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GB440286A - Improvements in exhaust driven accessories for internal combustion engines - Google Patents

Improvements in exhaust driven accessories for internal combustion engines

Info

Publication number
GB440286A
GB440286A GB27369/34A GB2736934A GB440286A GB 440286 A GB440286 A GB 440286A GB 27369/34 A GB27369/34 A GB 27369/34A GB 2736934 A GB2736934 A GB 2736934A GB 440286 A GB440286 A GB 440286A
Authority
GB
United Kingdom
Prior art keywords
nozzles
obturators
exhaust
internal combustion
combustion engines
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
GB27369/34A
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 GB27369/34A priority Critical patent/GB440286A/en
Publication of GB440286A publication Critical patent/GB440286A/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
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/141—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12—Control of the pumps
    • F02B37/22—Control of the pumps by varying cross-section of exhaust passages or air passages, e.g. by throttling turbine inlets or outlets or by varying effective number of guide conduits
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Supercharger (AREA)

Abstract

440,286. Elastic - fluid turbines. ELLOR, J. E., Grandell, South Drive, Chain Lane, Mickleover, Derby. Sept. 24, 1934, No. 27369. [Class 110 (iii)] The effective area of the nozzles of a turbine driven by the exhaust from a reciprocating internal-combustion engine is increased after the high initial pressure stage has passed in order to allow the gases to be evacuated without back pressure during the subsequent stages of exhaust. The increase is effected by the withdrawal of obturators d<1> from the nozzles d3. The obturators are withdrawn against the pressure of springs d<4> by a cam actuated linkage f<1>, f<2>, f3. With a six cylinder engine four nozzles in 'each half of the turbine casing are connected to the manifold of three cylinders. Three of the four nozzles are provided with obturators which are worked in unison by the linkage.
GB27369/34A 1934-09-24 1934-09-24 Improvements in exhaust driven accessories for internal combustion engines Expired GB440286A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB27369/34A GB440286A (en) 1934-09-24 1934-09-24 Improvements in exhaust driven accessories for internal combustion engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB27369/34A GB440286A (en) 1934-09-24 1934-09-24 Improvements in exhaust driven accessories for internal combustion engines

Publications (1)

Publication Number Publication Date
GB440286A true GB440286A (en) 1935-12-24

Family

ID=10258492

Family Applications (1)

Application Number Title Priority Date Filing Date
GB27369/34A Expired GB440286A (en) 1934-09-24 1934-09-24 Improvements in exhaust driven accessories for internal combustion engines

Country Status (1)

Country Link
GB (1) GB440286A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5058536A (en) * 1987-01-28 1991-10-22 Johnston Richard P Variable-cycle reciprocating internal combustion engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5058536A (en) * 1987-01-28 1991-10-22 Johnston Richard P Variable-cycle reciprocating internal combustion engine

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