GB502317A - Improvements in or relating to the exhaust systems of the internal combustion engines on aircraft - Google Patents

Improvements in or relating to the exhaust systems of the internal combustion engines on aircraft

Info

Publication number
GB502317A
GB502317A GB19548/38A GB1954838A GB502317A GB 502317 A GB502317 A GB 502317A GB 19548/38 A GB19548/38 A GB 19548/38A GB 1954838 A GB1954838 A GB 1954838A GB 502317 A GB502317 A GB 502317A
Authority
GB
United Kingdom
Prior art keywords
exhaust
tubes
aircraft
relating
exhaust systems
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
GB19548/38A
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.)
HUGO SCHNEEBELL
Original Assignee
HUGO SCHNEEBELL
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 HUGO SCHNEEBELL filed Critical HUGO SCHNEEBELL
Publication of GB502317A publication Critical patent/GB502317A/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
    • F01N3/00—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
    • F01N3/06—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for extinguishing sparks

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Exhaust Gas After Treatment (AREA)

Abstract

502,317. Exhaust systems for aircraft engines. SCHNEEBELI, H. July 1, 1938, No. 19548. Convention date, July 2, 1937. [Class 7 (ii)] [Also in Group XXXIII] Exhaust gas passes through a hollow engine cowling formed by walls 2, 3, separated by perforated tubes 6 through which the exhaust is ejected by air passing up the tubes. To facilitate dismantling and replacement the cowling may be made in separate sections corresponding to the exhaust pipes I leading from the cylinders. The air is deflected by a perforated plate 9 into the tubes 6 which have their ends flanged over the walls 2, 3.
GB19548/38A 1937-07-02 1938-07-01 Improvements in or relating to the exhaust systems of the internal combustion engines on aircraft Expired GB502317A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR502317X 1937-07-02

Publications (1)

Publication Number Publication Date
GB502317A true GB502317A (en) 1939-03-15

Family

ID=8906277

Family Applications (1)

Application Number Title Priority Date Filing Date
GB19548/38A Expired GB502317A (en) 1937-07-02 1938-07-01 Improvements in or relating to the exhaust systems of the internal combustion engines on aircraft

Country Status (1)

Country Link
GB (1) GB502317A (en)

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