MX2015000626A - Configuracion de aeronave resistente a giros. - Google Patents

Configuracion de aeronave resistente a giros.

Info

Publication number
MX2015000626A
MX2015000626A MX2015000626A MX2015000626A MX2015000626A MX 2015000626 A MX2015000626 A MX 2015000626A MX 2015000626 A MX2015000626 A MX 2015000626A MX 2015000626 A MX2015000626 A MX 2015000626A MX 2015000626 A MX2015000626 A MX 2015000626A
Authority
MX
Mexico
Prior art keywords
aircraft
wing
spin resistant
stall
configuration
Prior art date
Application number
MX2015000626A
Other languages
English (en)
Other versions
MX363459B (es
Inventor
Jon Karkow
Matthew Gionta
John Roncz
Dieter Koehler
David Lednicer
Original Assignee
Icon Aircraft Inc
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 Icon Aircraft Inc filed Critical Icon Aircraft Inc
Publication of MX2015000626A publication Critical patent/MX2015000626A/es
Publication of MX363459B publication Critical patent/MX363459B/es

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/10—Shape of wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/10—Influencing air flow over aircraft surfaces by affecting boundary layer flow using other surface properties, e.g. roughness
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/58—Wings provided with fences or spoilers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C35/00—Flying-boats; Seaplanes
    • B64C35/001—Flying-boats; Seaplanes with means for increasing stability on the water
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C35/00—Flying-boats; Seaplanes
    • B64C35/008—Amphibious sea planes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/02—Tailplanes
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Tires In General (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Toys (AREA)

Abstract

Se describe una configuración y sistema para hacer que una aeronave sea resistente a giros. La resistencia de la aeronave a los giros se lleva a cabo al restringir una celda de parada para una región del ala (220) adyacente al fuselaje y distante de la punta del ala (210). Las características del ala que facilitan esta restricción incluyen, pero no se limitan a, uno o varios sujetadores (215), tiras de parada (320), generadores de vórtice (630), torsiones de ala (510-550), barridos de alas y estabilizadores horizontales. Solas o en combinación, las características de configuración de aeronaves incorporadas por la presente invención hacen que las aeronaves sean resistentes a giros al restringir la celda de parada, que permite que las superficies de control de la aeronave permanezcan operativas para controlar la aeronave.
MX2015000626A 2012-07-20 2013-07-19 Configuracion de aeronave resistente a giros. MX363459B (es)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201261674267P 2012-07-20 2012-07-20
US13/946,572 US9327828B2 (en) 2012-07-20 2013-07-19 Spin resistant aircraft configuration
PCT/US2013/051355 WO2014074182A1 (en) 2012-07-20 2013-07-19 Spin resistant aircraft configuration

Publications (2)

Publication Number Publication Date
MX2015000626A true MX2015000626A (es) 2015-04-14
MX363459B MX363459B (es) 2019-03-25

Family

ID=49945732

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2015000626A MX363459B (es) 2012-07-20 2013-07-19 Configuracion de aeronave resistente a giros.

Country Status (10)

Country Link
US (3) US9327828B2 (es)
EP (1) EP2874873B1 (es)
CN (1) CN104203748B (es)
AU (2) AU2013341766B2 (es)
BR (1) BR112015000821B1 (es)
CA (1) CA2878905C (es)
ES (1) ES2620628T3 (es)
MX (1) MX363459B (es)
RU (1) RU2640669C2 (es)
WO (1) WO2014074182A1 (es)

Families Citing this family (11)

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BR112015000821B1 (pt) * 2012-07-20 2022-01-25 Icon Aircraft, Inc Configuração para uma aeronave anfíbia de asa alta e sistema para configuração resistente a giro em parafuso
US8939410B2 (en) * 2013-02-06 2015-01-27 Reginald J Exton Boundary layer flow disruptors for delaying transition to turbulent flow
US10239606B2 (en) * 2013-12-04 2019-03-26 Tamarack Aerospace Group, Inc. Airflow interrupting devices
US20150361951A1 (en) * 2014-06-17 2015-12-17 Siemens Energy, Inc. Pressure side stall strip for wind turbine blade
FR3039129B1 (fr) * 2015-07-20 2017-07-07 Airbus Helicopters Ailette de fuselage d'aeronef et aeronef associe
DK178874B1 (en) * 2015-08-19 2017-04-18 Envision Energy (Jiangsu) Co Ltd Wind turbine blade with tripping device and method thereof
DE102019202354A1 (de) * 2019-02-21 2020-08-27 HORTEN Aircraft GmbH Schwanzloses Flugzeug
CN110920866A (zh) * 2019-11-18 2020-03-27 北京航空航天大学 一种通过机翼扰流板抑制飞机摇滚运动的方法
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US11869877B2 (en) 2021-08-06 2024-01-09 Sandisk Technologies Llc Bonded assembly including inter-die via structures and methods for making the same

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Also Published As

Publication number Publication date
CA2878905C (en) 2020-07-07
US9926071B2 (en) 2018-03-27
AU2013341766B2 (en) 2016-06-09
ES2620628T3 (es) 2017-06-29
US20140021302A1 (en) 2014-01-23
US10723444B2 (en) 2020-07-28
RU2640669C2 (ru) 2018-01-11
WO2014074182A1 (en) 2014-05-15
CA2878905A1 (en) 2014-05-15
CN104203748A (zh) 2014-12-10
RU2014151868A (ru) 2016-09-10
MX363459B (es) 2019-03-25
CN104203748B (zh) 2016-08-24
US9327828B2 (en) 2016-05-03
US20170021916A1 (en) 2017-01-26
AU2013341766A1 (en) 2015-01-22
AU2016225939B2 (en) 2018-04-05
EP2874873B1 (en) 2016-12-14
EP2874873A1 (en) 2015-05-27
BR112015000821B1 (pt) 2022-01-25
US20180178903A1 (en) 2018-06-28
AU2016225939A1 (en) 2016-09-29
BR112015000821A2 (pt) 2019-11-05

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