CN208360506U - One kind taking off seat lock ring mechanism - Google Patents
One kind taking off seat lock ring mechanism Download PDFInfo
- Publication number
- CN208360506U CN208360506U CN201821033850.1U CN201821033850U CN208360506U CN 208360506 U CN208360506 U CN 208360506U CN 201821033850 U CN201821033850 U CN 201821033850U CN 208360506 U CN208360506 U CN 208360506U
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- CN
- China
- Prior art keywords
- motor
- mounting base
- screw rod
- threaded screw
- safety belt
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- Expired - Fee Related
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Abstract
The utility model relates to airplane spare parts technical fields, seat lock ring mechanism is taken off more particularly to one kind, including mounting base, control switch, motor one, first safety belt, motor two, first threaded screw rod, first sliding block, motor three, fixed block, second safety belt, first lock, motor four, second threaded screw rod, second sliding block, connecting rod and the second lock, mounting base includes the first mounting base and the second mounting base, first mounting base outer surface is respectively arranged with the sliding mouth of the first rectangle and outlet from top to bottom, two cavitys are divided by partition inside first mounting base, two cavitys respectively correspond outlet and the sliding mouth of the first rectangle, it exports corresponding inside cavity and motor one is installed, the utility model is easy to install and remove, its regulatory function can be adapted for a variety of figure crowds, it is applied widely and easy to use, security performance is high, Comfort level is adjustable, meets more Man's Demands, has very strong practicability.
Description
Technical field
The utility model relates to airplane spare parts technical fields, and in particular to one kind takes off seat lock ring mechanism.
Background technique
Aircraft is one of most common tool of mankind's remote traffic.But aircraft in flight course often due to air-flow
Deng causing to pitch, passenger will fix by the safety belt on aircraft seat at this time.Aircraft seat safety belt is able to bear
6600 Ns of pulling force, plays a protective role to passenger.It, will be due in air craft battery if passenger does not fasten seat belts
Powerful inertia and leave seat, cause to wound.But since the left and right buckle of the safety belt of aircraft is the abdomen in passenger
Portion position can not be adjusted according to the physical condition of passenger, be unable to satisfy the greater demand of passenger.In addition, since aircraft rises
The seat belt mechanisms flown on seat are fixedly mounted inside seat, therefore when safety belt breaks down, it will to maintenance people
Member brings great difficulty, it is therefore necessary to a kind of aircraft safety band is studied, to improve the comfort of birdman.
Utility model content
In view of the deficiencies of the prior art, the utility model discloses one kind to take off seat lock ring mechanism, for solving
Existing armchair structure of taking off is single, and no regulatory function, comfort level is poor, the small problem of the scope of application.
Specific technical solution is as follows:
One kind taking off seat lock ring mechanism, including mounting base, control switch, motor one, the first safety belt, motor
Two, the first threaded screw rod, the first sliding block, motor three, fixed block, the second safety belt, the first lock, motor four, the second screw thread silk
Bar, the second sliding block, connecting rod and the second lock, the mounting base include the first mounting base and the second mounting base, first peace
Dress seat outer surface is respectively arranged with the sliding mouth of the first rectangle and outlet from top to bottom, is divided into two by partition inside first mounting base
A cavity, two cavitys respectively correspond outlet and the sliding mouth of the first rectangle, and the corresponding inside cavity in the outlet is equipped with motor one,
The first safety belt is arranged on the output shaft of the motor one, the corresponding inside cavity of the sliding mouth of first rectangle is equipped with motor
Two, the first threaded screw rod is fixedly installed on the output shaft of the motor two, first threaded screw rod top passes through bearing and turns
It is dynamic to be connected on the first mounting base inner wall, the first sliding block, first sliding block and first are arranged on first threaded screw rod
Threaded screw rod is connected through a screw thread, and motor three is equipped on first sliding block, and the output shaft of the motor three is turned by bearing
Dynamic to be arranged on fixed block, the fixed block is fixed on the first sliding block, is arranged with second on three output shaft of motor
Safety belt, second mounting base outer surface are disposed with the sliding mouth of the second rectangle and first from top to bottom and latch, and described second
It is fixedly installed with motor four inside mounting base, is fixedly installed the second threaded screw rod on four output shaft of motor, described second
Threaded screw rod top is rotatably connected on the second mounting base inner wall by bearing, and is arranged on second threaded screw rod
Two sliding blocks, second sliding block are connected through a screw thread with second threaded screw rod, and second sliding block top is fixedly installed
Connecting rod, the connecting rod top are rotatably connected to the second lock by bearing；
Preferably, first mounting base and the second mounting base are separately mounted to the left and right sides of aircraft seat backrest, institute
It is mountable on the handrail of aircraft seat to state control switch；
Preferably, the control switch is electrically connected with motor one, motor two, motor three and motor four respectively；
Preferably, first safety belt runs through the outlet, and second safety belt is through the sliding mouth of first rectangle；
Preferably, the connecting rod extends to outside through the sliding mouth of the second rectangle.
The utility model has the advantages that
1, the utility model structure is simple, easy for installation, can quickly be mounted on the both sides of aircraft seat, is convenient for work
The detachable maintaining of personnel.
2, the length of the first safety belt of the utility model and the second safety belt is adjustable, by manipulating control switch, from
And motor one and the rotation of motor three are adjusted, to achieve the purpose that adjust belt length, the use scope of safety belt is expanded,
Suitable for the passenger of different building shape, the comfort of passenger's wearing is increased.
3, the second safety belt upper-lower height is adjustable, and the second lock height is also adjusted, and expands the second safety belt
Wearing regulative mode, can oblique shoulder wear, can also horizontal chest wear, form safe protection mechanism with the first safety belt, while
Suitable for the wearing of children, the security protection of children is increased.
Detailed description of the invention
In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment
Or attached drawing needed to be used in the description of the prior art is briefly described, it should be apparent that, the accompanying drawings in the following description is only
It is some embodiments of the utility model, for those of ordinary skill in the art, in the premise not made the creative labor
Under, it is also possible to obtain other drawings based on these drawings.
Fig. 1: seat lock ring mechanism overall structure diagram is taken off；
Fig. 2: seat lock ring mechanism the first mounting base schematic diagram of internal structure is taken off；
Fig. 3: seat lock ring mechanism the second mounting base schematic diagram of internal structure is taken off.
Appended drawing reference is as follows: 1, mounting base, the 101, first mounting base, 1011, outlet, the sliding mouth of the 1012, first rectangle,
1013, partition, the 102, second mounting base, the sliding mouth of the 1021, second rectangle, 2, control switch, 3, motor one, 4, the first safety belt,
5, motor two, the 6, first threaded screw rod, the 7, first sliding block, 8, motor three, 9, fixed block, the 10, second safety belt, the 11, first lock
Button, 12, motor four, 13, the second threaded screw rod, the 14, second sliding block, 15, connecting rod, the 16, second lock.
Specific embodiment
It is practical new below in conjunction with this to keep the objectives, technical solutions, and advantages of the embodiments of the present invention clearer
Attached drawing in type embodiment, the technical scheme in the utility model embodiment is clearly and completely described, it is clear that is retouched
The embodiment stated is the utility model a part of the embodiment, instead of all the embodiments.Based on the implementation in the utility model
Example, every other embodiment obtained by those of ordinary skill in the art without making creative efforts belong to
The range of the utility model protection.
Referring to Fig. 1-3: one kind taking off seat lock ring mechanism, including mounting base 1, control switch 2, motor one 3, first
Safety belt 4, motor 25, the first threaded screw rod 6, the first sliding block 7, motor 38, fixed block 9, the second safety belt 10, first lock
11, motor 4 12, the second threaded screw rod 13, the second sliding block 14, connecting rod 15 and the second lock 16, mounting base 1 include the first peace
Seat 101 and the second mounting base 102 are filled, 101 outer surface of the first mounting base is respectively arranged with the sliding mouth 1012 of the first rectangle from top to bottom
With outlet 1011, it is divided to by partition 1013 for two cavitys inside the first mounting base 101, two cavitys respectively correspond 1011 Hes of outlet
First rectangle slides mouth 1012, and 1011 corresponding inside cavities of outlet are equipped with motor 1, are arranged on the output shaft of motor 1
First safety belt 4, the sliding corresponding inside cavity of mouth 1012 of the first rectangle are equipped with motor 25, fix on the output shaft of motor 25
It is provided with the first threaded screw rod 6,6 top of the first threaded screw rod is rotatably connected on 101 inner wall of the first mounting base by bearing, the
The first sliding block 7 is arranged on one threaded screw rod 6, the first sliding block 7 is connected through a screw thread with the first threaded screw rod 6, on the first sliding block 7
Motor 38 is installed, the output shaft of motor 38 is rotatably arranged on fixed block 9 by bearing, and fixed block 9 is fixed at
On one sliding block 7, the second safety belt 10 is arranged on 38 output shaft of motor, 102 outer surface of the second mounting base is successively set from top to bottom
It is equipped with the sliding mouth 1021 of the second rectangle and the first lock 11, is fixedly installed with motor 4 12, motor 4 12 inside the second mounting base 102
The second threaded screw rod 13 is fixedly installed on output shaft, 13 top of the second threaded screw rod is rotatably connected on the second installation by bearing
On 102 inner walls of seat, the second sliding block 14 is arranged on the second threaded screw rod 13, the second sliding block 14 and the second threaded screw rod 13 pass through spiral shell
Line connection, 14 top of the second sliding block are fixedly installed connecting rod 15, and 15 top of connecting rod is rotatably connected to the second lock by bearing
Button 16.
Specifically, the first mounting base 101 and the second mounting base 102 are separately mounted to the left and right sides of aircraft seat backrest,
Control switch 2 is mountable on the handrail of aircraft seat, control switch 2 respectively with motor 1, motor 25, motor 38 and electricity
Machine 4 12 is electrically connected, and the first safety belt 4 is through outlet 1011, and the second safety belt 10 is through the sliding mouth 1012 of the first rectangle, connection
Bar 15 extends to outside through the sliding mouth 1021 of the second rectangle.
When the utility model is used, the first mounting base 101 and the second mounting base 102 are separately mounted to aircraft seat backrest
Left and right ends, control switch 2 is mounted on the handrail of seat, when aircraft will take off, the first safety belt 4 can be locked at
In first lock 11, then the second safety belt 10 is locked in the second lock 16, passenger can moderately adjust according to itself figure
The length of two safety belts, by manipulating control switch 2, motor 1 works, to carry out appropriate length to the first safety belt 4
Degree adjustment manipulates control switch 2, and motor 38 works, to carry out appropriate length adjustment to the second safety belt 10；According to multiplying
The wearing habit of visitor, can be by manipulating control switch 2, so that motor 25 and motor 4 12 work respectively, the first screw thread silk
Bar 6 and the rotation of the second threaded screw rod 13, the first sliding block 7 slides on two threaded screw rods respectively with the second sliding block 14, to adjust
The position of whole second safety belt 10 and the second lock 16, is fixed at this point, the second safety belt 10 can be worn on front by passenger, can also
It is fixed with oblique shoulder, while increasing passenger safety, also increases comfort level.
The utility model is easy to install and remove, and regulatory function can be adapted for a variety of figure crowds, applied widely
And it is easy to use, security performance is high, and comfort level is adjustable, meets more Man's Demands, has very strong practicability.
Above embodiments are only to illustrate the technical solution of the utility model, rather than its limitations；Although referring to aforementioned reality
Example is applied the utility model is described in detail, those skilled in the art should understand that: it still can be to preceding
Technical solution documented by each embodiment is stated to modify or equivalent replacement of some of the technical features；And these
It modifies or replaces, the spirit and model of various embodiments of the utility model technical solution that it does not separate the essence of the corresponding technical solution
It encloses.
Claims (5)
1. one kind takes off seat lock ring mechanism, it is characterised in that: including mounting base (1), control switch (2), motor one
(3), the first safety belt (4), motor two (5), the first threaded screw rod (6), the first sliding block (7), motor three (8), fixed block (9),
Second safety belt (10), the first lock (11), motor four (12), the second threaded screw rod (13), the second sliding block (14), connecting rod
(15) and second lock (16), the mounting base (1) include the first mounting base (101) and the second mounting base (102), described first
Mounting base (101) outer surface is respectively arranged with the first rectangle sliding mouth (1012) and outlet (1011), first peace from top to bottom
Dress seat (101) is internal to be divided into two cavitys by partition (1013), and two cavitys respectively correspond outlet (1011) and the first rectangle is sliding
Mouthful (1012), the corresponding inside cavity of the outlet (1011) are equipped with motor one (3), on the output shaft of the motor one (3)
It is arranged with the first safety belt (4), the corresponding inside cavity of first rectangle sliding mouth (1012) is equipped with motor two (5), described
It is fixedly installed on the output shaft of motor two (5) the first threaded screw rod (6), the first threaded screw rod (6) top passes through bearing
It is rotatably connected on the first mounting base (101) inner wall, is arranged with the first sliding block (7) on first threaded screw rod (6), described
One sliding block (7) is connected through a screw thread with the first threaded screw rod (6), is equipped with motor three (8) on first sliding block (7), described
The output shaft of motor three (8) is rotatably arranged on fixed block (9) by bearing, and it is sliding that the fixed block (9) is fixed at first
On block (7), be arranged with the second safety belt (10) on motor three (8) output shaft, the second mounting base (102) outer surface from
Top to bottm is disposed with the second rectangle sliding mouth (1021) and the first lock (11), fixes inside second mounting base (102)
Motor four (12) is installed, is fixedly installed the second threaded screw rod (13) on motor four (12) output shaft, second spiral shell
Line screw rod (13) top is rotatably connected on the second mounting base (102) inner wall by bearing, second threaded screw rod
(13) it being arranged on the second sliding block (14), second sliding block (14) is connected through a screw thread with second threaded screw rod (13),
Second sliding block (14) top is fixedly installed connecting rod (15), and connecting rod (15) top is rotatably connected to by bearing
Second lock (16).
2. according to claim 1 take off seat lock ring mechanism, it is characterised in that: first mounting base (101)
The left and right sides of aircraft seat backrest is separately mounted to the second mounting base (102), the control switch (2) is mountable in aircraft
On the handrail of seat.
3. according to claim 1 take off seat lock ring mechanism, it is characterised in that: the control switch (2) is respectively
It is electrically connected with motor one (3), motor two (5), motor three (8) and motor four (12).
4. according to claim 1 take off seat lock ring mechanism, it is characterised in that: first safety belt (4) is passed through
The outlet (1011) is worn, second safety belt (10) is sliding mouth (1012) through first rectangle.
5. according to claim 1 take off seat lock ring mechanism, it is characterised in that: the connecting rod (15) is through the
Two rectangles sliding mouth (1021) extend to outside.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821033850.1U CN208360506U (en) | 2018-07-02 | 2018-07-02 | One kind taking off seat lock ring mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821033850.1U CN208360506U (en) | 2018-07-02 | 2018-07-02 | One kind taking off seat lock ring mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208360506U true CN208360506U (en) | 2019-01-11 |
Family
ID=65032945
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821033850.1U Expired - Fee Related CN208360506U (en) | 2018-07-02 | 2018-07-02 | One kind taking off seat lock ring mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208360506U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114162002A (en) * | 2021-12-18 | 2022-03-11 | 瑞安市荣邦汽车部件有限公司 | Electric seat lock catch capable of self-adjusting balance |
-
2018
- 2018-07-02 CN CN201821033850.1U patent/CN208360506U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114162002A (en) * | 2021-12-18 | 2022-03-11 | 瑞安市荣邦汽车部件有限公司 | Electric seat lock catch capable of self-adjusting balance |
| CN114162002B (en) * | 2021-12-18 | 2022-11-11 | 瑞安市荣邦汽车部件有限公司 | Electric seat lock catch capable of self-adjusting balance |
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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: 20190111 Termination date: 20190702 |