CN108466804B

CN108466804B - Aerospace is got stabilising arrangement with stranded pipe clamp

Info

Publication number: CN108466804B
Application number: CN201810099840.6A
Authority: CN
Inventors: 倪惠芳
Original assignee: Individual
Current assignee: Individual
Priority date: 2018-01-31
Filing date: 2018-01-31
Publication date: 2021-03-09
Anticipated expiration: 2038-01-31
Also published as: CN108466804A

Abstract

The invention discloses a multi-strand pipeline clamping and stabilizing device for aerospace, which comprises a vertical rod and a movable seat, wherein a sliding groove is formed in the middle of the upper surface of the movable seat, a sliding block is arranged in the sliding groove in a sliding mode, a positioning block is integrally formed at the end part of the sliding block, a fixing clamp is hinged to the bottom of the movable seat, a hinged seat is fixedly arranged on the upper surface of the fixing clamp, a pin rod groove with a circular cross section is formed in the middle of the fixing clamp in a communicated mode, a pin rod is inserted into the pin rod groove, and a baffle is attached to the end part of the pin rod. The utility model discloses a pipe clamp, including the anchor rod groove, the anchor rod groove is seted up on the surface of sliding seat, the pole setting runs through the inside that gets into the sliding seat to be connected in the buffer block, the buffer block can slide in the inner chamber, the tip of buffer block simultaneously and the articulated setting of articulated seat that the fixation clamp upper surface set up, make the fixation clamp can stably press from both sides when pressing from both sides and get, through setting up the activity clamp, the pin rod that sets up simultaneously through one side rotates to one side in pin rod groove, make the activity clamp further press from both sides the pipeline tightly.

Description

Aerospace is got stabilising arrangement with stranded pipe clamp

Technical Field

The invention relates to the technical field of aerospace correlation, in particular to a multi-strand pipeline clamping and stabilizing device for aerospace.

Background

The development of aerospace industry is the result of the leap progress of scientific technology in the 20 th century and the leap forward of social production. Aerospace efforts have focused on numerous new achievements in science and technology. Although the prior aerospace activities are only the first few steps of the cradle for leaving the earth, the aerospace activities have the effects far beyond the scientific and technical field, have wide and profound influences on political, economic and military and even human social life, and are usually carried out by using various pipelines in aerospace experiments.

Disclosure of Invention

The invention aims to provide a multi-strand pipeline clamping and stabilizing device for aerospace, and aims to solve the problems in the background technology.

In order to achieve the purpose, the invention provides the following technical scheme: a multi-strand pipeline clamping and stabilizing device for aerospace comprises a vertical rod and a movable seat, wherein an inner cavity is formed in the surface of the movable seat, a buffer block is arranged in the inner cavity in a sliding mode, a sliding block is vertically welded and installed on the upper surface of the buffer block, a sliding groove is formed in the middle of the upper surface of the movable seat, a sliding block is arranged in the sliding mode inside the sliding groove, a positioning block is integrally formed at the end portion of the sliding block, a circular vertical rod groove is formed in the middle of one end of the movable seat and communicated with the inner cavity, the vertical rod penetrates through the vertical rod groove and extends into the inner cavity, the end portion of the vertical rod is welded and arranged in the middle of the lower surface of the buffer block, a fixing clamp is hinged to the bottom of the movable seat, a hinged seat is fixedly installed on the upper surface of the fixing clamp, the surface of the hinged seat and the end portion of the buffer block are hinged and, the pin rod is inserted into the pin rod groove, a baffle is attached to the end of the pin rod, a movable rod is vertically arranged on the surface of one side of the baffle, a movable groove is formed in one side of the fixing clamp, the movable rod penetrates through the movable groove and extends to the outside of the movable groove, and a movable clamp is welded to the end of the movable rod.

Preferably, the sliding seat is a square metal cavity structure, the inner wall of the inner cavity of the sliding seat is attached to the surface of the buffer block, a bearing is arranged at the part, which is tangent to the vertical rod groove, of the vertical rod, and the diameter of the vertical rod is not more than half of the width of the sliding seat.

Preferably, the spout is that the cross-section is square recess, and the both ends of this spout are airtight form, and the width of spout is the same with the width of slider, the locating piece is curved metal block structure for the upper surface, and the lower surface of this locating piece sets up with the upper surface laminating of sliding seat mutually.

Preferably, the buffer block is a concave metal block, two ends of the buffer block are respectively hinged with different fixing clamps, the fixing clamps are of arc-shaped metal clamp-shaped structures, and the height of the fixing clamps is not more than that of the movable seat.

Preferably, the inner wall of the pin rod groove is tangent to the outer surface of the pin rod, the length of the pin rod groove is smaller than the width of the fixing clamp, anti-slip threads are arranged at the end part of the pin rod, the diameter of the pin rod is the same as that of the baffle, and the baffle is a metal fixing plate with a circular section.

Preferably, the surface of movable rod and the tangent setting of the inner wall in activity groove, the length that this movable rod is greater than the length in activity groove, the activity presss from both sides totally 2, and the symmetric distribution sets up, and the cambered surface radian that this activity pressed from both sides is the same with the cambered surface radian of fixation clamp.

Compared with the prior art, the invention has the beneficial effects that:

1. a vertical rod groove is formed in the surface of the movable seat, the vertical rod penetrates into the inner part of the movable seat and is connected with the buffer block, the vertical rod provides kinetic energy, and the buffer block can slide in the inner cavity;

2. meanwhile, the end part of the buffer block is hinged with a hinge seat arranged on the upper surface of the fixed clamp, so that the fixed clamp can be stably clamped when being clamped;

3. through setting up the activity and pressing from both sides, simultaneously through the pin rod that one side set up to one side rotation of pin rod groove for the activity presss from both sides the pipeline tightly further.

Drawings

FIG. 1 is a schematic structural view of the present invention;

FIG. 2 is an enlarged view of the structure at A in FIG. 1;

fig. 3 is a schematic side sectional view of the movable seat structure of the present invention.

In the figure: 1 pole setting, 2 sliding seat, 3 spouts, 4 sliders, 5 locating blocks, 6 buffer blocks, 7 fixation clamps, 8 articulated seats, 9 pin rod grooves, 10 pin rods, 11 baffles, 12 movable grooves, 13 movable rods and 14 movable clamps.

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: a multi-strand pipeline clamping and stabilizing device for aerospace comprises a vertical rod 1 and a movable seat 2, wherein an inner cavity is formed in the surface of the movable seat 2, a buffer block 6 is arranged in the inner cavity in a sliding manner, a sliding block 4 is vertically welded and installed on the upper surface of the buffer block 6, a sliding groove 3 is formed in the middle of the upper surface of the movable seat 2, a sliding block 4 is arranged in the sliding manner in the sliding groove 3, a positioning block 5 is integrally formed at the end part of the sliding block 4, a circular vertical rod 1 groove is formed in the middle of one end of the movable seat 2, the vertical rod 1 groove is communicated with the inner cavity, the vertical rod 1 penetrates through the vertical rod 1 groove and extends into the inner cavity, the end part of the vertical rod 1 is welded and arranged in the middle of the lower surface of the buffer block 6, a fixing clamp 7 is hinged and installed at the bottom of the movable seat 2, a hinged seat 8 is fixedly installed on the upper surface of the fixing clamp 7, the surface, a pin rod 10 is inserted into the pin rod groove 9, a baffle plate 11 is attached to the end of the pin rod 10, a movable rod 13 is vertically installed on the surface of one side of the baffle plate 11, a movable groove 12 is arranged on one side of the fixed clamp 7, the movable rod 13 penetrates through the movable groove 12 and extends to the outside of the movable groove 12, and a movable clamp 14 is installed at the end of the movable rod 13 in a welding mode.

Further, as shown in fig. 1, the movable seat 2 is a square metal cavity structure, the inner wall of the inner cavity of the movable seat 2 is attached to the surface of the buffer block 6, a bearing is arranged at the cutting part of the vertical rod 1 and the groove of the vertical rod 1, and the diameter of the vertical rod 1 is not more than half of the width of the movable seat 2; the sliding chute 3 is a groove with a square section, two ends of the sliding chute 3 are sealed, the width of the sliding chute 3 is the same as that of the sliding block 4, the positioning block 5 is a metal block structure with an arc-shaped upper surface, and the lower surface of the positioning block 5 is attached to the upper surface of the movable seat 2; the pole setting groove has been seted up on the surface of sliding seat 2, and pole setting 1 runs through the inside that gets into sliding seat 2 to be connected in buffer block 6, and pole setting 1 provides kinetic energy, and buffer block 6 can slide in the inner chamber, and buffer block 6's tip is articulated with articulated seat 8 that the upper surface of fixation clamp 7 set up simultaneously and is set up, makes fixation clamp 7 can stably press from both sides when getting.

Further, as shown in fig. 2 and 3, the buffer block 6 is a concave metal block, two ends of the buffer block 6 are respectively hinged to different fixing clamps 7, each fixing clamp 7 is a metal clamp-shaped structure with an arc-shaped inner wall, the height of each fixing clamp 7 is not more than that of the corresponding movable seat 2, the inner wall of each pin rod groove 9 is tangent to the outer surface of each pin rod 10, the length of each pin rod groove 9 is smaller than the width of the corresponding fixing clamp 7, the end of each pin rod 10 is provided with anti-slip threads, the diameter of each pin rod 10 is the same as that of each baffle plate 11, each baffle plate 11 is a metal fixing plate with a circular cross section, the surface of each movable rod 13 is tangent to the inner wall of each movable groove 12, the length of each movable rod 13 is larger than that of each movable groove 12, the movable clamps 14 are 2 in total and symmetrically distributed, and the arc surfaces of the movable clamps 14 are the same as the arc surfaces of the fixing clamps 7; the movable clamp 14 is arranged, the movable clamp 4 is connected with the movable rod 13, the movable rod 13 is movably arranged inside the movable groove 12, and meanwhile, the pin rod 10 arranged on one side rotates towards one side of the pin rod groove 9, so that the movable clamp 14 further clamps the pipeline.

The working principle is as follows: the surface of the movable seat 2 is provided with a vertical rod groove, the vertical rod 1 penetrates into the interior of the movable seat 2 and is connected with the buffer block 6, the vertical rod 1 provides kinetic energy, the buffer block 6 can slide in the inner cavity, and meanwhile, the end part of the buffer block 6 is hinged with a hinge seat 8 arranged on the upper surface of the fixed clamp 7, so that the fixed clamp 7 can be stably clamped when being clamped; the movable clamp 14 is arranged, the movable clamp 4 is connected with the movable rod 13, the movable rod 13 is movably arranged inside the movable groove 12, and meanwhile, the pin rod 10 arranged on one side rotates towards one side of the pin rod groove 9, so that the movable clamp 14 further clamps the pipeline.

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 invention, the scope of which is defined in the appended claims and their equivalents.

In the description of the present invention, it is to be understood that the terms "coaxial", "bottom", "one end", "top", "middle", "other end", "upper", "one side", "top", "inner", "front", "center", "both ends", and the like, indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the referenced device or element must have a particular orientation, be constructed and operated in a particular orientation, and thus, are not to be construed as limiting the present invention.

In the present invention, unless otherwise expressly specified or limited, the terms "mounted," "disposed," "connected," "secured," "screwed" and the like are to be construed broadly, e.g., as meaning fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; the terms may be directly connected or indirectly connected through an intermediate, and may be communication between two elements or interaction relationship between two elements, unless otherwise specifically limited, and the specific meaning of the terms in the present invention will be understood by those skilled in the art according to specific situations.

Claims

1. The utility model provides a stabilising arrangement is got with stranded pipe clamp to aerospace, includes pole setting (1) and sliding seat (2), its characterized in that: the inner cavity is formed in the surface of the movable seat (2), the buffer block (6) is arranged in the inner cavity in a sliding mode, the buffer block (6) is a concave metal block, two ends of the buffer block (6) are respectively hinged with different fixing clamps (7), each fixing clamp (7) is of an arc-shaped metal clamp structure, the height of each fixing clamp (7) is not more than that of the corresponding movable seat (2), the sliding block (4) is vertically welded to the upper surface of the buffer block (6), the sliding groove (3) is formed in the middle of the upper surface of the movable seat (2), the sliding groove (3) is a groove with a square cross section, two ends of the sliding groove (3) are sealed, the width of the sliding groove (3) is the same as that of the sliding block (4), the sliding block (4) is arranged in the sliding mode in the inner cavity of the sliding groove (3), and the positioning block (5) is integrally formed at the end of the sliding block (4), the positioning block (5) is of an arc-shaped metal block structure, the lower surface of the positioning block (5) is attached to the upper surface of the movable seat (2), a round upright rod groove is formed in the middle of one end of the movable seat (2), the upright rod groove is communicated with the inner cavity, the upright rod (1) penetrates through the upright rod groove and extends into the inner cavity, the end part of the upright rod (1) is welded to the middle of the lower surface of the buffer block (6), a fixing clamp (7) is hinged to the bottom of the movable seat (2), a hinge seat (8) is fixedly mounted on the upper surface of the fixing clamp (7), the surface of the hinge seat (8) is hinged to the end part of the buffer block (6), a pin rod groove (9) with a round cross section is formed in the middle of the fixing clamp (7), a pin rod (10) is inserted into the pin rod groove (9), the tip laminating of this round pin pole (10) is equipped with baffle (11), movable rod (13) are installed to a side surface perpendicular of baffle (11), one side of fixation clamp (7) is equipped with movable groove (12), movable rod (13) run through movable groove (12) and extend to its outside, and the tip welded mounting of this movable rod (13) has movable clamp (14), the surface of movable rod (13) sets up with the inner wall of movable groove (12) is tangent, and the length of this movable rod (13) is greater than the length of movable groove (12), movable clamp (14) are total 2, and the symmetric distribution sets up, and the cambered surface radian of this movable clamp (14) is the same with the cambered surface radian of fixation clamp (7).

2. The aerospace multi-strand tube clamp stabilizer device according to claim 1, wherein: the adjustable seat (2) is a square metal cavity structure, the inner wall of an inner cavity of the adjustable seat (2) is attached to the surface of the buffer block (6), a bearing is arranged at the tangent part of the vertical rod (1) and the vertical rod groove, and the diameter of the vertical rod (1) is not more than half of the width of the adjustable seat (2).

3. The aerospace multi-strand tube clamp stabilizer device according to claim 1, wherein: the inner wall of the pin rod groove (9) is tangent to the outer surface of the pin rod (10), the length of the pin rod groove (9) is smaller than the width of the fixing clamp (7), anti-slip threads are arranged at the end part of the pin rod (10), the diameter of the pin rod (10) is the same as that of the baffle (11), and the baffle (11) is a metal fixing plate with a circular section.