GB809570A - Improved device for intermittent combustion - Google Patents

Improved device for intermittent combustion

Info

Publication number
GB809570A
GB809570A GB37843/56A GB3784356A GB809570A GB 809570 A GB809570 A GB 809570A GB 37843/56 A GB37843/56 A GB 37843/56A GB 3784356 A GB3784356 A GB 3784356A GB 809570 A GB809570 A GB 809570A
Authority
GB
United Kingdom
Prior art keywords
fuel
combustion
combustion chamber
frequency
discharge duct
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
GB37843/56A
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.)
Gustavsbergs Fabriker AB
Original Assignee
Gustavsbergs Fabriker AB
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 Gustavsbergs Fabriker AB filed Critical Gustavsbergs Fabriker AB
Publication of GB809570A publication Critical patent/GB809570A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CMETHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C15/00Apparatus in which combustion takes place in pulses influenced by acoustic resonance in a gas mass
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K7/00Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/02Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet
    • F02K7/06Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet with combustion chambers having valves

Landscapes

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

Abstract

809,570. Generating combustion products under pressure; liquid, gaseous or pulverized fuel combustion apparatus. GUSTAVSBERGS FABRIKER A.B. Dec.11, 1956 [Dec. 16, 1955], No. 37843/56. Class 51 (1). In an intermittently-operating combustion apparatus comprising a combustion chamber having openings with non- return valves for the supply of air, means for the supply of fuel (preferably liquid fuel), and an outlet for the products of combustion, the fuel supply means are positively controlled to supply fuel intermittently and at a frequency which is not greater than the resonance frequency of the apparatus and is lower than 50 periods per second. The outlet of the combustion chamber is connected to a device for recovering heat from the products of combustion. The apparatus shown comprises a combustion chamber 1 having air intakes 4 controlled by non-return valves 5, air passing through the tubes 6 into the chamber 1. A fuel injection device 2 supplied from a pump 3, and an igniter 7 are also provided. The combustion chamber 1 is connected to a discharge duct 8 and the combustion chamber and discharge duct are enclosed in a container 11 which may be supplied with water so as to constitute a hot water boiler or a steam generator. The discharge duct 8 includes two bends and a diffuser 9 is provided before each bend and a further diffuser 10 is provided at the outlet from the discharge duct. More than one discharge duct may be provided and the ratio of the length to the diameter of the duct is 180 to 1, or greater. The total cross-sectional area of the ducts in square metres is smaller than one quarter the product of the volume of the combustion chamber in cubic metres and the length of the discharge ducts in metres. The frequency of the fuel supply means, also the capacity of the fuel supply means at any one frequency, may be variable. The fuel supply means may be a reciprocating pump having means for varying the speed and/or the effective length of stroke thereof. Alternatively a pressurized source of fuel may be used being provided with an intermittently-operating cut-off valve which controls the supply of fuel to the combustion chamber and has a controllable frequency and/or controllable opening periods. Means such as swirl vanes may be provided for imparting rotary movement to the air entering the combustion chamber. The apparatus may be constructed for the combustion of gaseous or pulverized fuel.
GB37843/56A 1955-12-16 1956-12-11 Improved device for intermittent combustion Expired GB809570A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE809570X 1955-12-16

Publications (1)

Publication Number Publication Date
GB809570A true GB809570A (en) 1959-02-25

Family

ID=20342791

Family Applications (1)

Application Number Title Priority Date Filing Date
GB37843/56A Expired GB809570A (en) 1955-12-16 1956-12-11 Improved device for intermittent combustion

Country Status (1)

Country Link
GB (1) GB809570A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1271465B (en) * 1966-11-30 1968-06-27 Boelkow Gmbh Solid rocket combustion chamber
US11933607B2 (en) 2019-08-08 2024-03-19 Sigmasense, Llc. Electrode mapping and signal orthogonality for capacitive imaging glove

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1271465B (en) * 1966-11-30 1968-06-27 Boelkow Gmbh Solid rocket combustion chamber
US11933607B2 (en) 2019-08-08 2024-03-19 Sigmasense, Llc. Electrode mapping and signal orthogonality for capacitive imaging glove
US12018940B2 (en) 2019-08-08 2024-06-25 Sigmasense, Llc. Digit movement detection based on capacitive imaging

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