GB261232A - Improved method of and means for withdrawing the exhaust from internal combustion engines - Google Patents

Improved method of and means for withdrawing the exhaust from internal combustion engines

Info

Publication number
GB261232A
GB261232A GB610026A GB610026A GB261232A GB 261232 A GB261232 A GB 261232A GB 610026 A GB610026 A GB 610026A GB 610026 A GB610026 A GB 610026A GB 261232 A GB261232 A GB 261232A
Authority
GB
United Kingdom
Prior art keywords
exhaust
pipe
plane
gases
outlet
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
GB610026A
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 GB610026A priority Critical patent/GB261232A/en
Publication of GB261232A publication Critical patent/GB261232A/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
    • 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)
  • Exhaust Silencers (AREA)

Abstract

261,232. Matthews, W. C. March 4, 1926. Cylinders, pipes for; exhaust, cooling; forcing apparatus for gases.-In order to withdraw exhaust gases from aeroplane or like engines by suction, the gases are led to a region behind the line of maximum camber of a cambered body. In one form, the exhaust: pipe opens directly into a hollow metal plane having outlet pcrts in the upper surface behind the camber. In a modication, Fig. 2, the exhaust manifold 1 is connected to a pipe 5 lying along the inside of the plane 3 and enclosed in an outer pipe 8, through which air current s cauised to flow by the movement of the aeroplane, in order to protect the plane from the heat of the exhaust. Small outlet pipes 7 connect the pipe 5 to ports 4 in the plane 3. In a modification, an exhaust pipe is formed as a small hollow aerofoil 11, Fig. 3, with outlet holes or slots 4<1> in the upper surface. Such aerofoils may be arranged horizontally or vertically and tapered at the end remote from the exhaust manifold.
GB610026A 1926-03-04 1926-03-04 Improved method of and means for withdrawing the exhaust from internal combustion engines Expired GB261232A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB610026A GB261232A (en) 1926-03-04 1926-03-04 Improved method of and means for withdrawing the exhaust from internal combustion engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB610026A GB261232A (en) 1926-03-04 1926-03-04 Improved method of and means for withdrawing the exhaust from internal combustion engines

Publications (1)

Publication Number Publication Date
GB261232A true GB261232A (en) 1926-11-18

Family

ID=9808366

Family Applications (1)

Application Number Title Priority Date Filing Date
GB610026A Expired GB261232A (en) 1926-03-04 1926-03-04 Improved method of and means for withdrawing the exhaust from internal combustion engines

Country Status (1)

Country Link
GB (1) GB261232A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2425630A (en) * 1942-03-25 1947-08-12 Stewart Warner Corp Internal-combustion airplane heater
US2520910A (en) * 1943-07-15 1950-09-05 Fred P Chadsey Vacuum jet manifold
US2927725A (en) * 1953-07-03 1960-03-08 Armstrong Siddeley Motors Ltd Anti-icing means for a gas turbine engine of an aircraft

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2425630A (en) * 1942-03-25 1947-08-12 Stewart Warner Corp Internal-combustion airplane heater
US2520910A (en) * 1943-07-15 1950-09-05 Fred P Chadsey Vacuum jet manifold
US2927725A (en) * 1953-07-03 1960-03-08 Armstrong Siddeley Motors Ltd Anti-icing means for a gas turbine engine of an aircraft

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