JPS55119907A - Engine exhaust promoter - Google Patents

Engine exhaust promoter

Info

Publication number
JPS55119907A
JPS55119907A JP2781079A JP2781079A JPS55119907A JP S55119907 A JPS55119907 A JP S55119907A JP 2781079 A JP2781079 A JP 2781079A JP 2781079 A JP2781079 A JP 2781079A JP S55119907 A JPS55119907 A JP S55119907A
Authority
JP
Japan
Prior art keywords
exhaust
tubular section
tubular
exhaust gas
enlarged
Prior art date
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.)
Pending
Application number
JP2781079A
Other languages
Japanese (ja)
Inventor
Hirokuni Michikawa
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.)
Individual
Original Assignee
Individual
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.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to JP2781079A priority Critical patent/JPS55119907A/en
Publication of JPS55119907A publication Critical patent/JPS55119907A/en
Pending legal-status Critical Current

Links

Landscapes

  • Exhaust Silencers (AREA)

Abstract

PURPOSE: To save the fuel cost and to improve the output, by containing a plurality of thin plate screw blades circumferentially on a tubular member connectable to the end of engine exhaust tube to guide the exhaust gas spirally thereby providing slewing force to the exhaust gas and improving the exhaust performance.
CONSTITUTION: Tubular member 1 to be fixed at the end of engine exhaust tube 6 through screw metal 7 is comprised of first tubular section 1A gradually enlarged in the direction of exhaust flow along the axis, second tubular section 1B continuing to max. diameter end and gradually reduced in the direction of exhaust flow, and tubular section 1C abruptly enlarged from min. diameter end. Then a plurality of thin plate screw blades 2... for guiding the exhaust gas spirally are fixed on inner circumferential face in the range between tubular sections 1A, 1B. Screw blade 2 is provided with smoothly curved tongue 2a and tongue 2c sharply inclined against enlarged tubular section 1C.
COPYRIGHT: (C)1980,JPO&Japio
JP2781079A 1979-03-08 1979-03-08 Engine exhaust promoter Pending JPS55119907A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2781079A JPS55119907A (en) 1979-03-08 1979-03-08 Engine exhaust promoter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2781079A JPS55119907A (en) 1979-03-08 1979-03-08 Engine exhaust promoter

Publications (1)

Publication Number Publication Date
JPS55119907A true JPS55119907A (en) 1980-09-16

Family

ID=12231324

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2781079A Pending JPS55119907A (en) 1979-03-08 1979-03-08 Engine exhaust promoter

Country Status (1)

Country Link
JP (1) JPS55119907A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20000000328A (en) * 1999-10-12 2000-01-15 임인권 Soot-Particle Reduction Method with The Application of Turbo-Machine and Soot-Particle Reduction Device Using The Same
US6543221B1 (en) * 1998-08-26 2003-04-08 Zeuna-Staerker Gmbh & Co. Kg Device for stabilizing the flow in the exhaust line of an internal combustion engine
DE102006037978A1 (en) * 2006-08-14 2008-02-21 Webasto Ag End piece for an exhaust pipe
KR101955272B1 (en) * 2018-06-26 2019-03-08 김동업 Automobile Exhaust Control Device with Streamlined Twisting Wings

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6543221B1 (en) * 1998-08-26 2003-04-08 Zeuna-Staerker Gmbh & Co. Kg Device for stabilizing the flow in the exhaust line of an internal combustion engine
KR20000000328A (en) * 1999-10-12 2000-01-15 임인권 Soot-Particle Reduction Method with The Application of Turbo-Machine and Soot-Particle Reduction Device Using The Same
DE102006037978A1 (en) * 2006-08-14 2008-02-21 Webasto Ag End piece for an exhaust pipe
DE102006037978B4 (en) * 2006-08-14 2010-04-22 Webasto Ag End piece for an exhaust pipe
KR101955272B1 (en) * 2018-06-26 2019-03-08 김동업 Automobile Exhaust Control Device with Streamlined Twisting Wings

Similar Documents

Publication Publication Date Title
JPS5472507A (en) Axial flow fan with supplementary blades
JPS5472317A (en) Exhaust bypass apparatus for turbo-charger
GB1515496A (en) Oxygen sensor having protective hood around solid electrolyte tube
JPS55101728A (en) Structure of vane disposed at downstream side of waste gate valve in turbocharger
JPS55119907A (en) Engine exhaust promoter
GB744196A (en) Improvements in or relating to silencing means
FR2637017A1 (en) NOZZLE STRUCTURE FOR TURBO-STATO-FUSEE COMBINED PROPELLER
SE8306392D0 (en) EXTENDED RING CHANNEL, SPECIAL FOR HIGH POWER GAS TURBINES
JPS558802A (en) Cavity-type fluid reflective dispersion apparatus having groove on outer circumference
JPS57168099A (en) Muffler for jet fan
CA2281385A1 (en) Guiding mechanism for variable geometry vectoring nozzles
ATE80842T1 (en) DEVICE FOR COLLECTING THE EXHAUST GAS OF A JET ENGINE.
JPS60142009A (en) Exhaust device of two-cycle engine
JPS5527502A (en) Fluid power transmission apparatus
GB2007303A (en) By-pass gas turbine engine exhaust gas mixer
JPS55125311A (en) Exhaust pipe for four-stroke engine
JPS57176400A (en) Axial flow compressor
JPS55160116A (en) Exhaust gas controller for automobile
JPS54158505A (en) Internal combustion engine
JPS54102416A (en) Lead-out port construction for exhaust gas in return- flow system of exhaust gas
JPS54129222A (en) Catalytic exhaust gas purifier
JPS55161999A (en) Diffuser with variable vane
FR3135746B1 (en) PROPULSIVE ASSEMBLY FOR AN AIRCRAFT
JPS57105526A (en) Coupling shaft for use in gas turbine
GB757702A (en) Ducting particularly for turbine outlets