CN216007992U - Support frame for civil air defense engineering - Google Patents
Support frame for civil air defense engineering Download PDFInfo
- Publication number
- CN216007992U CN216007992U CN202121462304.1U CN202121462304U CN216007992U CN 216007992 U CN216007992 U CN 216007992U CN 202121462304 U CN202121462304 U CN 202121462304U CN 216007992 U CN216007992 U CN 216007992U
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- connector
- support frame
- head
- base
- air defense
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- 230000007123 defense Effects 0.000 title claims abstract description 24
- 230000001105 regulatory effect Effects 0.000 claims description 35
- 238000009434 installation Methods 0.000 claims description 11
- 238000010276 construction Methods 0.000 description 4
- 230000000630 rising effect Effects 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000000873 masking effect Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses a support frame for civil air defense engineering, which comprises a support frame body, wherein a base is arranged on the support frame body, a ball head is arranged in a ball head groove in the base, a bottom support rod is arranged in the center above the ball head, an adjusting key connector is arranged on the outer wall, close to the bottom, of the bottom support rod, an adjusting piece is arranged between the adjusting key connector and the connector on the upper surface of the base, connectors are symmetrically arranged at two ends of an adjusting block of the adjusting piece, the directions of threads in the two connectors are opposite, an adjusting block is arranged in the top end of the bottom support rod, a lifting adjusting rod is arranged on a thread head A on the adjusting block, and a top supporting head is arranged at the top end of the lifting adjusting rod.
Description
Technical Field
The utility model relates to the technical field of support frames for civil air defense engineering, in particular to a support frame for civil air defense engineering.
Background
The civil air defense engineering is an important facility for preventing enemies from attacking suddenly, effectively masking personnel and materials and preserving the war potential; the method is an engineering guarantee for adhering to town battles and supporting anti-aggression wars to victory for a long time.
With the lapse of time, the construction of civil air defense projects gradually goes up to normalized and scientific tracks, China has already built a large number of peacetime and wartime dual-purpose projects with high quality, large amplitude and good benefit, the kinds of civil air defense projects are complete, and a certain scale is formed. However, since early works built by the movement of the masses have been impressive in the mind of people in the past, many people are unaware of the current situation of civil air defense construction, and the understanding is still on the level of 70 s, and the civil air defense construction is regarded as a hole of air defense. In practice, this view is very faceted. Over the course of more than 20 years, civil air defense engineering has changed the look and image of the past.
The support frame often can be used as the pillar of safe support in the civil air defense engineering, but, the support frame that uses all is ligneous T type support or just the steel pipe directly supports at present, and this support frame that just needs to use accords with the scene of using, leads to the construction degree of difficulty to increase, and the selection of support frame is more troublesome.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a support frame for civil air defense engineering, which is convenient to use, can adjust the rising and the falling of the support frame, can also adjust the inclination angle of the support frame, and realizes good support, so as to solve the problems in the background technology.
In order to achieve the purpose, the utility model provides the following technical scheme: the utility model provides a support frame for civil air defense engineering, includes the support frame body, be equipped with the base on the support frame body, the inside of base is equipped with the bulb, the top central authorities of bulb are equipped with the mounting base, and the top central authorities of mounting base are equipped with the bottom sprag pole, bulb, mounting base and bottom sprag pole structure as an organic whole, the outer wall that the bottom sprag pole is close to the bottom is equipped with the regulating part connector, and regulating part connector and bottom sprag pole structure as an organic whole, be equipped with the regulating part between base and the regulating part connector, the inside lift adjustment spare that is equipped with in top of bottom sprag pole, the top of lift adjustment spare is equipped with the lift adjustment pole, the cooperation installation between bottom sprag pole, lift adjustment spare and the lift adjustment pole.
Preferably, the inside central authorities of base are equipped with the bulb groove, and bulb inslot portion evenly is equipped with the ball, the upper surface symmetry of base is equipped with connector A, and connector A and base structure as an organic whole, connector A's top inside is equipped with the connecting hole.
Preferably, the regulating part connector is circular, the outer wall of the regulating part connector is symmetrically provided with installation connectors, and the inside of each installation connector is provided with a connecting groove.
Preferably, be equipped with the regulating block on the regulating part, the central authorities of regulating block are equipped with the hexagon square, and the top and the below of regulating part all are equipped with connector B, the inside connecting hole that is equipped with of one end of connector B, the connecting hole runs through connector B in the horizontal direction.
Preferably, the central authorities of lift adjustment spare are equipped with the regulating block, the top of regulating block is equipped with thread head A, and the below of regulating block is equipped with thread head B, the outside lateral wall screw thread opposite direction of thread head A, thread head B.
Preferably, the inside thread groove that is equipped with in lift adjustment pole's bottom, lift adjustment pole's top is equipped with the top and holds in the palm the head, the inside of top support head is close to and evenly is equipped with the screw hole all around, and top support head and lift adjustment pole structure as an organic whole.
Compared with the prior art, the utility model has the beneficial effects that:
(1) an adjusting piece is arranged between the base and the adjusting piece connector, the inclination direction of the whole support frame body can be adjusted through the adjusting piece, so that the support frame body can be better matched with civil air defense engineering installation and use, and meanwhile, the adjusting piece can also well support the bottom support rod;
(2) a bottom support rod is arranged in the center above the mounting base, the ball head, the mounting base and the bottom support rod are of an integrated structure, the ball head is installed in a ball head groove in a matched mode, and the ball head can flexibly rotate in multiple angles in the ball head groove;
(3) the bottom supporting rod, the lifting adjusting piece and the lifting adjusting rod are installed in a matched mode, the bottom supporting rod and the lifting adjusting rod can be quickly closed or quickly separated by screwing the adjusting block, and adjusting efficiency is improved;
(4) the supporting frame body is convenient to use, the lifting and the lowering of the supporting frame can be adjusted, the inclination angle of the supporting frame can also be adjusted, good supporting is achieved, and the supporting frame is good in applicability.
Drawings
FIG. 1 is a schematic structural view of a support frame according to the present invention;
FIG. 2 is a schematic view of an adjustment member of the present invention;
fig. 3 is a schematic view of an adjusting member connector of the present invention.
In the figure: 1. a support frame body; 2. a lifting adjusting rod; 3. a top support head; 4. a lifting adjustment member; 5. an adjusting block; 6. a screw head A; 7. a screw head B; 8. an adjusting part connector; 9. an adjustment member; 10. a base; 11. a connector A; 12. a ball head groove; 13. a ball head; 14. mounting a base; 15. a connector B; 16. installing a connector; 17. a bottom support bar.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-3, the present invention provides a technical solution: the utility model provides a support frame for civil air defense engineering, includes support frame body 1, is equipped with base 10 on the support frame body 1, and the inside central authorities of base 10 are equipped with bulb groove 12, and bulb groove 12 is inside evenly to be equipped with the ball, reduces the frictional resistance between the subassembly, and the upper surface symmetry of base 10 is equipped with connector A11, and connector A11 and base 10 structure as an organic whole, the inside connecting hole that is equipped with in top of connector 10.
Be equipped with regulating part 9 between base 10 and the regulating part connector 8, be equipped with regulating part 5 on the regulating part 9, the central authorities of regulating part 5 are equipped with the hexagon square, the top and the below of regulating part 9 all are equipped with connector B15, the inside connecting hole that is equipped with of one end of connector B15, the connecting hole runs through connector B15 in the horizontal direction, can adjust the holistic incline direction of support frame body 1 through regulating part 9, make the cooperation civil air defense engineering installation that support frame body 1 can be better use, regulating part 9 also can have fine support to bottom sprag pole 17 simultaneously.
Inside lifting adjusting piece 4 that is equipped with in top of bottom sprag pole 17, the central authorities of lifting adjusting piece 4 are equipped with regulating block 5, the top of regulating block 5 is equipped with thread head A6, the below of regulating block 5 is equipped with thread head B7, thread head A6, thread head B7's outside lateral wall screw thread opposite direction, lifting adjusting piece 4's top is equipped with lift adjusting lever 2, the inside thread groove that is equipped with in bottom of lift adjusting lever 2, lift adjusting lever 2's top is equipped with top support head 3, the inside of top support head 3 is close to evenly is equipped with the screw hole all around, top support head 3 and lift adjusting lever 2 are structure as an organic whole, bottom sprag pole 17, cooperation installation between lift adjusting piece 4 and the lift adjusting lever 2, can make bottom sprag pole 17 and lift adjusting lever 2 between quick the getting close or quick part through twisting adjusting block 5, the efficiency of regulation is improved.
This support frame body 1's convenient to use can adjust the rising of support frame, reduce, also can adjust the inclination of support frame, realizes fine support, and the suitability of support holder is good.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides a support frame for civil air defense engineering, includes support frame body (1), its characterized in that: a base (10) is arranged on the support frame body (1), a ball head (13) is arranged inside the base (10), a mounting base (14) is arranged in the center above the ball head (13), a bottom support rod (17) is arranged in the center above the mounting base (14), the ball head (13), the mounting base (14) and the bottom support rod (17) are of an integrated structure, the outer wall of the bottom supporting rod (17) close to the bottom end is provided with an adjusting piece connector (8), the adjusting piece connector (8) and the bottom supporting rod (17) are of an integral structure, an adjusting piece (9) is arranged between the base (10) and the adjusting piece connector (8), a lifting adjusting piece (4) is arranged inside the top end of the bottom supporting rod (17), a lifting adjusting rod (2) is arranged above the lifting adjusting piece (4), the bottom support rod (17), the lifting adjusting piece (4) and the lifting adjusting rod (2) are installed in a matched mode.
2. The support frame for civil air defense engineering of claim 1, characterized in that: the utility model discloses a ball joint, including base (10), ball groove (12), upper surface symmetry of base (10) is equipped with connector A (11), and connector A (11) and base (10) structure as an organic whole, the inside connecting hole that is equipped with in top of connector A (11).
3. The support frame for civil air defense engineering of claim 1, characterized in that: the adjusting part connector (8) is in a circular ring shape, the outer wall of the adjusting part connector (8) is symmetrically provided with an installation connector (16), and the inside of the installation connector (16) is provided with a connecting groove.
4. The support frame for civil air defense engineering of claim 1, characterized in that: be equipped with regulating block (5) on regulating part (9), the central authorities of regulating block (5) are equipped with the hexagon square, and the top and the below of regulating part (9) all are equipped with connector B (15), the inside connecting hole that is equipped with of one end of connector B (15), connecting hole run through connector B (15) in the horizontal direction.
5. The support frame for civil air defense engineering of claim 1, characterized in that: the central authorities of lift adjustment spare (4) are equipped with regulating block (5), the top of regulating block (5) is equipped with screw thread head A (6), and the below of regulating block (5) is equipped with screw thread head B (7), the outside lateral wall screw thread opposite direction of screw thread head A (6), screw thread head B (7).
6. The support frame for civil air defense engineering of claim 1, characterized in that: the inside thread groove that is equipped with in bottom of lift adjustment pole (2), the top of lift adjustment pole (2) is equipped with top support head (3), the inside of top support head (3) is close to evenly to be equipped with the screw hole all around, and top support head (3) and lift adjustment pole (2) structure as an organic whole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121462304.1U CN216007992U (en) | 2021-06-30 | 2021-06-30 | Support frame for civil air defense engineering |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121462304.1U CN216007992U (en) | 2021-06-30 | 2021-06-30 | Support frame for civil air defense engineering |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216007992U true CN216007992U (en) | 2022-03-11 |
Family
ID=80590457
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121462304.1U Expired - Fee Related CN216007992U (en) | 2021-06-30 | 2021-06-30 | Support frame for civil air defense engineering |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216007992U (en) |
-
2021
- 2021-06-30 CN CN202121462304.1U patent/CN216007992U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20220311 |