US3853453A - Lobate combustion chamber - Google Patents

Lobate combustion chamber Download PDF

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Publication number
US3853453A
US3853453A US00346790A US34679073A US3853453A US 3853453 A US3853453 A US 3853453A US 00346790 A US00346790 A US 00346790A US 34679073 A US34679073 A US 34679073A US 3853453 A US3853453 A US 3853453A
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US
United States
Prior art keywords
combustion chamber
chamber
side chambers
inlet
shield
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 - Lifetime
Application number
US00346790A
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English (en)
Inventor
K Olsson
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Mareck BV
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Individual
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Publication date
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Publication of US3853453A publication Critical patent/US3853453A/en
Assigned to MARECK HOLDING N.V. reassignment MARECK HOLDING N.V. ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: OLSSON, KARL B.
Assigned to MARECK N.V. reassignment MARECK N.V. CHANGE OF NAME (SEE DOCUMENT FOR DETAILS). EFFECTIVE DATE: 9-04-80 Assignors: MARECK HOLDING N.V.
Assigned to MARECK B.V. reassignment MARECK B.V. ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: MARECK N.V.
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C15/00—Apparatus in which combustion takes place in pulses influenced by acoustic resonance in a gas mass

Definitions

  • a combustion chamber for pulsating combustion of a fuel air mixture has at one end an inlet for fuel air CCll. 4311/?2 mixture and at the pp end an outlet for gases- [58] Fie'ld 171
  • the cross section of the chamber at right angles to a 60 39 line between the inlet and the outlet has a configuration which deviates from the circle due to the fact that the chamber has a number of side chambers.
  • the present invention relates to a combustion chamber, particularly for pulsating combustion of a fuel air mixture, and having a final inlet at one end and an exhaust outlet at the opposite end.
  • Such combustion chambers may be used for heating a flow of water, air, or other fluid in which the chamber is immersed.
  • the object of the present invention is therefore to provide a combustion chamber having a configuration which, upon increase of the volume of the chamber, will result in a smaller increase of the heat load per surface unit in relation to what has hitherto been possible. Furthermore, the invention has for its object to prevent a straight through flow which in certain cases may reduce the efficiency of the combustion chamber.
  • the cross section of the chamber between the inlet and the outlet has a configuration which deviates from the circle due to the fact that the chamber has a number of side chambers, and there is a transverse shield which partitions the combustion chamber into first and second compartments so that a fuel mixture flowing through the inlet into the first compartment will be caused to flow around the shield through the side chambers into the second compartment and hence to the outlet.
  • FIG. I is an axial longitudinal section taken on the line ll in FIG. 2;
  • FIG. 2 is a cross section taken on the line 22 in FIG. 1;
  • FIG. 3 is a diagrammatic perspective view of the combustion chamber of FIGS. 1 and 2;
  • FIG. 4 is a cross section through another example of combustion chamber having substantially the same axial longitudinal section as in FIG. 1.
  • the illustrated combustion chamber is at one end provided with an inlet 12 for a fuel air mixture and at the opposite end with an outlet 14 for the combustion exhaust gases.
  • a mechanical non-return valve 13 may be provided in a known manner in the inlet.
  • the inlet of the combustion chamber may alternatively, in a manner known per se, be shaped as a so-called dynamic non-return valve. In those cases the combustion chamber may operate with pulsating combustion.
  • an ignition device such as a glow plug for starting the combustion.
  • a shield which, in the illustrated examples, consists of a plate 16.
  • This plate need not be flat but can be convex in either direction, The important feature is that it prevents straight through-flow to the outlet.
  • the combustion chamber has a configuration which deviates from the circle and is provided with at least two, in the example shown four, symmetrically positioned lobe like side chambers 18.
  • the side walls of the side chambers lie parallel to each other.
  • the outer wall of the side chambers extends as an arch as will be seen from FIG. 1 and FIG. 3.
  • the plate 16 is secured at the transition portions between the side walls of the side chambers.
  • the shield plate 16 extends partly into each of the side chambers and leaves a through-flow opening 22 between the free end edge 24 of the plate and the outer wall of the side chambers.
  • the plate may be positioned at different heights within the combustion chamber. In the example shown it is at about the middle of the height of the chamber between the inlet and the outlet.
  • the shield plate 16 When the fuel air mixture upon continuous operation is flowing from the inlet, it will strike the shield plate 16 and be caused by the plate to flow out into the side chambers 20 upon the combustion of the fuel air mixture. In the side chambers the gases will flow through the respective opening 22 to the outlet. Thus, the shield plate will divide the combustion chamber into a first compartment 26 and a second compartment 28.
  • the side chambers may have other cross sectional forms than those shown. Accordingly, it may be in some cases advantageous that the side chambers converge outwardly as is shown in FIG. 4 where the cross section form of the side chambers is triangular.
  • the plate is here denoted by the reference numeral 16a, and its edges by 24a.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)
  • Combustion Of Fluid Fuel (AREA)
  • Electrolytic Production Of Metals (AREA)
US00346790A 1972-04-04 1973-04-02 Lobate combustion chamber Expired - Lifetime US3853453A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE04294/72A SE361522B (fr) 1972-04-04 1972-04-04

Publications (1)

Publication Number Publication Date
US3853453A true US3853453A (en) 1974-12-10

Family

ID=20263873

Family Applications (1)

Application Number Title Priority Date Filing Date
US00346790A Expired - Lifetime US3853453A (en) 1972-04-04 1973-04-02 Lobate combustion chamber

Country Status (14)

Country Link
US (1) US3853453A (fr)
JP (1) JPS5244455B2 (fr)
BE (1) BE903024Q (fr)
CA (1) CA974135A (fr)
CH (1) CH553375A (fr)
DE (1) DE2316012C3 (fr)
DK (1) DK129368B (fr)
FI (1) FI52902C (fr)
FR (1) FR2178997B1 (fr)
GB (1) GB1380011A (fr)
IT (1) IT980056B (fr)
NL (1) NL179505B (fr)
NO (1) NO131807C (fr)
SE (1) SE361522B (fr)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3908069A (en) * 1973-04-13 1975-09-23 Shell Oil Co Coated particulate vinyl aromatic polymers
US4241720A (en) * 1979-01-26 1980-12-30 Kitchen John A Pulse combustion apparatus
US4241723A (en) * 1978-11-15 1980-12-30 Kitchen John A Pulse combustion apparatus
US4439134A (en) * 1980-08-12 1984-03-27 Mareck B.V. Combustion chamber for pulsating combustion
US4708634A (en) * 1985-06-27 1987-11-24 Societe Nationale Elf Aquitaine Drawn assembly for pulsatory combustion
US4759312A (en) * 1985-06-12 1988-07-26 Georg Pletzer Furnace system
US20050079461A1 (en) * 2002-04-19 2005-04-14 Jiro Kasahara Stationary detonation combustor, and stationary detonation wave generating method

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE418221B (sv) * 1979-08-14 1981-05-11 Karl Borje Olsson Brennkammare
US4475621A (en) * 1982-09-10 1984-10-09 Lennox Industries, Inc. Sound reduction means for pulsating type furnace

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2440491A (en) * 1935-03-21 1948-04-27 Des Vehicules Sev Soc Et Oil burner
DE960130C (de) * 1950-10-27 1957-03-14 Kaercher Fa Alfred Heizgeraet
US3005458A (en) * 1958-12-29 1961-10-24 Fargo Corp Therapeutic magnet
US3267986A (en) * 1962-05-18 1966-08-23 Olsson Karl Borje Apparatus for pulsating combustion
FR1509661A (fr) * 1966-02-17 1968-01-12 Junkers & C G M B H Installation de brûleur à combustion pulsatoire
US3606867A (en) * 1969-02-17 1971-09-21 Shell Oil Co Puisating combustion system

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE750516C (de) * 1939-03-17 1945-01-15 Verfahren zur Erzeugung von Druck und Waerme
US3041836A (en) * 1959-09-11 1962-07-03 Gen Electric Means for eliminating screech in jet propulsion systems

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2440491A (en) * 1935-03-21 1948-04-27 Des Vehicules Sev Soc Et Oil burner
DE960130C (de) * 1950-10-27 1957-03-14 Kaercher Fa Alfred Heizgeraet
US3005458A (en) * 1958-12-29 1961-10-24 Fargo Corp Therapeutic magnet
US3267986A (en) * 1962-05-18 1966-08-23 Olsson Karl Borje Apparatus for pulsating combustion
FR1509661A (fr) * 1966-02-17 1968-01-12 Junkers & C G M B H Installation de brûleur à combustion pulsatoire
US3606867A (en) * 1969-02-17 1971-09-21 Shell Oil Co Puisating combustion system

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3908069A (en) * 1973-04-13 1975-09-23 Shell Oil Co Coated particulate vinyl aromatic polymers
US4241723A (en) * 1978-11-15 1980-12-30 Kitchen John A Pulse combustion apparatus
US4241720A (en) * 1979-01-26 1980-12-30 Kitchen John A Pulse combustion apparatus
US4439134A (en) * 1980-08-12 1984-03-27 Mareck B.V. Combustion chamber for pulsating combustion
US4759312A (en) * 1985-06-12 1988-07-26 Georg Pletzer Furnace system
US4708634A (en) * 1985-06-27 1987-11-24 Societe Nationale Elf Aquitaine Drawn assembly for pulsatory combustion
US20050079461A1 (en) * 2002-04-19 2005-04-14 Jiro Kasahara Stationary detonation combustor, and stationary detonation wave generating method
US7310951B2 (en) * 2002-04-19 2007-12-25 Hokkaido Technology Licensing Office Co., Ltd. Steady-state detonation combustor and steady-state detonation wave generating method

Also Published As

Publication number Publication date
NO131807C (fr) 1975-08-06
BE903024Q (fr) 1985-12-02
DE2316012A1 (de) 1973-10-18
NO131807B (fr) 1975-04-28
FI52902B (fr) 1977-08-31
JPS498824A (fr) 1974-01-25
SE361522B (fr) 1973-11-05
CA974135A (en) 1975-09-09
DK129368C (fr) 1975-04-07
JPS5244455B2 (fr) 1977-11-08
NL179505B (nl) 1986-04-16
CH553375A (de) 1974-08-30
IT980056B (it) 1974-09-30
DK129368B (da) 1974-09-30
GB1380011A (en) 1975-01-08
FR2178997A1 (fr) 1973-11-16
DE2316012B2 (de) 1980-09-04
NL7304497A (fr) 1973-10-08
DE2316012C3 (de) 1981-06-04
FR2178997B1 (fr) 1974-05-17
FI52902C (fi) 1977-12-12

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Legal Events

Date Code Title Description
AS Assignment

Owner name: MARECK HOLDING N.V., HANDELSKADE 8, WILLEMSTAD, CU

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:OLSSON, KARL B.;REEL/FRAME:003929/0513

Effective date: 19811117

AS Assignment

Owner name: MARECK N.V.

Free format text: CHANGE OF NAME;ASSIGNOR:MARECK HOLDING N.V.;REEL/FRAME:003983/0060

Effective date: 19820105

AS Assignment

Owner name: MARECK B.V., MUSEUMPLEIN 11, 1071 DJ AMSTERDAM, NE

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:MARECK N.V.;REEL/FRAME:004571/0903

Effective date: 19860528