WO1981000610A1 - Chambre de combustion - Google Patents

Chambre de combustion Download PDF

Info

Publication number
WO1981000610A1
WO1981000610A1 PCT/SE1980/000206 SE8000206W WO8100610A1 WO 1981000610 A1 WO1981000610 A1 WO 1981000610A1 SE 8000206 W SE8000206 W SE 8000206W WO 8100610 A1 WO8100610 A1 WO 8100610A1
Authority
WO
WIPO (PCT)
Prior art keywords
chamber
partition wall
combustion chamber
wall
walls
Prior art date
Application number
PCT/SE1980/000206
Other languages
English (en)
Inventor
K Olsson
Original Assignee
Mareck Bv
K Olsson
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 Mareck Bv, K Olsson filed Critical Mareck Bv
Priority to AU62238/80A priority Critical patent/AU538750B2/en
Publication of WO1981000610A1 publication Critical patent/WO1981000610A1/fr

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 
    • F23C3/00Combustion apparatus characterised by the shape of the combustion chamber
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24HEATING; RANGES; VENTILATING
    • F24HFLUID HEATERS, e.g. WATER OR AIR HEATERS, HAVING HEAT-GENERATING MEANS, e.g. HEAT PUMPS, IN GENERAL
    • F24H9/00Details
    • F24H9/18Arrangement or mounting of grates or heating means
    • F24H9/1809Arrangement or mounting of grates or heating means for water heaters
    • F24H9/1832Arrangement or mounting of combustion heating means, e.g. grates or burners
    • F24H9/1836Arrangement or mounting of combustion heating means, e.g. grates or burners using fluid fuel

Definitions

  • the present invention relates to such combustion chambers as are disclosed in the preamble to the following claim 1.
  • a combustion chamber of the kind in question is disclosed / e.g. in the U.S. patent 3 853 453.
  • the partition wall will be in the shape of a cross.
  • the ends of the cross are free in the side chambers, while the side edges of the cross are attached to the inside of the combustion chamber.
  • the combustion chamber and the partition wall are usually cast in one piece, but it is also possible to manufacture the partition wall as a separate part and weld it in the combustion chamber.
  • the combustion chamber is intended to dissipate heat to the surroundings for heating. In most cases, known combustion chambers of the kind in question are surrounded by water in a hot water installation, e.g. hot water for a dwelling house. If cracks occur in the wall of the combustion chamber, the result can be that water comes into the combustion chamber and causes operational disturbances and stoppages.
  • the object of the present invention is to eliminate this risk.
  • the invention is based on the knowledge that cracks in the combustion chamber wall must . be prevented, while it is possible to allow cracks of a certain width in the partition wall without this the function of the apparatus.
  • the problem is solved in accordance with the invention such that in the manufacture of the partition wall, said wall is already provided with stress concentration locations or indications of fracture at predetermined places for providing desired cracks in the partition wall when said wall and the walls of the side chambers are subjected to heat stresses during the first runs as well as heatings during starting and coolings during stopping the apparatus.
  • the partition wall thus cracks into two parts in each side chamber, so that these parts can move freely relative each other during heating and cooling. The cracks which occur will, however, be so narrow that they do not affect the course of combustion.
  • Fig. 1 is a side view of the combustion chamber in accordance with the invention.
  • Fig. 2 is a view from above.
  • Fig. 3 is a section along the line 3-3 in Fig. 1
  • Fig. 4 is a section along the line 4-4 in Fig. 2
  • Fig. 5 is a section along the line 5-5 in Fig. 2.
  • the whole combustion chamber is integrally cast steel, and consists of identically similar side chambers 10,12,14,16 which are uniformly distributed around the central axis of the combustion chamber.
  • the side chamber 12 for example, has two opposing side walls 12a,12b and an arcuate outer wall 12c so that the side chambers will be substantially half- cylindrical.
  • the side walls of the side chambers merge into each other and form corners 18 in the central space of the combustion chamber, to which the side chambers are connected.
  • the outer walls of the side chambers run together in an upper end wall 20 and in a lower end wall 22.
  • An inlet port 24 is made in the end wall 20 for accommodating an axial inlet pipe (not shown) .
  • the end wall 22 is formed with an axial outlet 26, to which an exhaust pipe is to be connected.
  • the central zone of the combustion chamber is /'i ⁇ K .
  • the partition wall 28 is extended with side portions 28a at the side chambers, said portions extending as projections into the respective side chamber and are terminated with an end edge 28b situated at a predetermined distance from the outer wall of the respective side chamber, e.g. the outer wall 12c of the side chamber 12.
  • an end edge 28b situated at a predetermined distance from the outer wall of the respective side chamber, e.g. the outer wall 12c of the side chamber 12.
  • the part of the combustion chamber including the side walls, lying above the partition wall form a first chamber 32 in which the fuel-air mixture is ignited and combusted, where ⁇ after the combustion gases flow, with a certain amount of terminating combustion, down through the openings 30 to the subsequent second chamber 34 situated under the partition wall.
  • the illustrated combustion chamber is usually intended to be kept immersed in a container with water which is to be heated. Since the partition wall 28,28a is cast in one piece with the rest of the combustion chamber, the edge portions of the partition wall will be rigidly attached to the walls of the combustion chamber and to the side walls of the side chambers. This signifies, inter alia, that considerable heat stresses can be obtained at the side edges 28c of the wall portions
  • each wall portion has a stress concentration location at its middle in the form of grooves 36,38,40,42 on the upper side of the partition wall.
  • the stress concentration locations illustrated in the example extend out to the respective end edge 28b and meet at the centre 44 of the partition wall.
  • the stress concentration locations are formed as V-shaped grooves, the depth of which is substantially greater than the thickness of the partition wall at the stress concentration. In the example illustrated, the depth of the groove is about 85% of the thickness of the partition wall at the stress concentration.
  • the side portions have a thickness increasing from the middle and out towards the side edges, where the wall portions connect via a softly rounded junction to the side walls of the side chamber.
  • the stress concentrations can naturally have a plurality of other locations than those illustrated in conjunction with the described embodiment.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
  • Combustion Of Fluid Fuel (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)

Abstract

Une chambre de combustion possede une pluralite de chambres laterales (10, 12, 14, 16) distribuees autour de la region centrale de la chambre. Une paroi de separation (28) divise la chambre en une premiere chambre et en une seconde chambre (32 et 34) et se prolonge par des portions de paroi (28a) se projetant partiellement dans les chambres laterales et rattachees a leurs parois laterales (12a, 12b), et laissant une ouverture de passage du flux (30) au bord extreme (28b) de la portion de paroi respective (28a). La paroi de separation (28) est pourvue d'une pluralite de points de concentration de contraintes (36, 38, 40, 42) sur lesquels la cloison (28) se rompt en fissures etroites pendant les quelques premiers demarrages et chauffages jusqu'a atteindre la temperature de fonctionnement normal et les refroidissements se produisant a l'arret, de maniere a ce que la cloison (28) soit exempte de contraintes lors des fonctionnements ulterieurs de l'appareil.
PCT/SE1980/000206 1979-08-14 1980-08-13 Chambre de combustion WO1981000610A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU62238/80A AU538750B2 (en) 1979-08-14 1980-08-13 Combustion chamber

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SE7906798 1979-08-14
SE7906798A SE418221B (sv) 1979-08-14 1979-08-14 Brennkammare

Publications (1)

Publication Number Publication Date
WO1981000610A1 true WO1981000610A1 (fr) 1981-03-05

Family

ID=20338624

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/SE1980/000206 WO1981000610A1 (fr) 1979-08-14 1980-08-13 Chambre de combustion

Country Status (6)

Country Link
EP (1) EP0034601A1 (fr)
BE (1) BE884793A (fr)
FI (1) FI802548A (fr)
IT (1) IT1132415B (fr)
SE (1) SE418221B (fr)
WO (1) WO1981000610A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2584169A1 (fr) * 1985-06-27 1987-01-02 Elf En Ensemble embouti pour la combustion pulsatoire

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE422990B (sv) * 1980-08-12 1982-04-05 Mareck Bv Brenslekammare for pulserande forbrenning
AT395523B (de) * 1990-07-24 1993-01-25 Spellitz Fritz Optisches messsystem fuer die menschliche hornhaut
US6529074B1 (en) * 2001-07-26 2003-03-04 Cirrus Logic, Inc. Circuits and methods for output impedance matching in switched mode circuits

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE361522B (fr) * 1972-04-04 1973-11-05 K B Olsson
US3879167A (en) * 1974-04-18 1975-04-22 Jones & Laughlin Steel Corp Non-warping heat shield

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE361522B (fr) * 1972-04-04 1973-11-05 K B Olsson
US3879167A (en) * 1974-04-18 1975-04-22 Jones & Laughlin Steel Corp Non-warping heat shield

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2584169A1 (fr) * 1985-06-27 1987-01-02 Elf En Ensemble embouti pour la combustion pulsatoire
EP0208600A1 (fr) * 1985-06-27 1987-01-14 Societe Nationale Elf Aquitaine Ensemble embouti pour la combustion pulsatoire
US4708634A (en) * 1985-06-27 1987-11-24 Societe Nationale Elf Aquitaine Drawn assembly for pulsatory combustion

Also Published As

Publication number Publication date
SE418221B (sv) 1981-05-11
FI802548A (fi) 1981-02-15
EP0034601A1 (fr) 1981-09-02
IT8024187A0 (it) 1980-08-14
BE884793A (fr) 1980-12-01
SE7906798L (sv) 1981-02-15
IT1132415B (it) 1986-07-02

Similar Documents

Publication Publication Date Title
EP1657403B1 (fr) Aube avec arrondis large et avec circuit de refroidissement comprennant des microcanaux
EP0335481B1 (fr) Paroi avec des passages de refroidissement
JP3340744B2 (ja) 拡散後縁架台を含むタービン翼型
JP3053174B2 (ja) ターボ機械に使用するための翼部及びその製造方法
US4242871A (en) Louver burner liner
US4484440A (en) Exhaust manifold of dual type formed with chamber to receive exhaust gas sensor
US3540810A (en) Slanted partition for hollow airfoil vane insert
JPH07189975A (ja) 燃料を貯蔵タンクから内燃機関に供給するための装置
US4511306A (en) Combustion turbine single airfoil stator vane structure
US5341770A (en) Integral lime inhibitor
JPH021963B2 (fr)
JPH04301101A (ja) ガスタービンエンジンのディスクポストの熱的保護装置及び方法
US4455972A (en) Cylinder block of an internal combustion engine
WO1981000610A1 (fr) Chambre de combustion
US3936220A (en) Jacket construction for fluid-circulating pumps
US4327672A (en) Fuel burning boiler
AU6223880A (en) Combustion chamber
CA1180996A (fr) Chambre de combustion
US4632065A (en) Thermal baffle for water heaters and the like
US4495987A (en) Tube and tube sheet assembly
US3215125A (en) Sectional boiler construction
JPH04362256A (ja) 内燃機関の冷却装置
FI61561C (fi) Effekt-vaermeanordning
JPH0116360B2 (fr)
KR950007455Y1 (ko) 보일러

Legal Events

Date Code Title Description
AK Designated states

Designated state(s): AU DK JP NO SU US

AL Designated countries for regional patents

Designated state(s): AT CH DE FR GB NL