26 Advanced Aerodynamic Concepts, Inc. Strake fence flap
US5094411A (en) 1990-10-19 1992-03-10 Vigyan, Inc. Control configured vortex flaps
DE19850319C2 (de) 1998-11-02 2001-07-19 Deutsch Zentr Luft & Raumfahrt Flugzeugflügel mit stark gepfeilter Flügelvorderkante, insbesondere Deltaflügel

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4267990A (en) * 1977-11-17 1981-05-19 Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter Haftung Method for steering an aircraft
US4485992A (en) * 1981-09-10 1984-12-04 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Leading edge flap system for aircraft control augmentation
WO2000017046A1 (fi) * 1998-09-24 2000-03-30 Raimo Hirvinen Process for changing to maximum angle of attack of a profile

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of WO2011064456A1 *

Also Published As

Publication number Publication date
FI20096253A (fi) 2011-05-28
WO2011064456A1 (en) 2011-06-03
FI20096253A0 (sv) 2009-11-27
WO2011064456A9 (en) 2012-07-12
EP2504228A1 (en) 2012-10-03
FI122848B (fi) 2012-07-31

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Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20120627

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

DAX Request for extension of the european patent (deleted)
A4 Supplementary search report drawn up and despatched

Effective date: 20140606

RIC1 Information provided on ipc code assigned before grant

Ipc: B64C 39/12 20060101ALI20140602BHEP

Ipc: B64C 23/06 20060101ALI20140602BHEP

Ipc: B64C 3/50 20060101AFI20140602BHEP

Ipc: B64C 9/00 20060101ALI20140602BHEP

Ipc: B64C 39/10 20060101ALI20140602BHEP

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION HAS BEEN WITHDRAWN

18W Application withdrawn

Effective date: 20180410