BR112019005588A2 - métodos para mitigação de ondas de choque em veículos supersônicos e para geração de empuxo supersônico, e, veículo aéreo. - Google Patents
métodos para mitigação de ondas de choque em veículos supersônicos e para geração de empuxo supersônico, e, veículo aéreo.Info
- Publication number
- BR112019005588A2 BR112019005588A2 BR112019005588A BR112019005588A BR112019005588A2 BR 112019005588 A2 BR112019005588 A2 BR 112019005588A2 BR 112019005588 A BR112019005588 A BR 112019005588A BR 112019005588 A BR112019005588 A BR 112019005588A BR 112019005588 A2 BR112019005588 A2 BR 112019005588A2
- Authority
- BR
- Brazil
- Prior art keywords
- supersonic
- shock wave
- methods
- air vehicle
- vehicles
- Prior art date
Links
- 238000000034 method Methods 0.000 title abstract 2
- 230000035939 shock Effects 0.000 title abstract 2
- 230000000116 mitigating effect Effects 0.000 title 1
- 238000004581 coalescence Methods 0.000 abstract 1
- 230000006835 compression Effects 0.000 abstract 1
- 238000007906 compression Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/04—Influencing air flow over aircraft surfaces, not otherwise provided for by generating shock waves
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/10—Shape of wings
- B64C3/16—Frontal aspect
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C30/00—Supersonic type 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
- 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
- B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
-
- 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
- B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Exhaust Silencers (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
Abstract
um método para geração de empuxo supersônico inclui a geração de uma pluma de exaustão supersônica de empuxo (522) que tem uma primeira velocidade média de um motor (500) e que expele uma pluma de exaustão de desvio (532) que tem uma segunda velocidade média do motor, a primeira velocidade média maior do que a segunda velocidade média, de modo que a pluma de exaustão de desvio iniba a coalescência de uma onda de choque de compressão da pluma de exaustão de motor (536).
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201562222074P | 2015-09-22 | 2015-09-22 | |
US15/272,908 US10618638B2 (en) | 2015-09-22 | 2016-09-22 | Shockwave mitigation system for supersonic aircraft |
US15/272,908 | 2016-09-22 | ||
PCT/US2017/053006 WO2018067329A1 (en) | 2015-09-22 | 2017-09-22 | Shockwave mitigation system for supersonic aircraft |
Publications (2)
Publication Number | Publication Date |
---|---|
BR112019005588A2 true BR112019005588A2 (pt) | 2019-06-11 |
BR112019005588B1 BR112019005588B1 (pt) | 2024-02-06 |
Family
ID=60806521
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112019005588-6A BR112019005588B1 (pt) | 2015-09-22 | 2017-09-22 | Métodos para mitigação de ondas de choque em veículos supersônicos |
Country Status (6)
Country | Link |
---|---|
US (2) | US10618638B2 (pt) |
EP (1) | EP3515813A4 (pt) |
AU (1) | AU2017339709A1 (pt) |
BR (1) | BR112019005588B1 (pt) |
CA (1) | CA3037876A1 (pt) |
WO (1) | WO2018067329A1 (pt) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10618638B2 (en) * | 2015-09-22 | 2020-04-14 | Nctar, Llc | Shockwave mitigation system for supersonic aircraft |
US20200049011A1 (en) * | 2017-08-10 | 2020-02-13 | Paul NEISER | System and method for fluid manipulation |
CN108444724B (zh) * | 2018-04-27 | 2019-10-18 | 北京空间飞行器总体设计部 | 一种导流空间受限羽流对发动机影响的综合试验方法 |
US11519333B2 (en) * | 2020-09-10 | 2022-12-06 | General Electric Company | Turbine engine with shockwave attenuation |
CN114542288B (zh) * | 2022-01-10 | 2024-04-30 | 南京航空航天大学 | 一种自适应泄流高超声速进气道 |
Family Cites Families (31)
Publication number | Priority date | Publication date | Assignee | Title |
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US2950879A (en) | 1956-01-09 | 1960-08-30 | Boeing Co | Lift modifying protuberance and airfoil combinations |
US3314629A (en) | 1964-12-07 | 1967-04-18 | Scott C Rethorst | Shockless supersonic aircraft |
US3596852A (en) * | 1968-07-19 | 1971-08-03 | George H Wakefield | Supersonic aircraft |
US3737119A (en) * | 1970-06-15 | 1973-06-05 | Research Corp | Device for sonic boom reduction and improving aircraft performance |
US3938328A (en) * | 1971-11-08 | 1976-02-17 | The Boeing Company | Multicycle engine |
US3904151A (en) * | 1973-03-16 | 1975-09-09 | Vehicle Research Corp | Supersonic upflow wing |
US4008866A (en) * | 1973-03-16 | 1977-02-22 | Vehicle Research Corporation | Compression energy transformation system for a supersonic wing |
US4168044A (en) * | 1975-06-06 | 1979-09-18 | Vehicle Research Corporation | Energy conserving supersonic aircraft |
US4598886A (en) | 1979-08-13 | 1986-07-08 | The Boeing Company | Double parasol, favorable interference airplane |
US4405102A (en) * | 1981-11-20 | 1983-09-20 | The United States Of America As Represented By The Secretary Of The Navy | Variable wing position supersonic biplane |
US5231825A (en) * | 1990-04-09 | 1993-08-03 | General Electric Company | Method for compressor air extraction |
US5358156A (en) | 1990-07-23 | 1994-10-25 | Vehicle Research Corporation | Supersonic aircraft shock wave energy recovery system |
US5251846A (en) * | 1990-07-23 | 1993-10-12 | Vehicle Research Corporation | Supersonic aircraft shock wave energy recovery system |
WO1992001602A1 (en) | 1990-07-23 | 1992-02-06 | Vehicle Research Corporation | Supersonic aircraft shock wave energy recovery system |
US5289995A (en) | 1992-12-14 | 1994-03-01 | The Boeing Company | Supersonic aircraft |
US5934607A (en) * | 1997-01-21 | 1999-08-10 | Lockheed Martin Corporation | Shock suppression supersonic aircraft |
US5842666A (en) | 1997-02-21 | 1998-12-01 | Northrop Grumman Coporation | Laminar supersonic transport aircraft |
US6178740B1 (en) * | 1999-02-25 | 2001-01-30 | The Boeing Company | Turbo fan engine nacelle exhaust system with concave primary nozzle plug |
US6588703B1 (en) | 2000-02-08 | 2003-07-08 | Lockheed Martin Corporation | Passive aerodynamic sonic boom suppression for supersonic aircraft |
AU2002227282A1 (en) | 2000-12-08 | 2002-06-18 | Lockheed Martin Corporation | Joined wing supersonic aircraft |
BR0307340B8 (pt) | 2002-01-30 | 2013-02-19 | mÉtodo para configurar e operar um aviço para minimizar os efeitos de estampido sânico bem como mÉtodo e veÍculo aeroespacial configurado para reduzir os efeitos de estampido sânico. | |
US7546977B2 (en) | 2003-07-03 | 2009-06-16 | Lockheed-Martin Corporation | Passive aerodynamic sonic boom suppression for supersonic aircraft |
FR2870513B1 (fr) | 2004-05-24 | 2006-08-11 | Airbus France Sas | Nacelle de reacteur pour avion supersonique |
US7861966B2 (en) * | 2005-04-18 | 2011-01-04 | Vehicle Research Corporation | Supersonic aircraft footprint spreading control system and method |
JP4846808B2 (ja) | 2005-12-15 | 2011-12-28 | ガルフストリーム・エアロスペース・コーポレイション | 超音速航空機のための等エントロピー圧縮インレット |
US7837142B2 (en) | 2006-10-12 | 2010-11-23 | Aerion Corporation | Supersonic aircraft jet engine |
US8393158B2 (en) | 2007-10-24 | 2013-03-12 | Gulfstream Aerospace Corporation | Low shock strength inlet |
US9884688B2 (en) | 2013-02-14 | 2018-02-06 | Gulfstream Aerospace Corporation | Propulsion system using large scale vortex generators for flow redistribution and supersonic aircraft equipped with the propulsion system |
CN103879556B (zh) * | 2014-03-31 | 2016-03-02 | 冯加伟 | 宽飞行包线变体飞行器 |
US10618638B2 (en) * | 2015-09-22 | 2020-04-14 | Nctar, Llc | Shockwave mitigation system for supersonic aircraft |
US10793266B2 (en) * | 2016-11-14 | 2020-10-06 | Boom Technology, Inc. | Commercial supersonic aircraft and associated systems and methods |
-
2016
- 2016-09-22 US US15/272,908 patent/US10618638B2/en active Active
-
2017
- 2017-09-22 WO PCT/US2017/053006 patent/WO2018067329A1/en unknown
- 2017-09-22 CA CA3037876A patent/CA3037876A1/en active Pending
- 2017-09-22 BR BR112019005588-6A patent/BR112019005588B1/pt active IP Right Grant
- 2017-09-22 EP EP17858901.6A patent/EP3515813A4/en active Pending
- 2017-09-22 AU AU2017339709A patent/AU2017339709A1/en not_active Abandoned
-
2020
- 2020-03-09 US US16/813,718 patent/US11834154B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
EP3515813A1 (en) | 2019-07-31 |
BR112019005588B1 (pt) | 2024-02-06 |
CA3037876A1 (en) | 2018-04-12 |
WO2018067329A1 (en) | 2018-04-12 |
US11834154B2 (en) | 2023-12-05 |
US20200283129A1 (en) | 2020-09-10 |
AU2017339709A1 (en) | 2019-05-09 |
US20180001996A1 (en) | 2018-01-04 |
EP3515813A4 (en) | 2020-07-15 |
US10618638B2 (en) | 2020-04-14 |
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Legal Events
Date | Code | Title | Description |
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B350 | Update of information on the portal [chapter 15.35 patent gazette] | ||
B06W | Patent application suspended after preliminary examination (for patents with searches from other patent authorities) chapter 6.23 patent gazette] | ||
B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
B16A | Patent or certificate of addition of invention granted [chapter 16.1 patent gazette] |
Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 22/09/2017, OBSERVADAS AS CONDICOES LEGAIS |