BR8800851A - Sistema de motor de propulsao para aeronave - Google Patents
Sistema de motor de propulsao para aeronaveInfo
- Publication number
- BR8800851A BR8800851A BR8800851A BR8800851A BR8800851A BR 8800851 A BR8800851 A BR 8800851A BR 8800851 A BR8800851 A BR 8800851A BR 8800851 A BR8800851 A BR 8800851A BR 8800851 A BR8800851 A BR 8800851A
- Authority
- BR
- Brazil
- Prior art keywords
- engine
- aircraft
- engine system
- aircraft engine
- engine engine
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
- F02B37/001—Engines characterised by provision of pumps driven at least for part of the time by exhaust using exhaust drives arranged in parallel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
- F02B37/005—Exhaust driven pumps being combined with an exhaust driven auxiliary apparatus, e.g. a ventilator
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
- F02B37/04—Engines with exhaust drive and other drive of pumps, e.g. with exhaust-driven pump and mechanically-driven second pump
- F02B37/10—Engines with exhaust drive and other drive of pumps, e.g. with exhaust-driven pump and mechanically-driven second pump at least one pump being alternatively or simultaneously driven by exhaust and other drive, e.g. by pressurised fluid from a reservoir or an engine-driven pump
- F02B37/105—Engines with exhaust drive and other drive of pumps, e.g. with exhaust-driven pump and mechanically-driven second pump at least one pump being alternatively or simultaneously driven by exhaust and other drive, e.g. by pressurised fluid from a reservoir or an engine-driven pump exhaust drive and pump being both connected through gearing to engine-driven shaft
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B39/00—Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
- F02B39/02—Drives of pumps; Varying pump drive gear ratio
- F02B39/12—Drives characterised by use of couplings or clutches therein
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B41/00—Engines characterised by special means for improving conversion of heat or pressure energy into mechanical power
- F02B41/02—Engines with prolonged expansion
- F02B41/06—Engines with prolonged expansion in compound cylinders
-
- 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
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
- F02C6/10—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output supplying working fluid to a user, e.g. a chemical process, which returns working fluid to a turbine of the plant
- F02C6/12—Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K5/00—Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan
- F02K5/02—Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan the engine being of the reciprocating-piston type
-
- 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
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
-
- 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
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Supercharger (AREA)
- Ink Jet Recording Methods And Recording Media Thereof (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US07/017,825 US4815282A (en) | 1987-02-24 | 1987-02-24 | Turbocharged compund cycle ducted fan engine system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BR8800851A true BR8800851A (pt) | 1988-10-04 |
Family
ID=21784744
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BR8800851A BR8800851A (pt) | 1987-02-24 | 1988-02-24 | Sistema de motor de propulsao para aeronave |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US4815282A (pt) |
| JP (1) | JPS63227929A (pt) |
| AU (1) | AU1201888A (pt) |
| BR (1) | BR8800851A (pt) |
| DE (1) | DE3804906A1 (pt) |
| FR (1) | FR2611229A1 (pt) |
| GB (1) | GB2201467A (pt) |
Families Citing this family (66)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB8927785D0 (en) * | 1989-12-08 | 1990-05-30 | Westland Helicopters | Helicopters |
| CA2093683C (en) * | 1992-05-14 | 2002-10-15 | William Miller Farrell | Intercooled gas turbine engine |
| DE4237910C2 (de) * | 1992-11-10 | 1997-01-16 | Gerhard Ittner | Strahltriebwerk mit einem Verdichterantrieb, insbesondere Verbrennungsmotor und einer Kaltluftdosierturbine |
| US5471834A (en) * | 1994-02-14 | 1995-12-05 | Kapich; Davorin | Engine driven propulsion fan with turbochargers in series |
| RU2213876C2 (ru) * | 2001-01-25 | 2003-10-10 | Федеральное государственное унитарное предприятие "Московское машиностроительное производственное предприятие "Салют" | Трехконтурный турбореактивный двигатель |
| GB2379483A (en) * | 2001-09-08 | 2003-03-12 | Rolls Royce Plc | Augmented gas turbine propulsion system |
| EP1597463A1 (de) * | 2003-02-11 | 2005-11-23 | Uwe Borchert | Verfahren zur herstellung von gasturbinen und gasturbinenanordnung |
| WO2004074654A1 (en) * | 2003-02-24 | 2004-09-02 | Pratt & Whitney Canada Corp. | Integral cooling system for rotary engine |
| JP2006518822A (ja) * | 2003-02-24 | 2006-08-17 | プラット アンド ホイットニー カナダ コーポレイション | 低容積圧縮率の統合されたターボ複合ロータリエンジン |
| RU2266419C2 (ru) * | 2004-02-02 | 2005-12-20 | Григорчук Владимир Степанович | Воздушно-реактивный дизельный двигатель |
| US7353647B2 (en) * | 2004-05-13 | 2008-04-08 | General Electric Company | Methods and apparatus for assembling gas turbine engines |
| RU2294445C2 (ru) * | 2004-08-18 | 2007-02-27 | Открытое Акционерное Общество Центральная Компания Финансово-Промышленной Группы "Российский Авиационный Консорциум" | Двухконтурный реактивный двигатель |
| RU2315191C1 (ru) * | 2006-05-24 | 2008-01-20 | Владимир Степанович Григорчук | Газотурбинный двигатель |
| DE102007022042A1 (de) * | 2007-05-08 | 2008-11-13 | Voith Patent Gmbh | Antriebsstrang, insbesondere für Kraftfahrzeuge |
| US8015795B2 (en) * | 2007-05-18 | 2011-09-13 | United Technologies Corporation | Aircraft combination engines plural airflow conveyances system |
| US7836680B2 (en) * | 2007-06-20 | 2010-11-23 | United Technologies Corporation | Aircraft combination engines thermal management system |
| US9467021B2 (en) | 2010-02-16 | 2016-10-11 | Sine Waves, Inc. | Engine and induction generator |
| US8695565B2 (en) * | 2010-02-16 | 2014-04-15 | Sine Waves, Inc. | Co-axial rotary engine |
| RU2446304C2 (ru) * | 2010-04-15 | 2012-03-27 | Евгений Васильевич Лаптев | Комбинированный воздушно-реактивный двигатель |
| RU2433292C1 (ru) * | 2010-04-29 | 2011-11-10 | Евгений Петрович Голубков | Авиационный бесшатунно-вентиляторный двигатель |
| US9512721B2 (en) | 2012-07-20 | 2016-12-06 | Pratt & Whitney Canada Corp. | Compound cycle engine |
| US9926843B2 (en) * | 2012-07-20 | 2018-03-27 | Pratt & Whitney Canada Corp. | Compound cycle engine |
| US10107195B2 (en) | 2012-07-20 | 2018-10-23 | Pratt & Whitney Canada Corp. | Compound cycle engine |
| US9194232B2 (en) | 2012-07-20 | 2015-11-24 | Pratt & Whitney Canada Corp. | Compound cycle engine |
| US20140144136A1 (en) * | 2012-11-28 | 2014-05-29 | Spicer Off-Highway Belgium N.V. | System and method for waste heat recovery for internal combustion engines |
| US20160047305A1 (en) * | 2014-08-15 | 2016-02-18 | General Electric Company | Multi-stage axial compressor arrangement |
| US9932892B2 (en) | 2015-02-20 | 2018-04-03 | Pratt & Whitney Canada Corp. | Compound engine assembly with coaxial compressor and offset turbine section |
| US20160245162A1 (en) | 2015-02-20 | 2016-08-25 | Pratt & Whitney Canada Corp. | Compound engine assembly with offset turbine shaft, engine shaft and inlet duct |
| US9896998B2 (en) * | 2015-02-20 | 2018-02-20 | Pratt & Whitney Canada Corp. | Compound engine assembly with modulated flow |
| US10408123B2 (en) | 2015-02-20 | 2019-09-10 | Pratt & Whitney Canada Corp. | Engine assembly with modular compressor and turbine |
| US10533500B2 (en) | 2015-02-20 | 2020-01-14 | Pratt & Whitney Canada Corp. | Compound engine assembly with mount cage |
| US10371060B2 (en) | 2015-02-20 | 2019-08-06 | Pratt & Whitney Canada Corp. | Compound engine assembly with confined fire zone |
| US9869240B2 (en) * | 2015-02-20 | 2018-01-16 | Pratt & Whitney Canada Corp. | Compound engine assembly with cantilevered compressor and turbine |
| US9879591B2 (en) | 2015-02-20 | 2018-01-30 | Pratt & Whitney Canada Corp. | Engine intake assembly with selector valve |
| US10533492B2 (en) * | 2015-02-20 | 2020-01-14 | Pratt & Whitney Canada Corp. | Compound engine assembly with mount cage |
| US9797297B2 (en) * | 2015-02-20 | 2017-10-24 | Pratt & Whitney Canada Corp. | Compound engine assembly with common inlet |
| US10428734B2 (en) | 2015-02-20 | 2019-10-01 | Pratt & Whitney Canada Corp. | Compound engine assembly with inlet lip anti-icing |
| US10662903B2 (en) * | 2015-02-27 | 2020-05-26 | Avl Powertrain Engineering, Inc. | Waste heat recovery and boost systems including variable drive mechanisms |
| CA2933112C (en) * | 2015-06-16 | 2023-09-26 | Pratt & Whitney Canada Corp. | Compound cycle engine |
| US9759128B2 (en) | 2015-06-16 | 2017-09-12 | Pratt & Whitney Canada Corp. | Compound engine assembly with exhaust pipe nozzle |
| US10696417B2 (en) * | 2015-06-25 | 2020-06-30 | Pratt & Whitney Canada Corp. | Auxiliary power unit with excess air recovery |
| US9771165B2 (en) | 2015-06-25 | 2017-09-26 | Pratt & Whitney Canada Corp. | Compound engine assembly with direct drive of generator |
| US10590842B2 (en) * | 2015-06-25 | 2020-03-17 | Pratt & Whitney Canada Corp. | Compound engine assembly with bleed air |
| US10710738B2 (en) * | 2015-06-25 | 2020-07-14 | Pratt & Whitney Canada Corp. | Auxiliary power unit with intercooler |
| US11214381B2 (en) * | 2015-08-07 | 2022-01-04 | Pratt & Whitney Canada Corp. | Aircraft heating assembly with liquid cooled internal combustion engine and heating element using waste heat |
| US10253726B2 (en) | 2015-08-07 | 2019-04-09 | Pratt & Whitney Canada Corp. | Engine assembly with combined engine and cooling exhaust |
| US10240521B2 (en) * | 2015-08-07 | 2019-03-26 | Pratt & Whitney Canada Corp. | Auxiliary power unit with variable speed ratio |
| US10267191B2 (en) | 2015-08-07 | 2019-04-23 | Pratt & Whitney Canada Corp. | Turboprop engine assembly with combined engine and cooling exhaust |
| US10240522B2 (en) | 2015-08-07 | 2019-03-26 | Pratt & Whitney Canada Corp. | Auxiliary power unit with combined cooling of generator |
| RU168499U1 (ru) * | 2016-06-23 | 2017-02-07 | Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" | Выносной вентиляторный модуль авиационной силовой установки |
| US10883424B2 (en) | 2016-07-19 | 2021-01-05 | Pratt & Whitney Canada Corp. | Multi-spool gas turbine engine architecture |
| WO2018044757A1 (en) * | 2016-08-29 | 2018-03-08 | BINGHAM, Robert A. | Multi-hybrid aircraft engine |
| US11035293B2 (en) | 2016-09-15 | 2021-06-15 | Pratt & Whitney Canada Corp. | Reverse flow gas turbine engine with offset RGB |
| US10450952B2 (en) * | 2017-01-16 | 2019-10-22 | Pratt & Whitney Canada Corp. | Turbofan engine assembly with gearbox |
| US10634049B2 (en) | 2017-01-16 | 2020-04-28 | Pratt & Whitney Canada Corp. | Turbofan engine assembly with intercooler |
| US10738709B2 (en) | 2017-02-09 | 2020-08-11 | Pratt & Whitney Canada Corp. | Multi-spool gas turbine engine |
| US10808624B2 (en) | 2017-02-09 | 2020-10-20 | Pratt & Whitney Canada Corp. | Turbine rotor with low over-speed requirements |
| US10215052B2 (en) | 2017-03-14 | 2019-02-26 | Pratt & Whitney Canada Corp. | Inter-shaft bearing arrangement |
| US10746188B2 (en) | 2017-03-14 | 2020-08-18 | Pratt & Whitney Canada Corp. | Inter-shaft bearing connected to a compressor boost system |
| US10822100B2 (en) * | 2017-06-26 | 2020-11-03 | General Electric Company | Hybrid electric propulsion system for an aircraft |
| US10527012B2 (en) * | 2017-06-29 | 2020-01-07 | Pratt & Whitney Canada Corp. | Engine assembly with engine and cooler compartments |
| CN108119257B (zh) * | 2017-09-08 | 2020-06-23 | 邹国泉 | 亚音速内燃航空发动机 |
| US11732639B2 (en) * | 2019-03-01 | 2023-08-22 | Pratt & Whitney Canada Corp. | Mechanical disconnects for parallel power lanes in hybrid electric propulsion systems |
| US11827370B1 (en) * | 2022-06-21 | 2023-11-28 | Pratt & Whitney Canada Corp. | Aircraft propulsion system with intermittent combustion engine and electric transmission system and method for operating the same |
| US11891947B2 (en) * | 2022-06-23 | 2024-02-06 | Pratt & Whitney Canada Corp. | Aircraft engine, gas turbine intake therefore, and method of guiding exhaust gasses |
| US11933218B2 (en) * | 2022-07-22 | 2024-03-19 | Rtx Corporation | System with multiple forced induction engines |
Family Cites Families (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB596819A (en) * | 1945-07-18 | 1948-01-12 | Napier & Son Ltd | Improvements in or relating to internal combustion engine power plants |
| GB437078A (en) * | 1934-01-24 | 1935-10-23 | Alfred Buechi | Improvements in or relating to arrangements of exhaust driven superchargers with multiple row internal combustion engines |
| US2385366A (en) * | 1938-04-19 | 1945-09-25 | Jarvis C Marble | Power plant for aircraft |
| US2356557A (en) * | 1939-12-19 | 1944-08-22 | Anxionnaz Rene | Reaction propelling device with supercharged engine |
| US2397816A (en) * | 1942-02-09 | 1946-04-02 | Ford Motor Co | Exhaust turbosupercharger |
| US2465099A (en) * | 1943-11-20 | 1949-03-22 | Allis Chalmers Mfg Co | Propulsion means comprising an internal-combustion engine and a propulsive jet |
| US2585968A (en) * | 1944-02-21 | 1952-02-19 | Schneider Brothers Company | Turbosupercharged internal-combustion engine having hydraulic means to connect turbine to engine output shaft at high load |
| GB599974A (en) * | 1944-12-30 | 1948-03-25 | Sigma | Installation for propulsion by reaction, notably for aircraft |
| US2580591A (en) * | 1944-12-30 | 1952-01-01 | Gen Mechanique Appliquee Soc I | Jet engine having a plurality of turbocompressors operable in parallel or in series |
| FR916985A (fr) * | 1945-07-05 | 1946-12-20 | Perfectionnements aux moteurs et motopropulseurs complexes à combustion interne | |
| GB690272A (en) * | 1946-04-02 | 1953-04-15 | Rateau Soc | Improvements in or relating to jet propulsion plants |
| US2468157A (en) * | 1946-09-24 | 1949-04-26 | Napier & Son Ltd | Internal-combustion engine power plant |
| GB651365A (en) * | 1947-09-23 | 1951-03-14 | Sigma | Improvements in power gas plants, in particular for use on flying machines |
| GB718100A (en) * | 1951-05-17 | 1954-11-10 | Napier & Son Ltd | Improvements in or relating to compound power plants |
| GB734359A (en) * | 1952-12-01 | 1955-07-27 | Harry Robert Mayes | Improvements in internal combustion engines |
| GB866017A (en) * | 1956-11-09 | 1961-04-26 | Kloeckner Humboldt Deutz Ag | Four-stroke internal combustion engine having an exhaust gas turbo-charger |
| DE1840712U (de) * | 1958-08-22 | 1961-11-02 | Daimler Benz Ag | Aus einer kohlenbrennkraftmaschine und einem gasturbinentriebwerk bestehendes antriebsaggregat fuer fahrzeuge. |
| US3007302A (en) * | 1958-09-30 | 1961-11-07 | Continental Aviat & Eng Corp | Compound turbine-diesel power plant |
| GB919113A (en) * | 1960-03-11 | 1963-02-20 | Alexander Davidson Garden | Improvements in or relating to aircraft propulsive means |
| FR1304016A (fr) * | 1961-03-11 | 1962-09-21 | Perfectionnements apportés aux moteurs à combustion interne, suralimentés à l'aide d'une turbo-soufflante | |
| US4452043A (en) * | 1980-07-22 | 1984-06-05 | South Western Industrial Research Limited | Differential compound engine |
| JPS5754622U (pt) * | 1980-09-17 | 1982-03-30 | ||
| DE3330315A1 (de) * | 1983-08-23 | 1985-03-14 | Daimler-Benz Ag, 7000 Stuttgart | Antriebsanordnung von nebenaggregaten an einer brennkraftmaschine |
-
1987
- 1987-02-24 US US07/017,825 patent/US4815282A/en not_active Expired - Fee Related
-
1988
- 1988-02-10 GB GB08802988A patent/GB2201467A/en not_active Withdrawn
- 1988-02-17 DE DE3804906A patent/DE3804906A1/de not_active Withdrawn
- 1988-02-22 FR FR8802073A patent/FR2611229A1/fr active Pending
- 1988-02-22 AU AU12018/88A patent/AU1201888A/en not_active Abandoned
- 1988-02-24 JP JP63041827A patent/JPS63227929A/ja active Pending
- 1988-02-24 BR BR8800851A patent/BR8800851A/pt unknown
Also Published As
| Publication number | Publication date |
|---|---|
| GB8802988D0 (en) | 1988-03-09 |
| JPS63227929A (ja) | 1988-09-22 |
| FR2611229A1 (fr) | 1988-08-26 |
| GB2201467A (en) | 1988-09-01 |
| AU1201888A (en) | 1988-08-25 |
| DE3804906A1 (de) | 1988-09-01 |
| US4815282A (en) | 1989-03-28 |
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