CN103797229B - 用于调整超音速进气道的方法 - Google Patents

用于调整超音速进气道的方法 Download PDF

Info

Publication number: CN103797229B
Authority: CN; China
Prior art keywords: adjustable panel; panel; rear portion; anterior; adjustable
Prior art date: 2011-04-29
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.): Active

Application number

CN201280032672.XA

Other languages

English (en)

Chinese (zh)

Other versions

CN103797229A (zh

Inventor

亚历山大·尼古拉耶维奇·达维坚科

米哈伊尔·尤里耶维奇·斯特雷勒茨

弗拉迪米尔·亚历山德罗维奇·鲁尼舍夫

谢尔盖·尤里耶维奇·比比科夫

纳塔利娅·博里索夫娜·波利亚科娃

罗曼·维克托罗维奇·安德烈夫

亚历山大·阿列克谢耶维奇·斯米尔诺夫

阿列克谢·弗拉基米罗维奇·阿斯塔什金

阿纳托利·伊萨科维奇·苏茨克费尔

亚历山大·阿纳托列维奇·科西钦

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.)

OTKRYTOE AKCIONERNOE OBSCHESTVO AVIACIONNAYA HOLDINGOVAYA KOMPANIYA SUHOI

Original Assignee

OTKRYTOE AKCIONERNOE OBSCHESTVO AVIACIONNAYA HOLDINGOVAYA KOMPANIYA SUHOI

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.)

2011-04-29

Filing date

2012-04-28

Publication date

2016-10-26

2012-04-28 Application filed by OTKRYTOE AKCIONERNOE OBSCHESTVO AVIACIONNAYA HOLDINGOVAYA KOMPANIYA SUHOI filed Critical OTKRYTOE AKCIONERNOE OBSCHESTVO AVIACIONNAYA HOLDINGOVAYA KOMPANIYA SUHOI

2014-05-14 Publication of CN103797229A publication Critical patent/CN103797229A/zh

2016-10-26 Application granted granted Critical

2016-10-26 Publication of CN103797229B publication Critical patent/CN103797229B/zh

Status Active legal-status Critical Current

2032-04-28 Anticipated expiration legal-status Critical

Links

Classifications

- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/057—Control or regulation
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/80—Application in supersonic vehicles excluding hypersonic vehicles or ram, scram or rocket propulsion

CN201280032672.XA 2011-04-29 2012-04-28 用于调整超音速进气道的方法 Active CN103797229B (zh)

Applications Claiming Priority (3)

Application Number	Priority Date	Filing Date	Title
RU2011116972		2011-04-29
RU2011116972/06A RU2460892C1 (ru)	2011-04-29	2011-04-29	Способ регулирования сверхзвукового воздухозаборника
PCT/RU2012/000342 WO2012148319A1 (ru)	2011-04-29	2012-04-28	Способ регулирования сверхзвукового воздухозаборника

Publications (2)

Publication Number	Publication Date
CN103797229A CN103797229A (zh)	2014-05-14
CN103797229B true CN103797229B (zh)	2016-10-26

Family

ID=46938991

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
CN201280032672.XA Active CN103797229B (zh)	2011-04-29	2012-04-28	用于调整超音速进气道的方法

Country Status (3)

Country	Link
CN (1)	CN103797229B (cn)
RU (1)	RU2460892C1 (cn)
WO (1)	WO2012148319A1 (cn)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
CN103939217B (zh) *	2014-04-18	2016-03-02	南京航空航天大学	矩形截面高超声速变几何进气道及设计方法与工作方式
RU2672825C2 (ru) *	2017-04-17	2018-11-19	Федеральное государственное бюджетное учреждение науки Институт теоретической и прикладной механики им. С.А. Христиановича Сибирского отделения Российской академии наук (ИТПМ СО РАН)	Сверхзвуковой воздухозаборник (варианты)
CN107023395B (zh) *	2017-06-07	2019-02-26	中国空气动力研究与发展中心计算空气动力研究所	一种可调喉道面积的超声速飞行器进气道及调节方法
CN114450224A (zh) *	2019-07-01	2022-05-06	张传瑞	进行更为安静的超音速飞行的空气动力学技术和方法
CN112504612A (zh) *	2020-12-29	2021-03-16	北京航天益森风洞工程技术有限公司	一种二喉道实时可调的超扩段
CN113153530A (zh) *	2021-05-28	2021-07-23	西北工业大学	一种高超声速变结构进气道机构和宽域组合动力飞行器

Citations (5)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US3250071A (en) *	1962-05-16	1966-05-10	Bristol Siddeley Engines Ltd	Ramjet engine
GB1190812A (en) *	1967-04-18	1970-05-06	British Aircraft Corp Ltd	Improvements relating to Aircraft Air Intakes
US5881758A (en) *	1996-03-28	1999-03-16	The Boeing Company	Internal compression supersonic engine inlet
CN1384794A (zh) *	1999-08-25	2002-12-11	波音公司	超音速外部加压扩压器及其设计方法
CN101029597A (zh) *	2007-03-22	2007-09-05	南京航空航天大学	定几何超声速、高超声速可调进气道

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US3589379A (en) *	1969-02-17	1971-06-29	Mc Donnell Douglas Corp	Inlet duct
DE4008956A1 (de) *	1990-03-20	1991-09-26	Messerschmitt Boelkow Blohm	Einlaufsystem fuer ueber- oder hyperschallflugzeuge
DE19651491C2 (de) *	1996-12-11	1999-04-01	Daimler Benz Aerospace Ag	Lufteinlauf für Triebwerke
RU2171211C2 (ru) *	1997-12-29	2001-07-27	Медведев Владимир Тимофеевич	Самонастраивающийся воздухозаборник
RU2343297C1 (ru) *	2007-04-24	2009-01-10	Институт теоретической и прикладной механики им. С.А. Христиановича СО РАН (ИТПМ СО РАН)	Сверхзвуковой воздухозаборник

2011
- 2011-04-29 RU RU2011116972/06A patent/RU2460892C1/ru active
2012
- 2012-04-28 WO PCT/RU2012/000342 patent/WO2012148319A1/ru active Application Filing
- 2012-04-28 CN CN201280032672.XA patent/CN103797229B/zh active Active

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US3250071A (en) *	1962-05-16	1966-05-10	Bristol Siddeley Engines Ltd	Ramjet engine
GB1190812A (en) *	1967-04-18	1970-05-06	British Aircraft Corp Ltd	Improvements relating to Aircraft Air Intakes
US5881758A (en) *	1996-03-28	1999-03-16	The Boeing Company	Internal compression supersonic engine inlet
CN1384794A (zh) *	1999-08-25	2002-12-11	波音公司	超音速外部加压扩压器及其设计方法
CN101029597A (zh) *	2007-03-22	2007-09-05	南京航空航天大学	定几何超声速、高超声速可调进气道

Also Published As

Publication number	Publication date
WO2012148319A1 (ru)	2012-11-01
RU2460892C1 (ru)	2012-09-10
CN103797229A (zh)	2014-05-14

Similar Documents

Publication	Publication Date	Title
CN103748337B (zh)	2016-08-17	可调整的超音速进气道
CN103797229B (zh)	2016-10-26	用于调整超音速进气道的方法
US5598990A (en)	1997-02-04	Supersonic vortex generator
EP0253028B1 (en)	1990-08-08	Vortex generators for inlets
EP3016859B1 (en)	2020-01-08	Propulsion system for an aerial vehicle
CN103879556B (zh)	2016-03-02	宽飞行包线变体飞行器
EP2121436B1 (en)	2016-11-09	Vortex generator for flush air inlets performance improvement
US9587585B1 (en)	2017-03-07	Augmented propulsion system with boundary layer suction and wake blowing
US10907578B2 (en)	2021-02-02	Nacelle-integrated air-driven augmentor fan for increasing propulsor bypass ratio and efficiency
US20100181433A1 (en)	2010-07-22	Method for increasing the lift of aerodynamic surfaces and for reducing the drag
CN101200220A (zh)	2008-06-18	用于被动引导飞行器发动机喷嘴气流的***和方法
CN106628163B (zh)	2018-12-28	一种可实现大阻力减速和垂直起降的超音速无人战斗机
US20120292440A1 (en)	2012-11-22	Mass flow increase at takeoff in supersonic airliner
CN101798961A (zh)	2010-08-11	两级斜切的超声速进气唇口
CN107191272A (zh)	2017-09-22	一种矩形高超声速进气道的内通道型面设计方法
CN106321246B (zh)	2020-06-26	进气道流动限制器
US4979699A (en)	1990-12-25	Flight control augmentation inlet device
RU2670664C9 (ru)	2018-11-06	Асимметричный воздухозаборник для трехконтурного двигателя сверхзвукового самолета
CN104608919A (zh)	2015-05-13	一种有引流槽的前缘缝翼及引流槽的设计方法
CN203740126U (zh)	2014-07-30	宽飞行包线变体飞行器
US4860976A (en)	1989-08-29	Attached jet spanwise blowing lift augmentation system
US20070176052A1 (en)	2007-08-02	Air inlet for a turbofan engine
US20110240804A1 (en)	2011-10-06	Integrated aircraft
CN112780413B (zh)	2022-07-19	基于曲面百叶窗原理的tbcc进气道调节机构设计方法
CN112796888B (zh)	2022-09-23	一种基于百叶窗原理的tbcc进气道调节机构设计方法

Legal Events

Date	Code	Title
2014-05-14	C06	Publication
2014-05-14	PB01	Publication
2014-06-11	C10	Entry into substantive examination
2014-06-11	SE01	Entry into force of request for substantive examination
2016-10-26	C14	Grant of patent or utility model
2016-10-26	GR01	Patent grant