CN107063840A - A kind of device for solid rocket motor case list skirt axis pulling experiment - Google Patents
A kind of device for solid rocket motor case list skirt axis pulling experiment Download PDFInfo
- Publication number
- CN107063840A CN107063840A CN201611083786.3A CN201611083786A CN107063840A CN 107063840 A CN107063840 A CN 107063840A CN 201611083786 A CN201611083786 A CN 201611083786A CN 107063840 A CN107063840 A CN 107063840A
- Authority
- CN
- China
- Prior art keywords
- frame
- motor case
- rocket motor
- solid rocket
- solid
- 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.)
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Classifications
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N3/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N3/02—Details
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N3/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N3/08—Investigating strength properties of solid materials by application of mechanical stress by applying steady tensile or compressive forces
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2203/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N2203/0014—Type of force applied
- G01N2203/0016—Tensile or compressive
- G01N2203/0017—Tensile
Abstract
The present invention relates to a kind of device for solid rocket motor case list skirt axis pulling experiment, including end frame assembly, solid rocket motor case and concrete, frame assembly is held to include end frame, round steel and steel plate, the joint on the outside of the upper end of frame with solid rocket motor case is held to link together, hold the circular hole on the inside of the upper end of frame to be used to fix round steel, hold the through hole of the lower end of frame to be used to fix end frame and testing stand by bolt；Solid rocket motor case is fixed on the end frame of end frame assembly, and concrete, the height of concrete and the upper surface flush of steel plate are loaded inside solid rocket motor case.The present apparatus, connection is simple, safe and reliable, both may apply to solid rocket motor case list skirt axis pulling experiment, and can also be applied to the inconsistent axis pulling experiment of skirt stand under load before and after solid rocket motor case.
Description
Technical field
Drawn the present invention relates to a kind of axis pulling experiment device, more particularly to a kind of solid rocket motor case list skirt axle that is used for
The device of experiment.
Background technology
When solid rocket motor case only one of which skirt or inconsistent forward and backward skirt stand under load, in order to obtain solid-rocket hair
The axle of motivation housing skirt draws load, it is necessary to design a kind of method to meet the requirement of experiment.
Existing test method can only apply axle simultaneously to two skirts of solid rocket motor case and draw load, it is impossible to right
Single skirt carries out axle and draws loading.
The content of the invention
The technical problem to be solved in the present invention is to provide a kind of for solid rocket motor case list skirt axis pulling experiment
The problem of device, axis pulling experiment to solve solid rocket motor case list skirt.
To solve the technical problem existed, the technical solution adopted by the present invention is：One kind is used for solid propellant rocket shell
The device of body list skirt axis pulling experiment, including end frame assembly, solid rocket motor case and concrete, described end frame combination
Body includes end frame, round steel and steel plate, holds the correspondence position with the connecting socket of solid rocket motor case on the outside of the upper end of frame
Provided with multiple through holes, the through hole on the outside of the upper end of frame is held to be used for the joint that will hold frame and solid rocket motor case by bolt
Link together, multiple circular holes are evenly equipped with the inside of the upper end for holding frame, hold the circular hole on the inside of the upper end of frame to be used for threaded circle
Steel is fixed on the circular hole on the inside of the upper end of end frame, and the lower end outside of end frame is provided with multiple through holes, hold frame lower end outside it is logical
Hole is used to fix end frame and testing stand by bolt；Described round steel two ends are provided with screw thread, and round steel one end is fixed to nut
Hold on the circular hole on the inside of the upper end of frame, round steel other end nut fixation steel plate；Through hole is provided with the middle of described steel plate, steel plate leads to
Through hole is crossed installed in round steel one end and is fixed with nut, it is red at the upper surface of steel plate and the end socket of solid rocket motor case
Diatom is concordant；Described solid rocket motor case is fixed on the end frame of end frame assembly, solid propellant rocket
Enclosure interior loads concrete, the height of concrete and the upper surface flush of steel plate.
Beneficial effect：
The device connection of the present invention is simple, safe and reliable, realizes that obtaining solid rocket motor case list skirt axle draws load, both may be used
To be applied to solid rocket motor case list skirt axis pulling experiment, can also be applied to before and after solid rocket motor case skirt by
Carry inconsistent axis pulling experiment.
Brief description of the drawings
Fig. 1 is the device combination schematic diagram for solid rocket motor case list skirt axis pulling experiment；
Fig. 2 is end frame assembly schematic diagram；
Fig. 3 is end frame schematic diagram；
In figure：1 it is dismountable end frame assembly, 2 be solid rocket motor case, 3 be bolt, 4 be concrete, 5 is end
Frame, 6 be round steel, 7 be that nut and 8 is steel plate.
Embodiment
With reference to embodiment, the present invention will be further described.
As shown in figure 1, the present invention is used for the device of solid rocket motor case list skirt axis pulling experiment, experiment mainly includes
Dismountable end frame assembly 1, solid rocket motor case 2, bolt 3 and concrete 4.
As shown in Fig. 2 removably end frame assembly is made up of end frame 5, round steel 6, nut 7 and steel plate 8.The two of round steel 6
Side is provided with the screw thread of certain length.Steel plate 8 is provided with through hole.The surface of steel plate 8 is provided with through hole, is connected with round steel 6, for fixed solidification
Concrete afterwards.
As shown in figure 3, the side of end frame 5 is provided with multiple through holes that different distributions are justified, opposite side is provided with multiple through holes.Hold frame
With being provided with multiple through holes with the correspondence position of the connecting socket of solid rocket motor case 2 on the outside of 5 upper ends, for passing through bolt
End frame 5 be connected with the joint of solid rocket motor case 2, holds frame 5 upper end inner side to be evenly equipped with multiple circular holes, for will be with spiral shell
The round steel 6 of line is fixed in the frame 5 of end on mother rib lateral rotundum；The lower end outside of frame 5 is held to be provided with multiple through holes, with bolt by end frame 5 with testing
Platform is fixed.
The present invention provides a kind of device.With nut by Interal fixation to threaded round steel one end, steel plate is away from round steel end
The distance in face is 30mm, and then the threaded round steel other end is fixed on the inframe mother rib lateral rotundum of end with nut again, passes through nut
Distance of the steel plate away from round steel one end is adjusted, makes steel plate concordant with equatorial line at end socket, then with bolt by end frame and solid-rocket
The joint connection of motor body, is finally 1 by cement and sand weight ratio：2 concrete loads solid propellant rocket shell
Internal portion, concrete height is flushed with steel plate, it is concrete curing after, end frame one end is bolted to Test-bed, burns
Imposed load on room housing list skirt, can be used for solid propellant rocket skirt axis pulling experiment.
When it is implemented, according to nut, steel plate and nut order, by Interal fixation in threaded round steel one end（A）, will
Nut is fixed to the threaded round steel other end（B）；One end of round steel（B）Through end frame different distributions inner round side through hole, so
Round steel is fixed on the frame of end with nut afterwards；End frame assembly is fixed on solid rocket motor case joint with bolt；
It is weight 1 that cement and sand, which are pressed,：2 concrete is encased in inside solid rocket motor case, concrete height and steel plate
Flush, treat concrete curing；
The present invention is when carrying out the axis pulling experiment of solid rocket motor case skirt, and one end of end frame is fixed, and solid-rocket is sent out
Motivation housing skirt imposed load.
The present invention both may apply to solid rocket motor case list skirt or double skirt axis pulling experiments, can also be applied to solid
The inconsistent axis pulling experiment of the forward and backward skirt stand under load of body rocket engine cast.The present invention proves feasible by experiment, obtains solid
The axle of rocket engine cast skirt draws load.
Claims (3)
1. a kind of device of solid rocket motor case list skirt axis pulling experiment, including end frame assembly（1）, solid-rocket starts
Casing body（2）And concrete（4）, it is characterised in that：
Described end frame assembly（1）Including end frame（5）, round steel（6）And steel plate（8）, hold frame（5）Upper end on the outside of with solid fire
Arrow motor body（2）Connecting socket correspondence position be provided with multiple through holes, hold frame（5）Upper end on the outside of through hole be used for lead to
Cross bolt（3）By end frame（5）With solid rocket motor case（2）Joint link together, hold frame（5）Upper end on the inside of
Multiple circular holes are furnished with, frame is held（5）Upper end on the inside of circular hole be used for threaded round steel（6）Fixed to end frame（5）Upper end
On the circular hole of inner side, frame is held（5）Lower end outside be provided with multiple through holes, hold frame（5）Lower end outside through hole be used for pass through spiral shell
Bolt is by end frame（5）Fixed with testing stand；Described round steel（6）Two ends are provided with screw thread, round steel（6）One end is fixed to end frame with nut
（5）Upper end on the inside of circular hole on, round steel（6）Other end nut（7）Fixation steel plate（8）；Described steel plate（8）Centre is provided with
Through hole, steel plate 8）Round steel is arranged on by through hole（6）Simultaneously use nut in one end（7）It is fixed, steel plate（8）Upper surface and solid-rocket
Motor body（2）End socket at equatorial line it is concordant；
Described solid rocket motor case（2）It is fixed on end frame assembly（1）End frame（5）On, solid-rocket hair
Motivation housing（2）Inside loads concrete（4）, concrete（4）Height and steel plate（8）Upper surface flush.
2. device according to claim 1, it is characterised in that：Described end frame（5）Material be high-strength steel.
3. device according to claim 1, it is characterised in that：Described solid rocket motor case（2）For metal material
Material or composite.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611083786.3A CN107063840B (en) | 2016-11-30 | 2016-11-30 | Device for single skirt axial tension test of solid rocket engine shell |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611083786.3A CN107063840B (en) | 2016-11-30 | 2016-11-30 | Device for single skirt axial tension test of solid rocket engine shell |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107063840A true CN107063840A (en) | 2017-08-18 |
| CN107063840B CN107063840B (en) | 2021-11-26 |
Family
ID=59618691
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611083786.3A Active CN107063840B (en) | 2016-11-30 | 2016-11-30 | Device for single skirt axial tension test of solid rocket engine shell |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107063840B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114184386A (en) * | 2021-11-29 | 2022-03-15 | 西安航天动力测控技术研究所 | Spherical solid rocket engine testing arrangement |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114184386A (en) * | 2021-11-29 | 2022-03-15 | 西安航天动力测控技术研究所 | Spherical solid rocket engine testing arrangement |
| CN114184386B (en) * | 2021-11-29 | 2023-07-21 | 西安航天动力测控技术研究所 | Spherical solid rocket engine testing device |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107063840B (en) | 2021-11-26 |
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