BE601814A - Improvements to internal combustion engine exhaust systems - Google Patents
Improvements to internal combustion engine exhaust systemsInfo
- Publication number
- BE601814A BE601814A BE601814A BE601814A BE601814A BE 601814 A BE601814 A BE 601814A BE 601814 A BE601814 A BE 601814A BE 601814 A BE601814 A BE 601814A BE 601814 A BE601814 A BE 601814A
- Authority
- BE
- Belgium
- Prior art keywords
- combustion engine
- internal combustion
- engine exhaust
- exhaust systems
- systems
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/78—Other construction of jet pipes
- F02K1/82—Jet pipe walls, e.g. liners
- F02K1/827—Sound absorbing structures or liners
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Exhaust Silencers (AREA)
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ZA3095696X | 1959-09-25 | ||
ZA593792 | 1960-03-25 | ||
ZA602491 | 1960-06-17 | ||
ZA604429 | 1960-10-31 |
Publications (1)
Publication Number | Publication Date |
---|---|
BE601814A true BE601814A (en) | 1961-07-17 |
Family
ID=32475720
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE601814A BE601814A (en) | 1959-09-25 | 1961-03-27 | Improvements to internal combustion engine exhaust systems |
Country Status (2)
Country | Link |
---|---|
US (1) | US3095696A (en) |
BE (1) | BE601814A (en) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3371743A (en) * | 1965-04-29 | 1968-03-05 | American Radiator & Standard | Jet exhaust silencing nozzle with suction applied at exit wall |
US3410093A (en) * | 1967-05-26 | 1968-11-12 | Ghougasian John Nazareth | Reaction thrust engine with fluid operated compressor |
US3548597A (en) * | 1968-09-16 | 1970-12-22 | Alexander Hossen Etessam | Turbine engine for aircraft having a supplementary compressor driven by a supplementary turbine |
US3575260A (en) * | 1969-05-15 | 1971-04-20 | Rohr Corp | Method and apparatus for augmenting the thrust of a jet-propelled aircraft and suppressing the noise thereof |
DE3542541A1 (en) * | 1985-12-02 | 1987-06-04 | Ingelheim Peter Graf Von | DEVICE FOR GENERATING A TOWING FORCE |
US6094907A (en) * | 1996-06-05 | 2000-08-01 | The Boeing Company | Jet engine and method for reducing jet engine noise by reducing nacelle boundary layer thickness |
US8590288B2 (en) * | 2007-03-30 | 2013-11-26 | Toyota Jidosha Kabushiki Kaisha | Fan control apparatus |
US8356469B1 (en) | 2007-04-05 | 2013-01-22 | The United States Of America As Represented By The Secretary Of The Air Force | Gas turbine engine with dual compression rotor |
GB0908595D0 (en) * | 2009-05-20 | 2009-06-24 | Rolls Royce Plc | Propfan engine |
US9057329B2 (en) * | 2012-02-22 | 2015-06-16 | Honeywell International Inc. | Turboprop engine systems with noise reducing inlet assemblies |
US10260417B2 (en) * | 2015-12-22 | 2019-04-16 | General Electric Company | Air intake turboprop assemblies |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2620624A (en) * | 1952-12-09 | wislicenus | ||
US2974744A (en) * | 1961-03-14 | Silencer | ||
US2168528A (en) * | 1934-11-08 | 1939-08-08 | Kadenacy Michel | Exhaust passage of two-stroke internal combustion engines |
NL70849C (en) * | 1945-05-14 | |||
US2800765A (en) * | 1947-08-27 | 1957-07-30 | Westinghouse Electric Corp | Movable flame holder for combustion apparatus |
US2674087A (en) * | 1948-05-13 | 1954-04-06 | Peters & Russell Inc | Exhaust deflector |
US2637166A (en) * | 1948-10-07 | 1953-05-05 | James M Carswell | Pure reaction turbine with evacuated chamber and rotor element therefor |
US2882679A (en) * | 1950-12-22 | 1959-04-21 | Gen Motors Corp | Augmenter type afterburner for jet propelled aircraft |
FR1114647A (en) * | 1954-11-19 | 1956-04-16 | Snecma | Cooling of aircraft parts and accessories exposed to high temperatures |
FR1006139A (en) * | 1954-11-25 | 1952-04-21 | Cem Comp Electro Mec | Method and device for adjusting turbo-reactors |
GB783003A (en) * | 1955-03-31 | 1957-09-18 | Power Jets Res & Dev Ltd | Apparatus for reducing the noise of a fluid stream |
US2915136A (en) * | 1956-05-28 | 1959-12-01 | Friedrich O Ringleb | Apparatus for suppressing noise |
US2892582A (en) * | 1956-08-17 | 1959-06-30 | O'rourke Neil | Simplified boundary layer control for a jet |
US2920445A (en) * | 1957-01-15 | 1960-01-12 | Curtiss Wright Corp | Flame holder apparatus |
GB838602A (en) * | 1957-03-06 | 1960-06-22 | Power Jets Res & Dev Ltd | Improvements in or relating to gas turbine plant |
FR1208542A (en) * | 1958-06-19 | 1960-02-24 | & De Construction De Moteurs D | Improvements to jet adjustment devices |
US3009318A (en) * | 1960-04-22 | 1961-11-21 | Ryan Aeronautical Co | Turbofan engine with reversible pitch fan |
-
1960
- 1960-09-19 US US57003A patent/US3095696A/en not_active Expired - Lifetime
-
1961
- 1961-03-27 BE BE601814A patent/BE601814A/en unknown
Also Published As
Publication number | Publication date |
---|---|
US3095696A (en) | 1963-07-02 |
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