CN205191557U - Combustion chamber anti -backfire structure - Google Patents

Combustion chamber anti -backfire structure Download PDF

Info

Publication number
CN205191557U
CN205191557U CN201520925240.2U CN201520925240U CN205191557U CN 205191557 U CN205191557 U CN 205191557U CN 201520925240 U CN201520925240 U CN 201520925240U CN 205191557 U CN205191557 U CN 205191557U
Authority
CN
China
Prior art keywords
combustion chamber
ring cavity
fuel nozzle
fuel injector
nozzle
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.)
Active
Application number
CN201520925240.2U
Other languages
Chinese (zh)
Inventor
刘莉娜
米强
时晓军
何民
刘丛红
韩晓鑫
张永川
程治刚
常胜男
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.)
AVIC Harbin Dongan Engine Group Co Ltd
Original Assignee
AVIC Harbin Dongan Engine Group Co Ltd
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 AVIC Harbin Dongan Engine Group Co Ltd filed Critical AVIC Harbin Dongan Engine Group Co Ltd
Priority to CN201520925240.2U priority Critical patent/CN205191557U/en
Application granted granted Critical
Publication of CN205191557U publication Critical patent/CN205191557U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Combustion Methods Of Internal-Combustion Engines (AREA)

Abstract

The utility model relates to a combustion chamber anti -backfire structure, including combustion chamber casing, electric nozzle, fuel injector, fuel injector installs on the casing of combustion chamber, and electric nozzle installs before fuel injector and lies in the combustion chamber, fuel injector radially open and have the nozzle opening, form the ring cavity between fuel injector and the casing, the ring cavity is a variable cross -section structure, variable cross -section structure minimum at the cross sectional area who is lieing in electric nozzle terminal surface department for the ring cavity. The utility model discloses an improve in current structure, the simple preparation is feasible, and the effect is showing, and the effectual combustion efficiency that has guaranteed also that electric nozzle is not burnt out.

Description

A kind of combustion chamber anti-backfire structure
Technical field
The utility model relates to a kind of combustion chamber anti-backfire structure.
Background technology
Combustion chamber is one of large parts of engine three, and in it, chemical reaction occurring, is heat energy by the chemical energy of fuel, allowable temperature before the pressure-air after heating compressor pressure to turbine.Generally, the seed region of fuel in combustion chamber and air carry out premixed combustion, light fuel and the air of abundant premix in primary zone.When fuel combustion, gas expansion causes the instantaneous reduction of pressure, makes sparking plug forefoot area produce negative pressure, inhales near, produces tempering, cause combustion zone to be removed from ideal position, thus reduce burner efficiency, even by sparking plug scaling loss by combustion zone to sparking plug forefoot area.
Summary of the invention
The purpose of this utility model is to provide a kind of anti-backfire structure, can reach raising burner efficiency, avoids the object of sparking plug scaling loss.
The technical solution of the utility model is, combustion chamber anti-backfire structure comprises burning chamber shell, sparking plug, fuel nozzle, fuel nozzle is arranged on burning chamber shell, sparking plug to be arranged on before fuel nozzle and to be positioned at combustion chamber, described fuel nozzle radial direction has nozzle opening, ring cavity is formed between described fuel nozzle and housing, the fuel blending that pressure-air and nozzle opening spray flows to outside ring cavity, described ring cavity is a variable section structure, and described variable section structure is that the area of section that ring cavity is being positioned at sparking plug end is minimum.The variable section structure of described ring cavity is by shell inner surface inwardly protruding or/and fuel nozzle outer radial outer lug is formed.
The utility model in use, due to minimum at the area of sparking plug end face, fuel is rear and pressure-air premix from nozzle opening ejection, the passage flowing through convergent is expanded to smallest cross-sectional place, pressure raises, eliminate the negative pressure because gas expansion produces, thus sparking plug forefoot area can not be made to produce negative pressure, effectively prevent tempering phenomenon.The utility model by improving in existing structure, and method is simple and feasible, Be very effective, effectively ensure that efficiency of combustion, also ensure that sparking plug is not burnt.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Detailed description of the invention
As shown in the figure, combustion chamber anti-backfire structure comprises burning chamber shell 1, sparking plug 2, fuel nozzle 3, fuel nozzle 3 is arranged on burning chamber shell 1, be positioned at combustion chamber before sparking plug 2 is arranged on fuel nozzle 3, described fuel nozzle 3 radial direction has nozzle opening 5, ring cavity 4 is formed between described fuel nozzle and housing, the fuel blending that pressure-air and nozzle opening 5 spray flows to outside ring cavity 4, described ring cavity 4 is a variable section structure, and described variable section structure is that the area of section that ring cavity 4 is being positioned at sparking plug end face 6 place is minimum.The variable section structure of described ring cavity 4 is by shell inner surface inwardly protruding or/and fuel nozzle 3 outer radial outer lug is formed.

Claims (2)

1. a combustion chamber anti-backfire structure, it is characterized in that, described structure comprises burning chamber shell (1), sparking plug (2), fuel nozzle (3), fuel nozzle (3) is arranged on burning chamber shell (1), it is front and be positioned at combustion chamber that sparking plug (2) is arranged on fuel nozzle (3), described fuel nozzle (3) radial direction has nozzle opening (5), ring cavity (4) is formed between fuel nozzle and housing, the fuel blending that pressure-air and nozzle opening (5) spray flows to ring cavity (4) outward, described ring cavity (4) is a variable section structure, described variable section structure is that the area of section that ring cavity (4) is being positioned at sparking plug end face (6) place is minimum.
2. combustion chamber as claimed in claim 1 anti-backfire structure, is characterized in that, the variable section structure of described ring cavity (4) is by shell inner surface inwardly protruding or/and fuel nozzle (3) outer radial outer lug is formed.
CN201520925240.2U 2015-11-19 2015-11-19 Combustion chamber anti -backfire structure Active CN205191557U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520925240.2U CN205191557U (en) 2015-11-19 2015-11-19 Combustion chamber anti -backfire structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520925240.2U CN205191557U (en) 2015-11-19 2015-11-19 Combustion chamber anti -backfire structure

Publications (1)

Publication Number Publication Date
CN205191557U true CN205191557U (en) 2016-04-27

Family

ID=55784540

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201520925240.2U Active CN205191557U (en) 2015-11-19 2015-11-19 Combustion chamber anti -backfire structure

Country Status (1)

Country Link
CN (1) CN205191557U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105240847A (en) * 2015-11-19 2016-01-13 哈尔滨东安发动机(集团)有限公司 Anti-backfire structure of combustion chamber

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105240847A (en) * 2015-11-19 2016-01-13 哈尔滨东安发动机(集团)有限公司 Anti-backfire structure of combustion chamber

Similar Documents

Publication Publication Date Title
EP2980483A1 (en) Gas turbine combustor
MX2015005799A (en) Pressure-gain combustion apparatus and method.
JP2012211749A (en) Combustor for gas turbine engine and gas turbine engine
CN202792029U (en) Three-ring fire large-power combustor
JP2016035336A5 (en)
CN105444169A (en) Cooking appliance combustor for improving secondary air flowing
CN105276617A (en) Gas turbine combustor
CN203848291U (en) Premixed fuel gas positive pressure burning energy-saving burner
CN203309935U (en) Single-liner type combustion gas turbine combustion chamber
WO2012016748A3 (en) Gas turbine combustion chamber
CN205191557U (en) Combustion chamber anti -backfire structure
CN102644920A (en) Combustor with multiple ejector pipes
CN205543691U (en) Small -size non - cooling plasma jet point firearm
CN105240847A (en) Anti-backfire structure of combustion chamber
CN201954547U (en) Gas burner with high pressure head
CN105091031A (en) Turbomachine combustor including combustor sleeve baffle
CN203757718U (en) Outer ring burner cap of burner and gas stove burner
CN204005981U (en) A kind of gas burner assembly
CN202673455U (en) Spiral-flow type plasma ignition mouth
CN105509043B (en) A kind of fuel-gasifying cooking device
CN212746470U (en) Gas dual-purpose burner
CN215765098U (en) Outer ring combustion nozzle of combustor
CN203605283U (en) Stove internal combustion fire combustor
CN202852808U (en) Containing type jet flow coal dust furnace plasma thermal cracking burning device
CN105042637A (en) Combustion chamber

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant