CN104948347B - Thrust chamber collector with flow uniformizing function - Google Patents
Thrust chamber collector with flow uniformizing function Download PDFInfo
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- 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
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- inwall
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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
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.
Priority Applications (1)
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CN201410124535.XA CN104948347B (en) | 2014-03-31 | 2014-03-31 | Thrust chamber collector with flow uniformizing function |
Applications Claiming Priority (1)
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CN201410124535.XA CN104948347B (en) | 2014-03-31 | 2014-03-31 | Thrust chamber collector with flow uniformizing function |
Publications (2)
Publication Number | Publication Date |
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CN104948347A CN104948347A (en) | 2015-09-30 |
CN104948347B true CN104948347B (en) | 2017-02-15 |
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CN201410124535.XA Active CN104948347B (en) | 2014-03-31 | 2014-03-31 | Thrust chamber collector with flow uniformizing function |
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Families Citing this family (12)
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)
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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 |
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