UA106677C2 - Літак інтегрального аеродинамічного компонування - Google Patents
Літак інтегрального аеродинамічного компонуванняInfo
- Publication number
- UA106677C2 UA106677C2 UAA201302451A UAA201302451A UA106677C2 UA 106677 C2 UA106677 C2 UA 106677C2 UA A201302451 A UAA201302451 A UA A201302451A UA A201302451 A UAA201302451 A UA A201302451A UA 106677 C2 UA106677 C2 UA 106677C2
- Authority
- UA
- Ukraine
- Prior art keywords
- fuselage
- plane
- component plane
- aerodynamic component
- horizontal
- Prior art date
Links
- 230000004941 influx Effects 0.000 abstract 1
Classifications
-
- 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
- B64D27/20—Aircraft characterised by the type or position of power plants of jet type within, or attached to, fuselages
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C15/00—Attitude, flight direction, or altitude control by jet reaction
- B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
-
- 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
- B64C5/00—Stabilising surfaces
- B64C5/02—Tailplanes
-
- 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
-
- 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
- B64D2033/0266—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
- B64D2033/0286—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for turbofan engines
-
- 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
-
- 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
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Tires In General (AREA)
- Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
- Toys (AREA)
Abstract
Літак інтегрального аеродинамічного компонування містить фюзеляж, крило, консолі якого плавно зв'язані з фюзеляжем, горизонтальне і вертикальне оперення, дводвигунову силову установку. При цьому фюзеляж забезпечений напливом, який розташований над входом у повітрозабірники двигунів і включає керовані поворотні частини, середня частина фюзеляжу виконана сплощеною і утворена в подовжньому відношенні набором аеродинамічних профілів, мотогондоли двигунів рознесені одна від одної по горизонталі, а осі двигунів орієнтовані під гострим кутом до площини симетрії літака у напрямку польоту.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2010131640/11A RU2440916C1 (ru) | 2010-07-28 | 2010-07-28 | Самолет интегральной аэродинамической компоновки |
PCT/RU2011/000229 WO2012026846A1 (ru) | 2010-07-28 | 2011-04-07 | Самолет интегральной аэродинамической компоновки |
Publications (1)
Publication Number | Publication Date |
---|---|
UA106677C2 true UA106677C2 (uk) | 2014-09-25 |
Family
ID=45723663
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
UAA201302451A UA106677C2 (uk) | 2010-07-28 | 2011-07-04 | Літак інтегрального аеродинамічного компонування |
Country Status (8)
Country | Link |
---|---|
US (1) | US9180974B2 (uk) |
EP (1) | EP2599719A4 (uk) |
CN (1) | CN103209892B (uk) |
EA (1) | EA021280B1 (uk) |
IL (1) | IL224415A (uk) |
RU (1) | RU2440916C1 (uk) |
UA (1) | UA106677C2 (uk) |
WO (1) | WO2012026846A1 (uk) |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2472956C2 (ru) * | 2011-04-29 | 2013-01-20 | Открытое акционерное общество "ОКБ Сухого" | Сверхзвуковой регулируемый воздухозаборник |
GB201312593D0 (en) * | 2013-07-13 | 2013-08-28 | Mbda Uk Ltd | A thrust flow powered vehicle |
CN103538716B (zh) * | 2013-08-21 | 2016-09-07 | 林仕华 | 一种高效且稳定的斜形逆变机翼 |
CN105015795A (zh) * | 2014-04-28 | 2015-11-04 | 张焰 | 飞机设计方法与方案 |
RU2583824C2 (ru) * | 2014-08-01 | 2016-05-10 | Открытое акционерное общество "Авиационная холдинговая компания" Сухой" | Сверхзвуковой самолет с внутрифюзеляжными грузовыми отсеками |
CN104608917A (zh) * | 2015-01-28 | 2015-05-13 | 梧州晟裕科技有限公司 | 一种固定翼无人飞行器的尾翼结构 |
US10000274B2 (en) * | 2015-08-20 | 2018-06-19 | The Boeing Company | Mitigation of surface discontinuities between flight control surfaces and an airframe of an aircraft |
CN105523189B (zh) * | 2015-12-14 | 2017-11-21 | 成都飞机设计研究所 | 一种滑动变体可调caret进气道 |
CN106167089A (zh) * | 2016-07-19 | 2016-11-30 | 深圳市创翼睿翔天空科技有限公司 | 尾翼结构及具有其的无人机 |
CN106516086A (zh) * | 2016-10-19 | 2017-03-22 | 戈晓宁 | 高隐身无平尾升力体布局飞机 |
RU2632550C1 (ru) * | 2016-10-28 | 2017-10-05 | Публичное акционерное общество "Авиационная холдинговая компания "Сухой" | Летательный аппарат |
CN107284641B (zh) * | 2017-07-03 | 2023-09-08 | 安徽国援智能科技有限公司 | 一种适于超音速飞行的小型飞机气动外形 |
US20190185127A1 (en) * | 2017-12-18 | 2019-06-20 | Freedom Aircraft Ventures Llc | Aircraft design and technology |
US11059569B1 (en) * | 2017-12-29 | 2021-07-13 | United States Of America As Represented By The Administrator Of Nasa | Flight control system for aircraft having multi-functional flight control surface |
WO2019187828A1 (ja) * | 2018-03-29 | 2019-10-03 | 国立研究開発法人宇宙航空研究開発機構 | 超音速機の機体形状の設計方法、超音速機の生産方法及び超音速機 |
CN108910057B (zh) * | 2018-06-10 | 2024-03-29 | 东莞理工学院 | 一种具有多发动机的飞翼无人机 |
US11167836B2 (en) | 2018-06-21 | 2021-11-09 | Sierra Nevada Corporation | Devices and methods to attach composite core to a surrounding structure |
US11247776B2 (en) * | 2019-04-01 | 2022-02-15 | The Boeing Company | Aircraft having embedded engines |
CN110816870B (zh) * | 2019-09-30 | 2021-03-16 | 中国科学院力学研究所 | 一种改善宽域飞行器配平特性的设计方法 |
DE102020004273A1 (de) * | 2020-02-26 | 2021-08-26 | Airbus Defence and Space GmbH | Luftfahrzeugstruktur mit einer Einlassöffnung für Triebwerksluft |
WO2021251807A1 (ru) * | 2020-06-11 | 2021-12-16 | Алдан Асанович САПАРГАЛИЕВ | Тяговые поверхности аппарата самоперемещения |
RU2749175C1 (ru) * | 2020-07-10 | 2021-06-07 | Публичное акционерное общество "Авиационная холдинговая компания "Сухой" | Самолет интегральной аэродинамической компоновки |
CN112298578B (zh) * | 2020-11-27 | 2021-07-27 | 成都云鼎智控科技有限公司 | 无人飞行器发动机的控制系统 |
CN117087865B (zh) * | 2023-10-20 | 2024-01-26 | 中国空气动力研究与发展中心计算空气动力研究所 | 一种飞翼气动飞行器及控制方法 |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1029106A (en) * | 1965-02-19 | 1966-05-11 | Rolls Royce | Aircraft |
FR1552118A (uk) * | 1967-11-17 | 1969-01-03 | ||
US4025007A (en) * | 1974-08-16 | 1977-05-24 | Herbert Kaniut | Shifting horizontal tail with helical motions |
US4037808A (en) * | 1974-08-16 | 1977-07-26 | Herbert Kaniut | Travelling tail-unit with circular arc motion |
US4456204A (en) * | 1981-09-29 | 1984-06-26 | The Boeing Company | Deployable inlet for aeroplane center boost engine |
FR2635075B1 (fr) * | 1988-08-04 | 1994-09-23 | Onera (Off Nat Aerospatiale) | Entree d'air supersonique bidimensionnelle et asymetrique pour l'air de combustion d'un moteur d'aeronef |
FR2710607B1 (fr) * | 1993-10-01 | 1995-12-01 | Onera (Off Nat Aerospatiale) | Entrée d'air supersonique et hypersonique bidimensionnelle, à trois rampes mobiles, pour l'air de combustion d'un moteur d'aéronef . |
US5957405A (en) * | 1997-07-21 | 1999-09-28 | Williams International Co., L.L.C. | Twin engine aircraft |
RU2140376C1 (ru) | 1997-12-10 | 1999-10-27 | АООТ "ОКБ Сухого" | Самолет интегральной аэродинамической компоновки |
US20050045764A1 (en) * | 2003-08-29 | 2005-03-03 | Supersonic Aerospace International, Llc | Canard position and dihedral for boom reduction and pitch/directional control |
US7520123B2 (en) * | 2005-05-12 | 2009-04-21 | Lockheed Martin Corporation | Mixing-enhancement inserts for pulse detonation chambers |
CN201362361Y (zh) * | 2008-12-25 | 2009-12-16 | 李振荣 | 前后攻击型战斗机 |
-
2010
- 2010-07-28 RU RU2010131640/11A patent/RU2440916C1/ru active
-
2011
- 2011-04-07 CN CN201180047006.9A patent/CN103209892B/zh not_active Expired - Fee Related
- 2011-04-07 EP EP11820241.5A patent/EP2599719A4/en not_active Withdrawn
- 2011-04-07 EA EA201300030A patent/EA021280B1/ru not_active IP Right Cessation
- 2011-04-07 WO PCT/RU2011/000229 patent/WO2012026846A1/ru active Application Filing
- 2011-04-07 US US13/812,602 patent/US9180974B2/en not_active Expired - Fee Related
- 2011-07-04 UA UAA201302451A patent/UA106677C2/uk unknown
-
2013
- 2013-01-27 IL IL224415A patent/IL224415A/en active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
EA021280B1 (ru) | 2015-05-29 |
IL224415A (en) | 2017-12-31 |
EA201300030A1 (ru) | 2013-05-30 |
CN103209892A (zh) | 2013-07-17 |
US9180974B2 (en) | 2015-11-10 |
EP2599719A1 (en) | 2013-06-05 |
EP2599719A4 (en) | 2017-11-15 |
WO2012026846A1 (ru) | 2012-03-01 |
RU2440916C1 (ru) | 2012-01-27 |
US20140145027A1 (en) | 2014-05-29 |
CN103209892B (zh) | 2015-09-16 |
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