CN214824164U - Novel appearance support mechanism is transferred to body - Google Patents
Novel appearance support mechanism is transferred to body Download PDFInfo
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- CN214824164U CN214824164U CN202120182014.5U CN202120182014U CN214824164U CN 214824164 U CN214824164 U CN 214824164U CN 202120182014 U CN202120182014 U CN 202120182014U CN 214824164 U CN214824164 U CN 214824164U
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Abstract
A novel projectile posture adjusting support mechanism comprises a first movable support, a second movable support, a fixed support, a first force rod, a second force rod, a connecting sleeve, a first threaded rod and a second threaded rod; the first movable support and the second movable support are respectively in threaded connection with the first threaded rod, the fixed support is in threaded connection with the second threaded rod, the first threaded rod and the second threaded rod are connected through the connecting sleeve, the first force rod is fixedly installed at the contact position of the first threaded rod and the connecting sleeve, and the second force rod is fixedly installed at the head end of the second threaded rod; the utility model discloses a nimble adjustment of multiple shape load gesture is favorable to solving because of the jamming between padlock and the stores pylon causes the risk of damage for the aircraft, has ensured the security of hanging dress and the reliability of equipment, has improved the efficiency of hanging dress butt joint.
Description
Technical Field
The utility model relates to an aircraft string dress load field especially relates to a novel appearance support mechanism is transferred to projectile body.
Background
Aircraft need to mount a large number of loads of different models quickly to meet the need for performing flight tasks quickly. The aircraft has various load models, the load circular taper is not uniform, and the aircraft load is not supported by the tray support. As shown in fig. 1, two groups of supports are used in cooperation, each group of supports is provided with two supports and a slide rail 02, a first support 01 can move on the slide rail 02, so as to adjust the distance between the first support 01 and a second support 03, but the first support 01 and the second support 02 cannot move and adjust at the same time, and cannot translate and adjust at the same time, which may result in that the posture of a conical load cannot be adjusted effectively and reasonably, and the following problems easily exist: when the conical projectile body is flatly placed on the tray, the front height and the rear height are inconsistent and cannot be adjusted; when the heights of the two ends of the padlock are not consistent, the padlock is easy to be blocked in the guide groove; the distances between the two ends of the padlock and the hanging rack in the vertical direction are inconsistent, and the large padlock is difficult to hang and enter the guide groove. The problem of blocking and the like in the load operation can be caused by the unbalanced load of the airplane, so that the normal operation of the airplane is influenced.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a novel appearance support mechanism is transferred to projectile body to solve the aforementioned problem that exists among the prior art.
In order to realize the purpose, the utility model discloses a technical scheme as follows:
a novel elastic posture adjusting support mechanism comprises a first movable support, a second movable support, a fixed support, a first force rod, a second force rod, a connecting sleeve and a supporting connecting rod; the support connecting rod comprises a first threaded rod and a second threaded rod; the first movable support and the second movable support are respectively in threaded connection with the first threaded rod, the fixed support is in threaded connection with the second threaded rod, the first threaded rod is connected with the second threaded rod through the connecting sleeve, the first force rod is fixedly installed at the contact position of the first threaded rod and the connecting sleeve, and the second force rod is fixedly installed at the head end of the second threaded rod.
Preferably, threaded mounting holes are formed in the first movable support and the second movable support, and threads in the mounting holes correspond to threads in the first threaded rod.
Preferably, the screw thread directions in the mounting holes of the first movable support and the second movable support are the same.
Preferably, the first movable support and the second movable support are in a face-to-face relative position in the mounting direction in the first threaded rod.
Preferably, the first force rod passes through a through hole in the first threaded rod and the connecting sleeve to lock and connect the first threaded rod with the connecting sleeve.
Preferably, the second threaded rod is clamped with the connecting sleeve, so that the second threaded rod rotates in the connecting sleeve.
Preferably, a mounting hole with threads is formed in the fixed support, and the threads are matched with the second threaded rod to enable the second threaded rod to move left and right in the mounting hole.
Preferably, a nut is arranged at the head end of the second threaded rod, and the second force rod fixedly penetrates through a through hole in the nut.
The utility model has the advantages that: the utility model discloses a novel projectile body posture-adjusting support mechanism, which can independently adjust the distance of a movable support in each support component, and can simultaneously translate two movable supports, thereby ensuring that the posture of the support can be rapidly adjusted as required; the two movable supports can only move towards or away from each other at the same time, so that the gravity center of a load can not be changed, the distance between the two ends of the padlock and the vertical direction is kept unchanged, the padlock can smoothly enter the guide groove of the hanging rack, and the clamping stagnation probability of the padlock in the guide groove is reduced; the utility model discloses a nimble adjustment of multiple shape load gesture is favorable to solving because of the jamming between padlock and the stores pylon causes the risk of damage for the aircraft, has ensured the security of hanging dress and the reliability of equipment, has improved the efficiency of hanging dress butt joint.
Drawings
FIG. 1 is a schematic diagram of a prior art pallet support structure;
in the figure, 01-a first support, 02-a sliding rail, 03-a second support;
FIG. 2 is a schematic structural view of the novel projectile attitude adjustment support assembly;
in the figure: 1-first movable support, 2-second movable support, 3-fixed support, 4-first power pole, 5-second power pole, 6-adapter sleeve, 7-support connecting rod, 71-first threaded rod, 72-second threaded rod.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more clearly understood, the present invention is further described in detail below with reference to the accompanying drawings. It should be understood that the detailed description and specific examples, while indicating the invention, are given by way of illustration only.
A novel elastic posture-adjusting support mechanism comprises two groups of support components, wherein the support components are shown in figure 2 and comprise a first movable support 1, a second movable support 2, a fixed support 3, a first force rod 4, a second force rod 5, a connecting sleeve 6 and a supporting connecting rod 7; mounting holes are formed in the middle positions of the first movable support 1, the second movable support 2 and the fixed support 3 at the same height, and threads rotating in the same direction are arranged in the mounting holes; the relative position of adapter sleeve is equipped with corresponding connector, the support connecting rod includes first threaded rod 71 and second threaded rod 72, the head end of first threaded rod is equipped with horizontal through hole, second threaded rod 72 head end is provided with the nut, be equipped with horizontal through hole on the nut. The thread of the mounting hole in the fixed support 3 corresponds to the second threaded rod 72, and the fixed support 3 is mounted on the second threaded rod 72 through the mounting hole in a threaded coupling manner, so that the fixed support can move along the second threaded rod 72; the first movable support 1 and the second movable support 2 are in a face-to-face position and are installed in the first threaded rod 71 through the installation hole in a threaded connection mode; the head end of the first threaded rod 71 is in rolling connection with the tail end of the second threaded rod 72 through the connecting sleeve 6, one end of the connecting sleeve 6 connected with the first threaded rod 71 is provided with a pair of opposite through holes, and the size and the position of the through holes are the same as those of the transverse through holes in the first threaded rod 71; the tail end of the second threaded rod 72 is clamped in the connecting sleeve and can flexibly rotate in the connecting sleeve; the first force rod 4 passes through the through hole of the connecting sleeve 6 and the transverse penetrating hole of the first threaded rod 71; the second force rod 5 passes through the transverse through-hole in the nut of the second threaded rod 72.
The working principle of the novel projectile posture adjusting support mechanism is as follows: the first force rod 4 is rotated to drive the first threaded rod 71 to rotate, the first movable support 1 and the second movable support 2 simultaneously move in the opposite direction or the reverse direction along the first threaded rod 71 along with the rotation of the first threaded rod 71, and the rotating direction of the first force rod 4 drives the moving direction of the first movable support 1 and the second movable support 2, so that the distance between the first movable support 1 and the second movable support 2 is adjusted; the second force rod drives the second threaded rod 72 to move in the mounting hole in the fixed support 3, so that the whole translation adjustment of the novel projectile posture adjusting support mechanism is realized.
Examples
The two sets of support assemblies in this embodiment are arranged in parallel in the aircraft, and the distance between the two movable supports in each support assembly and the overall translation of the movable supports can be independently adjusted through the force rods.
Through adopting the utility model discloses an above-mentioned technical scheme has obtained following profitable effect:
the utility model discloses a novel projectile body posture-adjusting support mechanism, which can independently adjust the distance of a movable support in each support component, and can simultaneously translate two movable supports, thereby ensuring that the posture of the support can be rapidly adjusted as required; the two movable supports can only move towards or away from each other at the same time, so that the gravity center of a load can not be changed, the distance between the two ends of the padlock and the vertical direction is kept unchanged, the padlock can smoothly enter the guide groove of the hanging rack, and the clamping stagnation probability of the padlock in the guide groove is reduced; the utility model discloses a nimble adjustment of multiple shape load gesture is favorable to solving because of the jamming between padlock and the stores pylon causes the risk of damage for the aircraft, has ensured the security of hanging dress and the reliability of equipment, has improved the efficiency of hanging dress butt joint.
The foregoing is only a preferred embodiment of the present invention, and it should be noted that, for those skilled in the art, a plurality of improvements and decorations can be made without departing from the principle of the present invention, and these improvements and decorations should also be viewed as the protection scope of the present invention.
Claims (8)
1. A novel elastic posture adjusting support mechanism is characterized by comprising a first movable support, a second movable support, a fixed support, a first force rod, a second force rod, a connecting sleeve and a supporting connecting rod; the support connecting rod comprises a first threaded rod and a second threaded rod; the first movable support and the second movable support are respectively in threaded connection with the first threaded rod, the fixed support is in threaded connection with the second threaded rod, the first threaded rod is connected with the second threaded rod through the connecting sleeve, the first force rod is fixedly installed at the contact position of the first threaded rod and the connecting sleeve, and the second force rod is fixedly installed at the head end of the second threaded rod.
2. The new posture adjustment support mechanism of claim 1, wherein threaded mounting holes are provided in both said first movable support and said second movable support, said threads in said mounting holes corresponding to the threads in said first threaded rod.
3. The novel projectile attitude adjustment support mechanism according to claim 2, wherein the thread direction in the mounting holes of the first movable support and the second movable support is the same.
4. The novel projectile attitude mount mechanism of claim 1, wherein said first and second traveling mounts are mounted in said first threaded rod in face-to-face relative positions.
5. The novel projectile attitude adjustment mount mechanism of claim 1, wherein said first force rod passes through a bore connecting said first threaded rod and said connecting sleeve, lockingly connecting said first threaded rod to said connecting sleeve.
6. The novel projectile attitude adjustment support mechanism according to claim 1, wherein the second threaded rod is engaged with the connection sleeve so that the second threaded rod rotates in the connection sleeve.
7. The novel projectile attitude adjustment support mechanism according to claim 1, wherein a mounting hole with threads is formed in the fixed support, and the threads are matched with the second threaded rod to enable the second threaded rod to move left and right in the mounting hole.
8. The new posture adjustment support mechanism of claim 1, wherein a nut is provided at the head end of said second threaded rod, and said second force rod is fixedly passed through a through hole in said nut.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120182014.5U CN214824164U (en) | 2021-01-22 | 2021-01-22 | Novel appearance support mechanism is transferred to body |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120182014.5U CN214824164U (en) | 2021-01-22 | 2021-01-22 | Novel appearance support mechanism is transferred to body |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214824164U true CN214824164U (en) | 2021-11-23 |
Family
ID=78953099
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120182014.5U Active CN214824164U (en) | 2021-01-22 | 2021-01-22 | Novel appearance support mechanism is transferred to body |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214824164U (en) |
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2021
- 2021-01-22 CN CN202120182014.5U patent/CN214824164U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A new attitude adjusting support mechanism of projectile body Effective date of registration: 20220218 Granted publication date: 20211123 Pledgee: Bank of China Limited Beijing Capital Airport sub branch Pledgor: BEIJING ANDAWELL AVIATION EQUIPMENT Co.,Ltd. Registration number: Y2022110000035 |
|
| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20230804 Granted publication date: 20211123 Pledgee: Bank of China Limited Beijing Capital Airport sub branch Pledgor: BEIJING ANDAWELL AVIATION EQUIPMENT Co.,Ltd. Registration number: Y2022110000035 |