CN207759038U - A kind of aircraft hold connector - Google Patents
A kind of aircraft hold connector Download PDFInfo
- Publication number
- CN207759038U CN207759038U CN201820140801.1U CN201820140801U CN207759038U CN 207759038 U CN207759038 U CN 207759038U CN 201820140801 U CN201820140801 U CN 201820140801U CN 207759038 U CN207759038 U CN 207759038U
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- Prior art keywords
- opposite
- cargo
- montant
- groove
- wall
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Abstract
The utility model discloses a kind of aircraft hold connectors, including cargo hold, center bottom in the cargo hold is equipped with groove, it is equipped with sliding slot on the cargo hold bottom wall of the groove both sides, matched montant is equipped in the groove, the montant upper horizontal, which runs through, cross bar, ring winding slot is equipped in the middle part of the montant, wall has been fixedly connected with steel cable at left and right sides of the ring winding slot, two one end of the steel cable far from ring winding slot are equipped with movable block, two movable block bottom ends are equipped with sliding block, two sliding blocks are arranged in matched sliding slot, two opposite one end of the sliding block are equipped with spring, the opposite one end of two springs is fixedly connected with two chute walls respectively, the opposite one end of two movable blocks is equipped with connecting rod, two opposite one end of the connecting rod are equipped with baffle.The utility model is simple in structure, can fasten different size of cargo by simple connection, it is prevented to be scattered.
Description
Technical field
The utility model is related to aircraft hold technical field more particularly to a kind of aircraft hold connectors.
Background technology
Aircraft hold refers to underdeck inner space, is mainly used to store and transport cargo.The delivered payload capability of cargo hold by
The limitation withstood forces to weight limitation, volume limitation, the limitation of hatch door size and floor, aircraft meet with air-flow in flight and easily run on the way
It winnows with a dustpan so that cargo is easily scattered in cargo hold, and existing connector is fixed with cargo hold bottom plate, is only used for the goods of fixed specific dimensions
Object does not have general applicability.
Through retrieval, Chinese patent Authorization Notice No. is that CN205952288U discloses a kind of aircraft hold inside panel connection knot
Structure includes ceiling and sidewall paneling for connecting aircraft hold, and sidewall paneling is covered on the inside of the support post of airframe, side
Siding is connect with ceiling by a L-type ceiling longeron, which is made of a crosspiece and a perpendicular section, crosspiece
Connect with ceiling by spring clip nut and bolt, the end of crosspiece is stretched into the clamp of spring clip nut, clamp bottom with
It is equipped with wide cut gasket between ceiling, titanium alloy press strip is provided on the inside of ceiling, it is vertical that perpendicular section bung rivet is fixed on support
On column, and between sidewall paneling and support post.
Existing connector has the following disadvantages：The apparatus structure is complicated, cannot be to the cargo of different volumes size
Play fastening effect so that cargo is scattered everywhere when disposable air-flow jolts, fragile cargo.
Utility model content
The purpose of this utility model is to provide a kind of aircraft hold connector, have simple in structure, passes through simple connection
The advantages of different size of cargo can be fastened, it is prevented to be scattered, solves cargo when disposable air-flow jolts and is easily scattered damage
The problem of.
According to a kind of aircraft hold connector of the utility model embodiment, including cargo hold, in the bottom end in the cargo hold
Portion is equipped with groove, and sliding slot is equipped on the cargo hold bottom wall of the groove both sides, matched montant is equipped in the groove,
The montant upper horizontal is equipped with ring winding slot, the ring winding slot left and right sides through there is cross bar in the middle part of the montant
Wall has been fixedly connected with steel cable, and two one end of the steel cable far from ring winding slot are equipped with movable block, two activities
Block bottom end is equipped with sliding block, and two sliding blocks are arranged in matched sliding slot, the opposite one end of two sliding blocks
It is equipped with spring, the opposite one end of two springs is fixedly connected with two chute walls respectively, two movable block phases
One end of the back of the body is equipped with connecting rod, and two opposite one end of the connecting rod are equipped with baffle.
Further, outer wall is equipped with a circle external screw thread on the downside of the montant, and the groove inner wall is equipped with a circle therewith
Match internal thread.
Further, two movable block tops are equipped with convex block, and two opposite middle side parts of the convex block are all provided with
There is arc groove.
Further, the cross bar both sides are arranged with one layer of Anti-slip cover.
Further, wall is equipped with one layer of rubber pad at left and right sides of the cargo hold.
Further, the steel cable is made of high-carbon steel.
The utility model has an advantageous effect in that compared with prior art：
1, fastening can be played the role of by the elastic force of spring by, which being merged with the group of baffle by movable block, clamps cargo, prevents
Only cargo is scattered because of air craft battery；Position by changing sliding block can change baffle at a distance from cargo hold side wall, to change
Clamp the volume of cargo so that the device can be suitable for the cargo of different volumes size；
2, be threadedly coupled with groove by montant so that after montant rotational angle can self-locking, easy to operation, rubber pad energy
Cushioning effect is enough played, protection cargo is without damage；The apparatus structure is simple, can be fastened by simple connection different size of
Cargo prevents it to be scattered.
Description of the drawings
Attached drawing is used to provide a further understanding of the present invention, and a part for constitution instruction, with this practicality
Novel embodiment for explaining the utility model, does not constitute limitations of the present invention together.In the accompanying drawings：
Fig. 1 be the utility model proposes a kind of aircraft hold connector structural schematic diagram；
Fig. 2 is the structure enlargement diagram of a-quadrant in Fig. 1.
In figure：1- cargo holds, 2- sliding slots, 3- baffles, 4- connecting rods, 5- sliding blocks, 6- movable blocks, 7- springs, 8- grooves, 9- circles
Arc slot, 10- convex blocks, 11- steel cables, 12- cross bars, 13- montants, 14- ring windings slot, 15- internal threads, 16- external screw threads, 17- rubbers
Rubber cushion.
Specific implementation mode
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
The every other embodiment obtained, shall fall within the protection scope of the present invention.
Referring to Fig.1-2, a kind of aircraft hold connector, including cargo hold 1, the center bottom in cargo hold 1 is equipped with groove 8, recessed
It is equipped with sliding slot 2 on 1 bottom wall of cargo hold of 8 both sides of slot, matched montant 13,13 upper horizontal of montant are equipped in groove 8
Through there is cross bar 12, easy to operation that montant 13 is made to rotate, 13 middle part of montant is equipped with ring winding slot 14, ring winding slot 14 or so
Two side has been fixedly connected with steel cable 11, and two one end of steel cable 11 far from ring winding slot 14 are equipped with movable block 6, two work
6 bottom end of motion block is equipped with sliding block 5, and two sliding blocks 5 are arranged in matched sliding slot 2, and two opposite one end of sliding block 5 are equal
Equipped with spring 7, there is reset function, the opposite one end of two springs 7 to be fixedly connected respectively with two 2 side walls of sliding slot, two work
The opposite one end of motion block 6 is equipped with connecting rod 4, and two opposite one end of connecting rod 4 are equipped with baffle 3, can fasten cargo.
13 downside outer wall of montant is equipped with a circle external screw thread 16, and 8 inner wall of groove is equipped with a matched internal thread of circle
15, two 6 tops of movable block are equipped with convex block 10, and two opposite middle side parts of convex block 10 are equipped with arc groove 9,12 liang of cross bar
Side is arranged with one layer of Anti-slip cover, increases frictional force, and 1 left and right sides wall of cargo hold is equipped with one layer of rubber pad 17, reduce cargo by
The impact arrived, steel cable 11 are made of high-carbon steel.
In use, cargo is carried in cargo hold 1 first, then according to the volume size of different cargos, cross bar 12 is held
Rotation, makes steel cable 11 be wound in ring winding slot 14 so that and baffle 3 is far from 1 side wall of cargo hold, until distance is more than cargo width,
Cargo total number is placed between 1 side wall of baffle 3 and cargo hold so that cargo side is bonded rubber pad 17, then reversely rotates horizontal
Bar 12 so that movable block 6 relatively moves under the elastic force effect of spring 7 so that baffle 3 is close to cargo and clamps, you can completes
Cargo is fixed, and when needing to take out certain side cargo, is held movement movable block 6 at the arc groove 9 of convex block 10, is kept baffle 3 separate
Cargo can be taken off；It arrives at when needing picking, rotary bar 12 makes two side shields 3 while removing, while picking, saves
The picking time.
Place is not described in detail for the utility model, is the known technology of those skilled in the art.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is appreciated that can these embodiments be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaiied
Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of aircraft hold connector, it is characterised in that：Including cargo hold (1), the center bottom in the cargo hold (1) is equipped with recessed
Slot (8) is equipped with sliding slot (2) on cargo hold (1) bottom wall of groove (8) both sides, is equipped in the groove (8) matched
Montant (13), montant (13) upper horizontal is equipped with ring winding slot through there is a cross bar (12) in the middle part of the montant (13)
(14), wall has been fixedly connected with steel cable (11) at left and right sides of the ring winding slot (14), and two steel cables (11) are far from ring
One end of shape winding slot (14) is equipped with movable block (6), and two movable block (6) bottom ends are equipped with sliding block (5), two cunnings
Block (5) is arranged in matched sliding slot (2), and two opposite one end of the sliding block (5) are equipped with spring (7), and two
The opposite one end of a spring (7) is fixedly connected with two sliding slot (2) side walls respectively, and two movable blocks (6) are opposite
One end is equipped with connecting rod (4), and two opposite one end of the connecting rod (4) are equipped with baffle (3).
2. a kind of aircraft hold connector according to claim 1, it is characterised in that：On the downside of the montant (13) on outer wall
Equipped with a circle external screw thread (16), groove (8) inner wall is equipped with a matched internal thread (15) of circle.
3. a kind of aircraft hold connector according to claim 1, it is characterised in that：Two movable block (6) tops
It is equipped with convex block (10), two opposite middle side parts of the convex block (10) are equipped with arc groove (9).
4. a kind of aircraft hold connector according to claim 1, it is characterised in that：Cross bar (12) both sides are arranged
There is one layer of Anti-slip cover.
5. a kind of aircraft hold connector according to claim 1, it is characterised in that：Wall at left and right sides of the cargo hold (1)
It is equipped with one layer of rubber pad (17).
6. a kind of aircraft hold connector according to claim 1, it is characterised in that：The steel cable (11) is by high-carbon steel
At.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820140801.1U CN207759038U (en) | 2018-01-27 | 2018-01-27 | A kind of aircraft hold connector |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820140801.1U CN207759038U (en) | 2018-01-27 | 2018-01-27 | A kind of aircraft hold connector |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207759038U true CN207759038U (en) | 2018-08-24 |
Family
ID=63182188
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820140801.1U Expired - Fee Related CN207759038U (en) | 2018-01-27 | 2018-01-27 | A kind of aircraft hold connector |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207759038U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111071451A (en) * | 2020-01-16 | 2020-04-28 | 深圳市守正航空工业有限公司 | Cargo aircraft machine carries toolbox |
-
2018
- 2018-01-27 CN CN201820140801.1U patent/CN207759038U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111071451A (en) * | 2020-01-16 | 2020-04-28 | 深圳市守正航空工业有限公司 | Cargo aircraft machine carries toolbox |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180824 Termination date: 20200127 |