Detachable small-pipe-diameter aviation conduit linear section shape correcting device

Abstract

The utility model relates to the field of shape correction of aviation conduits, and particularly discloses a detachable small-diameter aviation conduit linear segment shape correction device which comprises a control end, one end of the control end is used for shape correction of an aviation conduit, the other end of the control end is connected with an adapter, and the adapter is further connected with a handle used for assisting shape correction. The problem of installation and shape correction of the small-pipe-diameter aviation guide pipe under the narrow area environment on an airplane on the premise that the straight-line section control requirement is met is solved. And the whole shape correcting device is convenient and rapid to disassemble and assemble and can meet different use requirements. And meanwhile, the shape correcting device is not limited to aviation hydraulic conduits, and the device can be used for achieving related requirements for installation and shape correcting of similar small-diameter conduits in all narrow space areas.

Description

TECHNICAL FIELD

[0001] The utility model relates to a shape correcting device, in particular to a detachable small pipe diameter aviation guide pipe straight line segment shape correcting device and belongs to the field of aviation guide pipe shape correction. BACKGROUND

[0002] Aviation hydraulic guide pipes are distributed in the whole aircraft body area, in some narrow space areas, aviation hydraulic guide pipes cannot be directly matched and assembled with aircraft body structure joints due to the reasons such as low bending pipe manufacturing precision, need to carry out shape correction and installation work on the hydraulic guide pipes in the on-aircraft environment. It is very difficult to carry out shape correction work on aviation hydraulic guide pipes in the narrow area on the aircraft, and the control requirements of the straight line segment of the hydraulic guide pipe are also met under the premise that the pipe type correction of the hydraulic guide pipe meets the installation requirements, so as to prevent the flat pipe nozzle from colliding with the guide pipe body due to insufficient straight line segment length, which may cause flight safety problems. Therefore, a detachable aviation guide pipe straight line segment shape correcting device is designed to realize shape correction and installation work under the premise that the small pipe diameter hydraulic guide pipe meets the straight line segment control requirements in the narrow space on the aircraft, which has important economic value. SUMMARY

[0003] In view of the problems in the prior art, the utility model provides a detachable small pipe diameter aviation guide pipe straight line segment shape correcting device.

[0004] The purpose of the utility model can be realized through the following technical schemes:

[0005] A detachable small pipe diameter aviation guide pipe straight line segment shape correcting device, comprising a control end head, one end of the control end head is used for shape correction of an aviation guide pipe, the other end is connected with an adapter, and a handle used for assisting shape correction is further connected on the adapter.

[0006] Optionally, the control end head comprises a first threaded joint and a shape correcting rod, one end of the first threaded joint is connected with the end of the shape correcting rod, and the other end of the first threaded joint is used for being connected with the adapter.

[0007] Optionally, the outer wall of the first threaded joint is further fixedly sleeved with a nut.

[0008] Optionally, an end seat is arranged at the connecting position of the shape correcting rod and the first threaded joint, the end of the end seat away from the first threaded joint is a conical surface, and the end of the shape correcting rod away from the first threaded joint is a spherical surface.

[0009] Optionally, a first threaded hole is arranged at the connecting position of the adapter and the control end head, and the first threaded hole is used for connecting and installing the first threaded joint.

[0010] Optionally, a second threaded joint is connected with the end adjacent to the first threaded hole on the adapter, and the second threaded joint is used for connecting and installing the handle.

[0011] Optionally, a third threaded hole is formed in one end of the handle, and a second threaded hole is formed in the sidewall of the other end of the handle, and the two ends of the handle are connected with the second threaded joint through the third threaded hole or the second threaded hole, respectively.

[0012] The utility model discloses beneficial effects of:

[0013] The application solves the installation and shape correction problem of small-diameter aviation conduit under the premise of meeting the straight line segment control requirement in the narrow area on the airplane. The whole shape correction device is convenient and fast to disassemble and install, and can adapt to different use requirements. Meanwhile, the shape correction device is not limited to aviation hydraulic conduit, and can be used to realize related requirements for the installation and shape correction problem of similar small-diameter conduit in all narrow space areas. BRIEF DESCRIPTION OF DRAWINGS

[0014] In order to facilitate the understanding of those skilled in the art, the utility model will be further described below in combination with the drawings.

[0015] Figure 1 It is an installation structure schematic view of the shape correction device of the utility model.

[0016] Figure 2 It is another installation structure schematic view of the shape correction device of the utility model.

[0017] Figure 3 It is a control end head structure schematic view of the utility model.

[0018] Figure 4 It is an adapter structure schematic view of the utility model.

[0019] Figure 5 It is a handle structure schematic view of the utility model.

[0020] In the drawing: 1, control end head; 2, adapter; 3, handle; 4, shape correction rod; 5, nut; 6, first threaded joint; 7, second threaded joint; 8, first threaded hole; 9, second threaded hole. DETAILED DESCRIPTION

[0021] The technical scheme of the utility model will be described clearly and completely below in combination with embodiments. Obviously, the described embodiments are only part of the embodiments of the utility model, not all the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by those skilled in the art without creative labor belong to the protection scope of the utility model.

[0022] Please refer to Figures 1-5As shown in the figure, a detachable small-diameter aviation conduit straight section shaping device includes a control end head 1, one end of the control end head 1 is used for shaping of the aviation conduit, the other end is connected with an adapter 2, and a handle 3 used for auxiliary shaping is further connected on the adapter 2. The adapter 2 is arranged so that the control end head 1 and the handle 3 are not in the same straight line, after the control end head 1 enters the inside of the narrow area on the aircraft, the handle 3 can be extended out to be held by the maintenance personnel as a force arm, thereby facilitating movement of the control end head 1.

[0023] Specifically, the control end head 1 includes a first threaded joint 6 and a shaping rod 4, one end of the first threaded joint 6 is connected with the end of the shaping rod 4, and the other end of the first threaded joint 6 is used for connection with the adapter 2. The outer wall of the first threaded joint 6 is further fixedly sleeved with a nut 5. The arrangement of the two parts of the control end head 1 can facilitate connection with the adapter 2 and achieve the shaping purpose. The arrangement of the nut 5 facilitates rotation of the first threaded joint 6 by using a wrench to turn the nut 5 when the first threaded joint 6 is connected with the adapter 2, thereby achieving threaded installation with the first threaded hole 8.

[0024] Specifically, an end seat is arranged at the connection between the shaping rod 4 and the first threaded joint 6, the end of the end seat away from the first threaded joint 6 is a conical surface, and the end of the shaping rod 4 away from the first threaded joint 6 is a spherical surface. The arrangement of the conical surface of the end seat makes the conical surface of the end seat coincide with the conduit bell mouth after the shaping rod 4 is inserted into the inside of the aviation conduit straight section, thereby ensuring that the conduit bell mouth is not damaged during in-flight shaping. The spherical surface arrangement of the end of the shaping rod 4 ensures that the conduit is not prone to abnormal deformation, bruising and other conditions during in-flight shaping.

[0025] Specifically, a first threaded hole 8 is arranged at the connection between the adapter 2 and the control end head 1, and the first threaded hole 8 is used for connection and installation of the first threaded joint 6.

[0026] Specifically, a second threaded joint 7 is connected with one end of the adapter 2 adjacent to the first threaded hole 8, and the second threaded joint 7 is used for connection and installation of the handle 3. A third threaded hole is formed in one end of the handle 3, and a second threaded hole 9 is formed in the side wall of the other end of the handle 3, and the two ends of the handle 3 can be connected with the second threaded joint 7 through the third threaded hole or the second threaded hole 9.

[0027] The handle 3 and the adapter 2 have two installation forms, the first installation form is as shown in the figure Figure 1 The third threaded hole at the end of the handle 3 is threadedly installed with the second threaded joint 7, and the second installation form is as shown in the figure Figure 2As shown, the second threaded hole 9 of the one end side wall of the handle 3 is screwed with the second threaded joint 7. Through the two kinds of installation, the handle 3 can respectively apply force upward and downward and leftward and rightward to the control end 1, and then the overall shaping of the aviation conduit can be realized, and different shaping requirements can be adapted. During use, one of the installation modes can be selected for use according to the requirements of the to-be-shaped and actual on-board operation environment, or the two modes can be alternately used.

[0028] In use, the control end 1 is screwed with the first threaded hole 8 of the adapter 2 through the first threaded joint 6, and the handle 3 is screwed with the second threaded joint 7 of the adapter 2 through the second threaded hole 9 or the third threaded hole. The diameter range of the aviation conduit suitable for the shaping device is 6-10 mm. When the straight section of the aviation conduit needs to be shaped, hold the handle 3 and insert the shaping rod 4 at one end of the control end 1 into the inside of the straight section of the aviation conduit. The shaping rod 4 is moved back and forth, rotated or forced to move in the inside of the straight section of the aviation conduit through the handle 3, or the straight section of the aviation conduit is forced to move, so that the shaping work of the straight section of the aviation conduit can be completed. After the shaping is completed, the whole device can be taken out from the on-board operation area.

[0029] The preferred embodiments of the utility model disclosed above are only used for helping to describe the utility model. The preferred embodiments do not describe all the details, and the utility model is not limited to the specific implementation mode. Obviously, according to the content of the specification, many modifications and changes can be made. The specification selects and specifically describes these embodiments, so as to better explain the principle and practical application of the utility model, so that the technical personnel in the technical field can well understand and utilize the utility model. The utility model is limited by the claims and the whole range and equivalents.

Claims

1. A detachable straight section straightening device for small-diameter aviation ducts, characterized in that, It includes a control end (1), one end of which is used for the alignment of the aviation duct, and the other end is connected to an adapter (2). The adapter (2) is also connected to a handle (3) for auxiliary alignment.

2. The detachable small-diameter aviation duct straight section straightening device according to claim 1, characterized in that, The control terminal (1) includes a first threaded connector (6) and a straightening rod (4). One end of the first threaded connector (6) is connected to the end of the straightening rod (4), and the other end of the first threaded connector (6) is used to connect to the adapter (2).

3. The detachable small-diameter aviation duct straight section straightening device according to claim 2, characterized in that, The outer wall of the first threaded connector (6) is also fixedly fitted with a nut (5).

4. The detachable small-diameter aviation duct straight section straightening device according to claim 2, characterized in that, An end seat is provided at the connection between the straightening rod (4) and the first threaded joint (6). The end of the end seat away from the first threaded joint (6) is tapered, and the end of the straightening rod (4) away from the first threaded joint (6) is spherical.

5. A detachable small-diameter aviation duct straight section straightening device according to claim 2, characterized in that, The adapter (2) is provided with a first threaded hole (8) at the connection between it and the control terminal (1). The first threaded hole (8) is used for the connection and installation of the first threaded connector (6).

6. A detachable small-diameter aviation duct straight section straightening device according to claim 5, characterized in that, The adapter (2) is connected to a second threaded connector (7) at one end adjacent to the first threaded hole (8). The second threaded connector (7) is used for connecting and installing the handle (3).

7. A detachable small-diameter aviation duct straight section straightening device according to claim 6, characterized in that, One end of the handle (3) is provided with a third threaded hole, and the other end of the side wall is provided with a second threaded hole (9). Both ends of the handle (3) can be connected to the second threaded connector (7) through the third threaded hole or the second threaded hole (9).

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