GB546402A - Improvements relating to the exhaust manifolds of aircraft and other engines - Google Patents

Improvements relating to the exhaust manifolds of aircraft and other engines

Info

Publication number
GB546402A
GB546402A GB1159241A GB1159241A GB546402A GB 546402 A GB546402 A GB 546402A GB 1159241 A GB1159241 A GB 1159241A GB 1159241 A GB1159241 A GB 1159241A GB 546402 A GB546402 A GB 546402A
Authority
GB
United Kingdom
Prior art keywords
aircraft
engines
improvements relating
exhaust manifolds
manifold
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
GB1159241A
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 GB1159241A priority Critical patent/GB546402A/en
Publication of GB546402A publication Critical patent/GB546402A/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
    • F01N13/18—Construction facilitating manufacture, assembly, or disassembly
    • F01N13/1805—Fixing exhaust manifolds, exhaust pipes or pipe sections to each other, to engine or to vehicle body
    • F01N13/1811—Fixing exhaust manifolds, exhaust pipes or pipe sections to each other, to engine or to vehicle body with means permitting relative movement, e.g. compensation of thermal expansion or vibration
    • 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
    • F01N2260/00—Exhaust treating devices having provisions not otherwise provided for
    • F01N2260/10—Exhaust treating devices having provisions not otherwise provided for for avoiding stress caused by expansions or contractions due to temperature variations

Abstract

546,402. Exhaust pipes, BARCLAY, L. J. Sept. 10, 1941, No. 11592. [Class 7 (ii)] An expansion joint in the exhaust manifold of an engine for aircraft in particular is formed by a pair of sleeves D, E which are spaced apart to receive the end B of the manifold. The sleeves are preferably welded to the end A of the manifold.
GB1159241A 1941-09-10 1941-09-10 Improvements relating to the exhaust manifolds of aircraft and other engines Expired GB546402A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1159241A GB546402A (en) 1941-09-10 1941-09-10 Improvements relating to the exhaust manifolds of aircraft and other engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1159241A GB546402A (en) 1941-09-10 1941-09-10 Improvements relating to the exhaust manifolds of aircraft and other engines

Publications (1)

Publication Number Publication Date
GB546402A true GB546402A (en) 1942-07-10

Family

ID=9989067

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1159241A Expired GB546402A (en) 1941-09-10 1941-09-10 Improvements relating to the exhaust manifolds of aircraft and other engines

Country Status (1)

Country Link
GB (1) GB546402A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2174755A (en) * 1985-04-29 1986-11-12 Teledyne Ind Exhaust manifold for opposed cylinder ic engines
DE102014100472A1 (en) * 2014-01-16 2015-07-16 Eberspächer Exhaust Technology GmbH & Co. KG COMPONENTS OF DIFFERENT MATERIALS MADE OF ASSEMBLY OF EXHAUST SYSTEM WITH IMPROVED DURABILITY

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2174755A (en) * 1985-04-29 1986-11-12 Teledyne Ind Exhaust manifold for opposed cylinder ic engines
DE102014100472A1 (en) * 2014-01-16 2015-07-16 Eberspächer Exhaust Technology GmbH & Co. KG COMPONENTS OF DIFFERENT MATERIALS MADE OF ASSEMBLY OF EXHAUST SYSTEM WITH IMPROVED DURABILITY

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