GB363382A - Improvements in or relating to exhaust pipe systems for two-stroke internal combustion engines - Google Patents

Improvements in or relating to exhaust pipe systems for two-stroke internal combustion engines

Info

Publication number
GB363382A
GB363382A GB24252/30A GB2425230A GB363382A GB 363382 A GB363382 A GB 363382A GB 24252/30 A GB24252/30 A GB 24252/30A GB 2425230 A GB2425230 A GB 2425230A GB 363382 A GB363382 A GB 363382A
Authority
GB
United Kingdom
Prior art keywords
exhaust pipe
relating
internal combustion
combustion engines
stroke internal
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.)
Expired
Application number
GB24252/30A
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.)
Siemens and Halske AG
Siemens AG
Original Assignee
Siemens and Halske AG
Siemens AG
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 Siemens and Halske AG, Siemens AG filed Critical Siemens and Halske AG
Publication of GB363382A publication Critical patent/GB363382A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N13/00—Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00
    • F01N13/08—Other arrangements or adaptations of exhaust conduits
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N13/00—Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00
    • F01N13/08—Other arrangements or adaptations of exhaust conduits
    • F01N13/082—Other arrangements or adaptations of exhaust conduits of tailpipe, e.g. with means for mixing air with exhaust for exhaust cooling, dilution or evacuation

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Retarders (AREA)
  • Exhaust Silencers (AREA)

Abstract

363,382. Aircraft engine accessories. SIEMENS & HALSKE AKT.-GES., Siemensstadt, Berlin. Aug. 13, 1930, No. 24252. Convention date, Aug. 30, 1929. [Class 4.] A two - stroke aircraft engine mounted in a wing 30 has air admission ports 32 facing the direction of travel, and the outlet of the exhaust pipe 35 is located in the upper part of the wing.
GB24252/30A 1929-08-30 1930-08-13 Improvements in or relating to exhaust pipe systems for two-stroke internal combustion engines Expired GB363382A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE363382X 1929-08-30

Publications (1)

Publication Number Publication Date
GB363382A true GB363382A (en) 1931-12-14

Family

ID=6311043

Family Applications (1)

Application Number Title Priority Date Filing Date
GB24252/30A Expired GB363382A (en) 1929-08-30 1930-08-13 Improvements in or relating to exhaust pipe systems for two-stroke internal combustion engines

Country Status (1)

Country Link
GB (1) GB363382A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2623356A (en) * 1952-12-30 Rotary compressor
US3453824A (en) * 1967-11-20 1969-07-08 Joseph M Biesecker Exhaust system for motor bikes
US3491534A (en) * 1968-04-24 1970-01-27 Trans Dapt Of California Inc Exhaust manifold
US3516247A (en) * 1968-06-24 1970-06-23 California Tube Products Inc Collector for automobile exhaust system
US3692006A (en) * 1970-07-13 1972-09-19 Outboard Marine Corp Multi-cylinder pulse charging system
US3786890A (en) * 1971-12-20 1974-01-22 Textron Inc Snowmobile muffler and header assembly
BE1002399A3 (en) * 1987-05-21 1991-01-29 Outboard Marine Corp '' Y '' EXHAUST SYSTEM WITH EQUAL BRANCHES FOR TWO-STROKE ENGINES.

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2623356A (en) * 1952-12-30 Rotary compressor
US3453824A (en) * 1967-11-20 1969-07-08 Joseph M Biesecker Exhaust system for motor bikes
US3491534A (en) * 1968-04-24 1970-01-27 Trans Dapt Of California Inc Exhaust manifold
US3516247A (en) * 1968-06-24 1970-06-23 California Tube Products Inc Collector for automobile exhaust system
US3692006A (en) * 1970-07-13 1972-09-19 Outboard Marine Corp Multi-cylinder pulse charging system
US3786890A (en) * 1971-12-20 1974-01-22 Textron Inc Snowmobile muffler and header assembly
BE1002399A3 (en) * 1987-05-21 1991-01-29 Outboard Marine Corp '' Y '' EXHAUST SYSTEM WITH EQUAL BRANCHES FOR TWO-STROKE ENGINES.

Similar Documents

Publication Publication Date Title
GB363382A (en) Improvements in or relating to exhaust pipe systems for two-stroke internal combustion engines
GB352912A (en)
GB652671A (en) Improvements in or relating to carburettors for internal combustion engines
GB337248A (en) Improvements in two-stroke cycle internal combustion engines
GB291086A (en) Improvements in or relating to two stroke internal combustion engines
GB382151A (en) Improvements in or relating to exhaust gas turbo-blower aggregates for internal combustion engines
GB424469A (en) Improvements relating to exhaust systems of internalcombustion engines
GB421648A (en) Improvements in and relating to exhaust silencers for internal combustion engines
GB298624A (en) Improvements in or relating to two-stroke internal combustion engines
GB450396A (en) Improvements in or relating to two-stroke internal combustion engines
GB298128A (en) Improvements in and relating to the charging and scavenging of four stroke internal combustion engines
GB530746A (en) Improvements in or relating to internal combustion engines comprising five or seven cylinders being charged by means of exhaust gas turbo-blowers
GB375668A (en) Improvements in or relating to exhaust manifolds for two-stroke radial engines
GB722149A (en) Improvements in or relating to combustion chambers of internal combustion engines
GB363462A (en) Improvements in or relating to the arrangement and disposition of the cylinder head covers and the admission conduits of the cylinders of internal-combustion engines
GB443769A (en) Improvements in exhaust gas purifiers for internal combustion engines
FR1089292A (en) Improved structure of an intake duct associated with the combustion chamber of an internal combustion engine with intake air turbulence
GB531864A (en) Improvements in and relating to the utilisation of the exhaust gases of internal combustion aircraft engines
GB266772A (en) Improvements in internal combustion engines
GB288646A (en) Improvements in means for controlling internal combustion engines
GB205519A (en) Improvements in or relating to internal combustion engine installations in ships
GB287996A (en) Process of preparing charges for combustion in internal combustion engines
GB374789A (en) Improvements in or relating to the cylinders of two-stroke internal combustion engines
GB273143A (en) Improvements in scavenging ports for the cylinders of internal combustion engines
GB348874A (en) Improvements in two-stroke cycle air-cooled aircraft motors