Anchoring agent retaining device
By designing an anchoring agent anti-retrogression device with a cap-shaped main body and elastic support plates, the problem of poor air expulsion during anchoring agent injection was solved, thereby improving the flight speed of the anchoring agent and the construction quality.
Patent Information
- Application Number
- CN202520623597.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-04-03
- Publication Date
- 2026-01-16
- Estimated Expiration
- 2035-04-03
AI Technical Summary
Existing anchoring agent anti-reverse devices cannot guarantee sufficient flight speed while expelling excess air, thus affecting the quality of anchoring construction.
An anchoring agent anti-retrogression device was designed, including a cap-shaped main body and elastic support plates. The elastic support plates are distributed circumferentially and inclined. The aerodynamic ring increases the windward area. Combined with the arc-shaped notch and through-hole design, the exhaust of the anchoring agent and the initial flight velocity are optimized.
It effectively removes excess air, increases the initial velocity of the anchoring agent, enhances the anchoring effect, and ensures stable injection of the anchoring agent into the working hole.
Smart Images

Figure CN223806165U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to tunnel anchor rod support technical field, concretely relates to a kind of anchoring agent stop device. BACKGROUND
[0002] In surrounding rock support engineering construction, it needs to use anchor rod to stabilize and reinforce surrounding rock, and in the prior art, when anchoring construction is carried out on a tunnel, a hole is first arranged according to construction drawings, then a drill hole device is used to drill an anchor rod hole in the surrounding rock at the hole arrangement position, and then an anchoring agent is pushed into the working hole and is blocked.The anchor rod installation device is used to install the hollow anchor rod in the anchor rod hole, and finally the handheld pistol drill is used to rotate the anchor rod nut to stir the anchor rod, so that the anchoring agent at the bottom of the hole is mixed with AB glue to be coagulated, and after waiting for 30 seconds, the handheld pistol drill is used to tighten the anchor rod nut to fix the tray.
[0003] In the actual construction process in the tunnel, in order to facilitate the installation of the anchor rod, the diameter of the anchor rod hole drilled in the design and construction is usually greater than the diameter of the anchor rod and the diameter of the anchoring agent, so that the anchoring agent is easy to slip off when being injected, which affects the overall quality of the anchoring construction.
[0004] In order to prevent the anchoring agent from slipping off when being injected, the anchoring agent tail end is generally sleeved with a stop device, for example, a push-resistance type fixing device for anchoring agent disclosed in CN204663556U, which comprises a hollow cap-shaped sleeve cap for sleeving one end of the anchoring agent bag body, and a plurality of elastic contraction fins are inclinedly extended outward at the outer end of the sleeve cap and have tension, so that the anchoring agent cannot be returned after being injected.However, the arrangement of the elastic contraction fins can ensure that the anchoring agent expels excess air when entering the working hole, but it cannot ensure sufficient flight speed when the anchoring agent is shot from the air injection pipe due to insufficient windward area. UTILITY MODEL CONTENTS
[0005] The utility model aims at solving the problem that the existing anchoring agent stop device cannot ensure sufficient flight speed while meeting the requirement of expelling excess air when the anchoring agent enters the working hole.
[0006] The technical scheme provided by the utility model is as follows: an anchoring agent stop device, comprising:
[0007] A cap-shaped main body is used for sleeving the anchoring agent.
[0008] An elastic support sheet is arranged on the outer surface of the cap-shaped main body, at least two layers are arranged, each layer is provided with a plurality of elastic support sheets and is distributed along the circumference of the cap-shaped main body, one end of each elastic support sheet is connected to the outer surface of the cap-shaped main body, and the other end is a free end and is inclined towards the bottom of the cap-shaped main body.
[0009] A pneumatic ring is arranged on the outer surface of the cover-shaped body, and the pneumatic ring is located on the side of the elastic supporting sheet facing the bottom of the cover-shaped body.
[0010] The elastic supporting sheet of each layer is arranged with a plurality of pieces and is distributed along the circumference of the cover-shaped body, so that the gap between the elastic supporting sheets can discharge excess air when the anchoring agent enters the working hole; the pneumatic ring near the bottom increases the windward area and improves the energy accumulated by the anchoring agent from the compressed air jet pipe, thereby improving the initial flight speed.
[0011] As a preferred, the outer diameter of the free end of the elastic supporting sheet of each layer is greater than the outer diameter of the pneumatic ring, which avoids the influence of the pneumatic ring on the discharge of excess air when the anchoring agent enters the working hole.
[0012] As a preferred, the inner ring of the pneumatic ring is connected to the outer surface of the cover-shaped body, and the outer ring is inclined toward the bottom of the cover-shaped body, which improves the strength of the pneumatic ring.
[0013] As a preferred, the outer diameter of the free end of the elastic supporting sheet located at the upper part is greater than the outer diameter of the free end of the elastic supporting sheet located at the lower part. The design of small upper and large lower improves the entry of the anchoring agent into the working hole and improves the flow guiding effect of the elastic supporting sheet at the upper part.
[0014] As a preferred, the adjacent elastic supporting sheets of the same layer are connected by an arc-shaped transition, so that an arc-shaped gap is formed between the adjacent elastic supporting sheets. The arc-shaped gap is used as a gap to discharge excess air when the anchoring agent enters the working hole, and also plays a role in improving the strength of the elastic supporting sheet.
[0015] As a preferred, the elastic supporting sheets of adjacent layers are staggered in the vertical direction, which increases the windward area without affecting the discharge of excess air, improves the energy accumulated by the anchoring agent from the compressed air jet pipe, and thereby improves the initial flight speed.
[0016] As a preferred, the inner surface of the cover-shaped body is provided with at least one elastic supporting ring, the outer ring of the elastic supporting ring is connected to the inner surface of the cover-shaped body, and the inner ring is inclined toward the bottom of the cover-shaped body. The structure of the elastic supporting ring similar to a reversed hook prevents the anchoring agent from being separated and discharged during the launching process.
[0017] As a preferred, a plurality of through holes are uniformly distributed on the side wall of the cover-shaped body, and the through holes are used to allow the anchoring agent to flow out of the cover-shaped body during the process of stirring the anchor rod, so as to prevent the amount of anchoring agent around the cover-shaped body at the bottom of the hole from being too small to affect the anchoring effect of the anchor rod.
[0018] As preferred, a plurality of through holes are evenly distributed on the sidewall of the cover-shaped body, and at least one circle of the through holes is arranged between the elastic supporting ring closest to the bottom of the cover-shaped body and the bottom of the cover-shaped body, so that the amount of anchoring agent between the cover-shaped body and the anchor rod is increased, and the anchoring effect of the anchor rod is improved.
[0019] Compared with the prior art, the utility model has the beneficial effects that:
[0020] The elastic supporting pieces of each layer are arranged in a plurality of pieces and are distributed along the circumference of the cover-shaped body, so that the gaps between the elastic supporting pieces can discharge excess air when the anchoring agent enters the working hole; the pneumatic ring close to the bottom increases the windward area, and improves the energy accumulated by the anchoring agent from the compressed air injection pipe, so as to improve the initial flight speed. BRIEF DESCRIPTION OF DRAWINGS
[0021] Figure 1 It is a three-dimensional schematic view of the embodiment one of the utility model;
[0022] Figure 2 It is a three-dimensional schematic view of the embodiment one of the utility model from another angle;
[0023] Figure 3 It is a front view schematic view of the embodiment one of the utility model;
[0024] Figure 4 It is Figure 3 It is a sectional view schematic view at A-A;
[0025] Figure 5 It is a bottom view schematic view of the embodiment one of the utility model;
[0026] Figure 6 It is a top view schematic view of the embodiment one of the utility model.
[0027] Mark explanation: cover-shaped body 1, through hole 11, elastic supporting piece 2, pneumatic ring 3, arc-shaped notch 4, elastic supporting ring 5. DETAILED DESCRIPTION
[0028] The specific embodiments of the utility model are further described below in combination with the drawings. It should be understood that the specific embodiments described herein are only used to illustrate and explain the utility model, and are not used to limit the utility model.
[0029] Embodiment one, an anchoring agent retreat-stop device, comprising:
[0030] Cover-shaped body 1 for being sleeved on the anchoring agent;
[0031] Elastic supporting piece 2, at least two layers are arranged, and two layers are arranged in the embodiment, such as Figures 1-4As shown, each layer is provided with six elastic supporting pieces 2 and is distributed along the circumference of the cap-shaped body 1. Figure 5 and Figure 6 As shown, the elastic supporting pieces 2 of each layer can be provided with different or same number as required. One end of each elastic supporting piece 2 is connected to the outer surface of the cap-shaped body 1, and the other end is a free end and is inclined towards the bottom of the cap-shaped body 1. The elastic supporting pieces 2 of adjacent layers are distributed staggered in the vertical direction.
[0032] A pneumatic ring 3 is provided on the outer surface of the cap-shaped body 1. The pneumatic ring 3 is located on the side of the elastic supporting piece 2 towards the bottom of the cap-shaped body 1. The outer diameter of the free end of the elastic supporting piece 2 of each layer is greater than the outer diameter of the pneumatic ring 3, further increasing the windward area and improving the energy accumulated by the anchor agent from the compressed air jet pipe, thereby improving the initial flight speed.
[0033] It should be noted that the "vertical", "up and down" and other related descriptions described herein are defined according to the placement position of the stop device as shown, and are not necessarily the direction in the actual use state. Figure 3
[0034] In use, the stop device is installed on the tail end of the anchor agent, and the elastic supporting pieces 2 are retracted when encountering the working hole to allow the entire stop device to enter the working hole. After entering the working hole, the elastic supporting pieces 2 abut against the hole wall to achieve the stop.
[0035] The material of the elastic supporting piece 2 can be ABS, photosensitive resin and rubber.
[0036] Each layer of the elastic supporting piece 2 is provided with a plurality of pieces and is distributed along the circumference of the cap-shaped body 1, so that the gap between the elastic supporting pieces 2 can discharge excess air when the anchor agent enters the working hole. The elastic supporting pieces 2 of the upper and lower layers are staggered, which does not affect the discharge of excess air, while increasing the windward area and improving the energy accumulated by the anchor agent from the compressed air jet pipe, thereby improving the initial flight speed.
[0037] The outer diameter of the free end of the elastic supporting piece 2 located at the upper part is greater than the outer diameter of the free end of the elastic supporting piece 2 located at the lower part and is greater than the diameter of the drill bit. The design of the upper small and the lower large, on the one hand, facilitates the anchor agent to enter the working hole, and on the other hand, improves the flow guiding effect of the elastic supporting piece 2 at the upper part.
[0038] The adjacent elastic supporting pieces 2 in the same layer are connected by arc transition, so that the adjacent elastic supporting pieces 2 form an arc-shaped gap 4. The arc-shaped gap 4 is used as a gap to discharge excess air when the anchor agent enters the working hole, and also plays a role in improving the strength of the elastic supporting piece 2.
[0039] The inner ring of the pneumatic ring 3 is connected to the outer surface of the cover-shaped body 1, and the outer ring is inclined toward the bottom of the cover-shaped body 1, thereby improving the strength of the pneumatic ring 3.
[0040] The inner surface of the cover-shaped body 1 is provided with at least one elastic supporting ring 5, and three elastic supporting rings 5 are arranged in the embodiment. Figure 4 As shown in the figure, the outer ring of the elastic supporting ring 5 is connected to the inner surface of the cover-shaped body 1, and the inner ring is inclined toward the bottom of the cover-shaped body 1, and the structure similar to the inverted hook of the elastic supporting ring 5 prevents the anchoring agent sleeved into the cover-shaped body 1 from being separated and discharged in the process of compressed air injection.
[0041] A plurality of through holes 11 are uniformly distributed on the side wall of the cover-shaped body 1, and the through holes 11 are used to allow the anchoring agent to flow out of the cover-shaped body 1 in the process of stirring the anchor rod, thereby preventing the anchoring agent around the cover-shaped body 1 at the bottom of the hole from being too small to affect the anchoring effect of the anchor rod.
[0042] A plurality of through holes 11 are uniformly distributed on the side wall of the cover-shaped body 1, and at least one ring of through holes 11 is arranged between the bottom of the cover-shaped body 1 and the bottom of the cover-shaped body 1. The elastic supporting ring 5 closest to the bottom of the cover-shaped body 1 improves the amount of anchoring agent between the cover-shaped body 1 and the anchor rod, thereby improving the anchoring effect of the anchor rod.
[0043] The preferred embodiments of the utility model are described in detail above in combination with the drawings, but the utility model is not limited to the specific details in the above embodiments, and various simple modifications can be made to the technical solutions of the utility model within the technical concept of the utility model, and these simple modifications all belong to the protection scope of the utility model.
Claims
1. An anchoring agent anti-backout device, characterized in that, The utility model relates to a cover-shaped main body (1) for sleeving on the outside of an anchoring agent, elastic supporting pieces (2) arranged on the outer surface of the cover-shaped main body (1), at least two layers of the elastic supporting pieces (2) being arranged, a plurality of the elastic supporting pieces (2) being arranged in each layer and being distributed along the circumference of the cover-shaped main body (1), one end of each of the elastic supporting pieces (2) being connected to the outer surface of the cover-shaped main body (1), the other end being a free end and being inclined towards the bottom of the cover-shaped main body (1), and a pneumatic ring (3) arranged on the outer surface of the cover-shaped main body (1), the pneumatic ring (3) being located on the side of the elastic supporting pieces (2) inclined towards the bottom of the cover-shaped main body (1). The outer diameter of the free end of each of the elastic supporting pieces (2) in each layer is greater than the outer diameter of the pneumatic ring (3). The inner ring of the pneumatic ring (3) is connected to the outer surface of the cover-shaped main body (1), and the outer ring is inclined towards the bottom of the cover-shaped main body (1). The outer diameter of the free end of the elastic supporting piece (2) located on the upper part is greater than the outer diameter of the free end of the elastic supporting piece (2) located on the lower part.
2. The anchoring agent retreat prevention device according to claim 1, wherein The elastic supporting pieces (2) in the same layer and adjacent to each other are connected in an arc-shaped transition manner, so that an arc-shaped gap (4) is formed between the adjacent elastic supporting pieces (2).
3. The anchoring agent retreat prevention device according to claim 1, wherein The elastic supporting pieces (2) in adjacent layers are distributed in a staggered manner in the vertical direction.
4. The anchoring agent retreat prevention device according to any one of claims 1 to 3, characterized in that The inner surface of the cover-shaped main body (1) is provided with at least one layer of elastic supporting rings (5), the outer ring of the elastic supporting ring (5) is connected to the inner surface of the cover-shaped main body (1), and the inner ring is inclined towards the bottom of the cover-shaped main body (1).
5. The anchoring agent retreat prevention device according to any one of claims 1 to 3, wherein A plurality of through holes (11) are uniformly distributed on the side wall of the cover-shaped main body (1).
6. The anchoring agent retreat prevention device according to any one of claims 1 to 3, wherein A plurality of through holes (11) are uniformly distributed on the side wall of the cover-shaped main body (1), and at least one ring of the through holes (11) is arranged between the elastic supporting ring (5) closest to the bottom of the cover-shaped main body (1) and the bottom of the cover-shaped main body (1).
7. The anchoring agent retreat prevention device according to any one of claims 1 to 3, wherein 8. The anchoring agent retreat prevention device according to any one of claims 1 to 3, wherein 9. The anchoring agent retreat prevention device according to claim 7, wherein
Citation Information
Patent Citations
Pushing away of resin anchor agent hinders formula fixing device
CN204663556U