CN104948347B - Thrust chamber collector with flow uniformizing function - Google Patents

Thrust chamber collector with flow uniformizing function Download PDF

Info

Publication number
CN104948347B
CN104948347B CN201410124535.XA CN201410124535A CN104948347B CN 104948347 B CN104948347 B CN 104948347B CN 201410124535 A CN201410124535 A CN 201410124535A CN 104948347 B CN104948347 B CN 104948347B
Authority
CN
China
Prior art keywords
collector
wall
inlet
outside
inwall
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
CN201410124535.XA
Other languages
Chinese (zh)
Other versions
CN104948347A (en
Inventor
周伟
杨继东
谢恒�
王晓丽
袁宇
李晓旭
宣智超
卢明
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.)
Beijing Aerospace Propulsion Institute
Original Assignee
Beijing Aerospace Propulsion Institute
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 Beijing Aerospace Propulsion Institute filed Critical Beijing Aerospace Propulsion Institute
Priority to CN201410124535.XA priority Critical patent/CN104948347B/en
Publication of CN104948347A publication Critical patent/CN104948347A/en
Application granted granted Critical
Publication of CN104948347B publication Critical patent/CN104948347B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Jet Pumps And Other Pumps (AREA)

Abstract

The invention relates to the liquid rocket propulsion technology, and particularly discloses a thrust chamber collector with a flow uniformizing function. A body shell is composed of an inner wall and an outer wall together. A cylinder formed when the inner wall is closed serves as a combustion chamber. An interlayer between the inner wall and the outer wall forms a cooling passageway. Annular grooves are formed in the inlet and the outlet of the cooling passageway. A bent pipe of the collector is welded and connected to the body shell at the annular groove in the inlet of the cooling passageway. A collector cavity is formed by the bent pipe and the body shell. The opening of the collector cavity is welded and connected to an inlet flange to form a collector inlet. Due to the double-collection-cavity structure, fluid is secondarily uniformized before entering the cooling passageway; by means of a horn-shaped expansion inlet with a reverse-Y-shaped diversion piece, fluid can more stably turn at the collector inlet, pressure fluctuation at the inlet and the two sides is reduced, local pressure loss can be reduced, and the diversion piece can play a role in reinforcing structure supporting.

Description

A kind of thrust chamber collector with flow equalizing function
Technical field
The invention belongs to liquid-propellant rocket engine designing technique is and in particular to a kind of collection of liquid rocket engine thrust chamber Clutch.
Background technology
Liquid rocket engine thrust chamber inner chamber is the combustion gas of high temperature, high pressure, in order to avoid locular wall occurs ablative degradation, It is provided with cooling jacket between inner and outer wall, introduce cryogen and locular wall is cooled down.The effect of inlet collector is exactly In every autonomous channel that the fluid distribution that engine general assembly Pipeline transport is come is distributed to cooling jacket complete cycle.In order to ensure The flow distribution of cooling duct is more uniform, to avoid combustion gas side wall temperature circumferential asymmetry even it is desirable to the pressure in collector exit Distribution is more uniform better.
As depicted in figs. 1 and 2, existing collector is designed with the circular single cavity structure of circular cross-section, collector Chamber 5 is directly connected with cooling duct 6 import, and pipe somewhere is arranged a suction flange 1 and is connected with general assembly pipeline, entrance no water conservancy diversion Device.This kind of collector structure has the following disadvantages:(1)The pressure reduction that fluid is formed along the flowing of collector chamber 5 ring directly contributes Collector outlet pressure is uneven;(2)The right-angle turning that intimate 90 degree of porch causes inlet region pressure distribution fluctuation more acute Strong.
Content of the invention
It is an object of the invention to provide a kind of outlet pressure uniformly, inlet fluid turn round more gentle, pressure oscillation and The less thrust chamber collector with flow equalizing function of local pressure loss.
Technical scheme is as follows:
A kind of thrust chamber collector with flow equalizing function, it includes columnar inwall, is located at the cylinder of inner wall outside The outer wall of shape, inwall closing forms combustion chamber, the space formation cooling duct between inner and outer wall, the side of the porch of outer wall Annular groove is circumferentially machined with wall, outside the described porch of outer wall, is fixed with annular distance seat, fixation outside described annular distance seat sets There is collector bend pipe;Described annular distance seat be disc, outside section be circular arc, inside section be shoulder structure, shoulder with Internal inner and outer wall is fixedly connected;Described annular distance seat be machined with several radial holes radially along complete cycle, each radial hole Run through inside and outside annular distance seat section;It is machined with arc opening, the outside of pipe is provided with method inside described collector bend pipe Blue;The section outer arc shape of described annular distance seat and the arc opening of above-mentioned collector bend pipe form complete circle;
In a kind of above-mentioned thrust chamber collector with flow equalizing function:The outside of described pipe processes one and enters Mouthful, porch is provided with expanding suction flange, and porch is fixed with " people " shape flow deflector simultaneously.
In a kind of above-mentioned thrust chamber collector with flow equalizing function:The aperture of each described radial hole is different.
In a kind of above-mentioned thrust chamber collector with flow equalizing function:The different form in the aperture of described radial hole For being respectively the minimum and maximum hole in aperture from two nearest and farthest radial holes of collector entrance, then dividing to entrance both sides Aperture diminishes radial hole not circumferentially successively.
The remarkable result of the present invention is:Due in collector bend pipe design and installation annular distance seat so that collector bend pipe Form outer set chamber between inwall and annular distance seat, formation interior set chamber between annular distance seat and burning chamber shell, double set cavity configurations, Fluid is made to realize secondary all flowing before entering cooling duct.
Externally the radial bore apertures between set chamber and interior set chamber are designed using not equal aperture, according to the ring in outer set chamber To pressure differential devise radial hole pore size so that the circumferential pressure difference adjustment in set chamber outward adapt to pore size so that Interior set cavity pressure before passage tends to uniform.
Collector elbow inlet, using the tubaeform expanded flange structure of band " people " shape flow deflector, makes collector porch flow Body turns round more gentle, reduces the pressure oscillation of entrance and two lateral areas, and can reduce local pressure loss;Other flow deflector is also The effect strengthening entrance structure inner chamber bearing capacity can be played.
Brief description
Fig. 1 is single-chamber collector structural front view in prior art;
Fig. 2 is the A-A sectional view of Fig. 1;
Fig. 3 is the thrust chamber collector structural representation with flow equalizing function;
Fig. 4 is the B-B sectional view of Fig. 3;
Fig. 5 is the stereochemical structure profile of the thrust chamber collector with flow equalizing function;
In figure:1. suction flange;2. collector bend pipe;3. inwall;4. outer wall;5. collector chamber;6. cooling duct;7. expand Open type suction flange;8. annular distance seat;9. outer set chamber;10. radial hole;Set chamber in 11.;12. flow deflectors;13. combustion chambers.
Specific embodiment
Below in conjunction with the accompanying drawings and specific embodiment is described in further detail to the present invention.
As shown in Figure 3 and Figure 4, the bend pipe that the pipe that described collector bend pipe 2 is circular for section surrounds, and bend pipe Inner side be machined with arc opening, the external circumferential optional position of pipe processes an entrance.In this porch, expanding is installed Suction flange 7, is welded and fixed " people " shape flow deflector 12 in porch simultaneously.
Annular distance seat 8 is welded on the arc opening of the inner side of pipe, described welding annular distance seat 8 is disc, its section Shape is as shown in figure 3, be circular arc outside section, it forms complete circle, in section with the section of above-mentioned collector bend pipe 2 Side is with shoulder structure, shoulder and internal inwall 3 and the fixing welding of outer wall 4.Annular distance seat 8 be machined with number radially along complete cycle Individual radial hole 10, in the present embodiment, the number of radial hole 10 is 36.Each radial hole 10 runs through inside and outside the two of annular distance seat 8 section Side.
So that interior set cavity pressure tends to uniform, the circumferential pressure difference in outer set chamber is adjusted, each radial hole 10 apertures are using the design of not equal aperture.As shown in figure 4, in the present embodiment, by two footpaths nearest and farthest from collector entrance It is respectively designed to the minimum and maximum hole in aperture to hole 10, then to entrance both sides radial hole 10 hole successively circumferentially respectively Footpath diminishes.
Compared with collector the same, the collector of the present invention also has closes, by inwall 3, the combustion chamber 13 being formed, and Outer wall 4 is installed, the space formation cooling duct 6 between inwall 3 and outer wall 4 outside inwall 3.The side wall of the porch of outer wall 4 On be circumferentially machined with annular groove.
The inner side of above-mentioned annular distance seat 8 is just welded at the annular groove of outer wall 4 porch, so just may be used from Fig. 3 and Fig. 4 Arrive, the cavity constituting between the inwall of collector bend pipe 2 and annular distance seat 8 is outer set chamber 9, and annular distance seat 8 and inwall 3 outer wall 4 Between the housing of combustion chamber 13 being collectively forming, i.e. space at the annular groove of outer wall 4 porch, define so-called interior set Chamber 11.From fig. 4, it can be seen that above-mentioned outer set chamber 9 and interior set chamber 11 are annular chamber, and set chamber 9 and Nei Ji outward The radial hole 10 passing through to process in chamber 11 is closed on annular space seat 8 communicate.
After fluid enters expanding suction flange 7, under the collective effect of expanding suction flange 7 and flow deflector 12, Smooth enters outer set chamber 9 along flow deflector 12 both sides so that the pressure at inlet fluctuation in collector bend pipe 2 is effectively pressed down System.In addition, when fluid enters into interior set chamber 11 from outer set chamber 9 by radial hole 10, radial hole 10 makes interior collector chamber Pressure distribution in 11 is optimized, larger in the position aperture low near entrance, static pressure, in the position high away from entrance, static pressure Put that aperture is less, thus making fluid gather the pressure reduction that in chamber 9, ring flowing is formed outside can be had after radial hole 10 Effect decay, then after interior set chamber 11 carries out secondary distribution, the pressure of cooling duct 6 entrance can be made to tend to uniform.

Claims (4)

1. a kind of thrust chamber collector with flow equalizing function, it includes columnar inwall (3), is located at outside inwall (3) Columnar outer wall (4), inwall (3) closing forms combustion chamber (13), and the space between inwall (3) and outer wall (4) forms cooling Passage (6), the side wall of the porch of outer wall (4) is circumferentially machined with annular groove it is characterised in that:The entering of described outer wall (4) It is fixed with annular distance seat (8) outside at mouthful, outside described annular distance seat (8), be fixed with collector bend pipe (2);Described annular distance seat (8) it is annular, for circular arc outside section, be shoulder structure, shoulder and internal inwall (3) and outer wall (4) inside section It is fixedly connected;Described annular distance seat (8) be machined with several radial holes (10) radially along complete cycle, each radial hole (10) runs through ring Inside and outside hole seat (8) section;It is machined with arc opening, the outside of pipe is provided with method inside described collector bend pipe (2) Blue;The section outer arc shape of described annular distance seat (8) forms complete circle with the arc opening of above-mentioned collector bend pipe (2) Shape.
2. as claimed in claim 1 a kind of thrust chamber collector with flow equalizing function it is characterised in that:Described pipe One entrance of outside processing, porch is provided with expanding suction flange (7), and porch is fixed with " people " shape flow deflector simultaneously (12).
3. as claimed in claim 1 a kind of thrust chamber collector with flow equalizing function it is characterised in that:Described several footpaths Different to each aperture of hole (10).
4. as claimed in claim 3 a kind of thrust chamber collector with flow equalizing function it is characterised in that:Described radial hole (10) the different form in aperture is, from two nearest and farthest radial holes (10) of collector entrance be respectively aperture maximum and Minimum hole, then to entrance both sides, radial hole (10) circumferentially diminishes in aperture successively respectively.
CN201410124535.XA 2014-03-31 2014-03-31 Thrust chamber collector with flow uniformizing function Active CN104948347B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410124535.XA CN104948347B (en) 2014-03-31 2014-03-31 Thrust chamber collector with flow uniformizing function

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410124535.XA CN104948347B (en) 2014-03-31 2014-03-31 Thrust chamber collector with flow uniformizing function

Publications (2)

Publication Number Publication Date
CN104948347A CN104948347A (en) 2015-09-30
CN104948347B true CN104948347B (en) 2017-02-15

Family

ID=54163314

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410124535.XA Active CN104948347B (en) 2014-03-31 2014-03-31 Thrust chamber collector with flow uniformizing function

Country Status (1)

Country Link
CN (1) CN104948347B (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106286007B (en) * 2016-09-23 2018-03-20 北京动力机械研究所 A kind of gas collection ring cavity rectifier structure for improving cooling qi leel cloth
CN106383972B (en) * 2016-11-04 2023-05-12 北京航天动力研究所 Collector for rocket engine thrust chamber and radial hole flow equalization design method thereof
CN107940157B (en) * 2017-11-20 2020-07-24 西安航天动力研究所 Regenerative cooling gas guide pipe and processing method thereof
CN112145316B (en) * 2018-01-23 2021-07-23 陕西蓝箭航天技术有限公司 Liquid engine
CN108979900A (en) * 2018-08-29 2018-12-11 北京航天动力研究所 A kind of collection pendular ring in liquid rocket engine thrust chamber body portion
CN108825406A (en) * 2018-08-29 2018-11-16 北京航天动力研究所 A kind of liquid rocket engine thrust chamber body portion outer wall construction
CN109779790A (en) * 2019-03-11 2019-05-21 北京星际荣耀空间科技有限公司 A kind of thrust chamber of liquid-propellant rocket engine
CN110282163B (en) * 2019-07-08 2021-04-02 盐城科宇机械制造有限公司 Spacecraft collector with flange
CN111456866A (en) * 2020-04-14 2020-07-28 合肥中科重明科技有限公司 Cooling liquid film forming structure of liquid rocket engine
CN111963338B (en) * 2020-08-11 2022-08-12 西安航天动力研究所 Flow guiding device of gas branch pipeline
CN112253333B (en) * 2020-09-17 2021-08-10 北京航天动力研究所 Collector inlet flow guide structure with flow equalizing function
CN114571053B (en) * 2022-03-18 2023-12-12 北京航天动力研究所 Titanium alloy vacuum diffusion welding spray pipe and design method

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2356572C3 (en) * 1973-11-13 1979-03-29 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Liquid-cooled rocket combustion chamber with thrust nozzle
US9194335B2 (en) * 2012-03-09 2015-11-24 Aerojet Rocketdyne Of De, Inc. Rocket engine coolant system including an exit manifold having at least one flow guide within the manifold
CN203130283U (en) * 2013-03-15 2013-08-14 北京航天动力研究所 Flow equalizer for suppressing flow distortion
CN203796441U (en) * 2014-03-31 2014-08-27 北京航天动力研究所 Thrust chamber collector with flow equalizing function

Also Published As

Publication number Publication date
CN104948347A (en) 2015-09-30

Similar Documents

Publication Publication Date Title
CN104948347B (en) Thrust chamber collector with flow uniformizing function
RU2302533C2 (en) Steam turbine intake hole and method of its modification
US7805943B2 (en) Shroud for a turbomachine combustion chamber
CN109163876B (en) A kind of water-cooled supersonic nozzle
RU2015130236A (en) ACTIVE NATURAL COOLING OF THE EXTERNAL CASING OF A GAS TURBINE, INCLUDING THE RELEASE OF AIR INTO A CAVITY WITH PRESSURE UNDER THE PRESSURE OF THE ENVIRONMENT
US9581026B2 (en) Steam turbine
CN109000878B (en) A kind of diffuser for plasma wind tunnel
FR2929993A1 (en) DIVERGENT COOLING ARRANGEMENTS FOR COMBUSTION CHAMBER SHIELDS AND CORRESPONDING METHOD
US10989074B2 (en) Turbine exhaust hood
CN105089852A (en) Combustion chamber inner liner cooling structure
WO2020063750A1 (en) Liquid cooling servo motor
US9400111B2 (en) Gas turbine combustor and gas turbine
JP2019002376A (en) Gas turbine engine
US20230033194A1 (en) Resonator ring for combustion chamber systems
CN106026500A (en) Water cooling motor shell
CN203796441U (en) Thrust chamber collector with flow equalizing function
US11365883B2 (en) Turbine engine combustion chamber bottom
CN207668180U (en) A kind of non-rotation type close-up formula controlled rolling passing water cooler
JP2021513927A5 (en)
CN108798790A (en) Blade profile tube nozzle for gas turbine
CN207379130U (en) A kind of water cooled seal housing
CN103470581B (en) A kind of radial gas rectifier
CN202621560U (en) Roller with inner-cooling structure
CN104594954B (en) Turbine structure and there is its gas turbine
CN106593546A (en) Turbine low-pressure steam admission mode and equipment

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant