UA110507C2 - Літак - Google Patents

Літак

Info

Publication number
UA110507C2
UA110507C2 UAA201309879A UAA201309879A UA110507C2 UA 110507 C2 UA110507 C2 UA 110507C2 UA A201309879 A UAA201309879 A UA A201309879A UA A201309879 A UAA201309879 A UA A201309879A UA 110507 C2 UA110507 C2 UA 110507C2
Authority
UA
Ukraine
Prior art keywords
krill
litak
statements
great
attack
Prior art date
Application number
UAA201309879A
Other languages
English (en)
Inventor
Massimo Lucchesini
Emanuele Merlo
Original Assignee
Alenia Aermacchi Spa
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 Alenia Aermacchi Spa filed Critical Alenia Aermacchi Spa
Publication of UA110507C2 publication Critical patent/UA110507C2/ru

Links

Classifications

    • 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
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/0009—Aerodynamic aspects
    • 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
    • B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
    • 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
    • B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
    • B64C1/1476—Canopies; Windscreens or similar transparent elements
    • 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
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • 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
    • B64D7/00—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft
    • 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)
  • Fluid Mechanics (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Details Of Aerials (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Tires In General (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Mobile Radio Communication Systems (AREA)
  • Radio Relay Systems (AREA)
  • Control Of Turbines (AREA)

Abstract

Літак (10) з покращеними аеродинамічними характеристиками, адаптований для підтримання подовжньої стабільності по напрямку та дуже хорошої поведінки при помірно великому куті атаки. Вказаний літак (10) складається з фюзеляжу (12), до якого кріпляться крила (18, 20) певної форми, та носової частини (52). Зазначений літак (10) також містить пристрій керування вихорами (72) напливу переднього краю кореневої частини крила (НПККЧ), сформований з метою симетризації стрімкого зростання вихорів, які створюються таким НПККЧ при помірно великому куті атаки. Вказаний літак містить замінне обладнання зі щонайменше одним пристроєм розсіювання спадних радіолокаційних хвиль щонайменше на одній гарячій частині літака.
UAA201309879A 2011-02-14 2011-05-30 Літак UA110507C2 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IT000122A ITTO20110122A1 (it) 2011-02-14 2011-02-14 Configurazione velivolo a prestazioni aerodinamiche migliorate.
PCT/IB2011/001230 WO2012110845A1 (en) 2011-02-14 2011-05-30 Aircraft with improved aerodynamic performance

Publications (1)

Publication Number Publication Date
UA110507C2 true UA110507C2 (ru) 2016-01-12

Family

ID=44546067

Family Applications (1)

Application Number Title Priority Date Filing Date
UAA201309879A UA110507C2 (ru) 2011-02-14 2011-05-30 Літак

Country Status (13)

Country Link
US (1) US9284046B2 (ru)
EP (1) EP2675712B1 (ru)
KR (1) KR101840507B1 (ru)
CN (1) CN103476675B (ru)
BR (1) BR112013020203B1 (ru)
ES (1) ES2688994T3 (ru)
IL (1) IL227897A (ru)
IT (1) ITTO20110122A1 (ru)
PL (1) PL2675712T3 (ru)
SG (1) SG192725A1 (ru)
UA (1) UA110507C2 (ru)
WO (1) WO2012110845A1 (ru)
ZA (1) ZA201306092B (ru)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9233755B1 (en) * 2007-10-16 2016-01-12 Aerion Corporation Highly efficient supersonic laminar flow wing structure
US8991768B1 (en) * 2007-10-16 2015-03-31 Aerion Corporation Highly efficient transonic laminar flow wing
FR3000025B1 (fr) * 2012-12-21 2016-12-09 Airbus Aeronef comprenant un poste de pilotage delocalise en dehors d'une partie superieure de la pointe avant
CN105015795A (zh) * 2014-04-28 2015-11-04 张焰 飞机设计方法与方案
CN104443353B (zh) * 2014-12-15 2016-08-31 佛山市神风航空科技有限公司 一种变翼飞机
US9758253B2 (en) * 2015-06-25 2017-09-12 Northrop Grumman Systems Corporation Swept gradient boundary layer diverter
US10364021B2 (en) * 2016-09-26 2019-07-30 General Electric Company Aircraft having an aft engine and stabilizer root fillet
US20190185127A1 (en) * 2017-12-18 2019-06-20 Freedom Aircraft Ventures Llc Aircraft design and technology
US10814981B2 (en) * 2018-03-13 2020-10-27 Goodrich Corporation Ram air inlets having radar absorbing material
US11167836B2 (en) 2018-06-21 2021-11-09 Sierra Nevada Corporation Devices and methods to attach composite core to a surrounding structure
DE102020004273B4 (de) * 2020-02-26 2024-07-18 Airbus Defence and Space GmbH Luftfahrzeugstruktur mit einer Einlassöffnung für Triebwerksluft
KR102459628B1 (ko) * 2022-04-15 2022-10-28 국방과학연구소 비행체 흡입구의 불시동 방지 장치, 그것을 구비한 비행체 및 그것의 제어 방법
CN115352617B (zh) * 2022-07-05 2024-01-30 中国航空工业集团公司沈阳飞机设计研究所 一种飞机机头
CN115238378B (zh) * 2022-07-12 2023-07-07 中国航空工业集团公司沈阳飞机设计研究所 一种大迎角气动力设计方法

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3509568A (en) * 1968-07-08 1970-04-28 North American Rockwell Inlet attenuator assembly
US4132375A (en) * 1976-01-21 1979-01-02 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Vortex-lift roll-control device
DE3641286C3 (de) 1986-12-03 1998-06-10 Seewer Ag Burgdorf Verfahren zum Ausrollen von Teig
DE3641289A1 (de) 1986-12-03 1988-06-16 Messerschmitt Boelkow Blohm Verfahren und vorrichtung zur radartarnung von triebwerkseinlaeufen
DE3901010C1 (ru) * 1989-01-14 1990-08-23 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De
RU2144885C1 (ru) 1999-07-20 2000-01-27 Дондуков Александр Николаевич Маневренный учебно-тренировочный и многоцелевой самолет "як-130"
ITMI20012170A1 (it) 2001-10-18 2003-04-18 Aermacchi S P A Configurazione velivolo a prestazioni aerodinamiche migliorate
FR2891525B1 (fr) * 2005-09-30 2007-11-09 Airbus France Sas Dispositif de controle d'un sillage tourbillonnaire engendre par un element oblong sur l'extrados d'une surface portante d'un aeronef.
JP2007168491A (ja) * 2005-12-19 2007-07-05 Ishikawajima Harima Heavy Ind Co Ltd 航空機用インテークダクト
US7721989B2 (en) 2006-03-01 2010-05-25 The Boeing Company Multi-path inlet for aircraft engine
BRPI0603262B1 (pt) * 2006-08-08 2021-02-23 Yaborã Indústria Aeronáutica S.A asa de aeronave incluindo um slat no bordo de ataque da asa e um fence rígido preso a uma porção estruturalmente rígida não móvel da asa
US20100028684A1 (en) * 2008-07-31 2010-02-04 Jose Mariscal Conductive multilayer stack

Also Published As

Publication number Publication date
EP2675712B1 (en) 2018-07-04
BR112013020203A2 (pt) 2016-11-08
RU2013140287A (ru) 2015-03-27
ES2688994T3 (es) 2018-11-07
PL2675712T3 (pl) 2019-01-31
ZA201306092B (en) 2014-04-30
IL227897A (en) 2016-02-29
CN103476675A (zh) 2013-12-25
US20140070056A1 (en) 2014-03-13
SG192725A1 (en) 2013-09-30
CN103476675B (zh) 2016-08-24
WO2012110845A1 (en) 2012-08-23
EP2675712A1 (en) 2013-12-25
IL227897A0 (en) 2013-09-30
KR101840507B1 (ko) 2018-03-20
BR112013020203B1 (pt) 2021-02-02
ITTO20110122A1 (it) 2012-08-15
KR20140049966A (ko) 2014-04-28
US9284046B2 (en) 2016-03-15

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