CN206598991U - A kind of device for being used to adjust aero seat lifting - Google Patents
A kind of device for being used to adjust aero seat lifting Download PDFInfo
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- CN206598991U CN206598991U CN201720089835.8U CN201720089835U CN206598991U CN 206598991 U CN206598991 U CN 206598991U CN 201720089835 U CN201720089835 U CN 201720089835U CN 206598991 U CN206598991 U CN 206598991U
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- slide rail
- sliding block
- block
- seat
- adjust
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Abstract
The utility model is related to a kind of aerospace field, more particularly to a kind of device for being used to adjust aero seat lifting.The technical problems to be solved in the utility model is to provide a kind of device for being used to adjust aero seat lifting of the electric or hand regulation of energy.In order to solve the above-mentioned technical problem, the utility model provides such a device for being used to adjust aero seat lifting, includes bottom plate, seat leg, electric adjusting mechanism, stretch cord, screw, block, first sliding block etc.；Bottom base plate is symmetrically connected with seat leg, the first slide rail is symmetrically connected with the top of bottom plate, the first slide rail top is uniformly provided with screwed hole, and the first slide rail internal upper part is symmetrically connected with block, slidingtype is connected with the first sliding block on the inside of first slide rail, and the first sliding block and the first slide rail coordinate.The utility model is by being provided with electric adjusting mechanism, to solve the regulation of aircraft aero seat height, is marked to adapt to various flights, so that the need for aircraft seat adapts to different height pilots.
Description
Technical field
The utility model is related to a kind of aerospace field, more particularly to a kind of dress for being used to adjust aero seat lifting
Put.
Background technology
The development of Aero-Space cause is the science and technology leap progress of 20th century, the result that social production is advanced by leaps and bounds.Boat
The achievement of empty space flight has concentrated numerous New TownMovements of science and technology.Aerospace operations so far, although be also the mankind
Initial several steps of this cradle of the earth are left, but its effect is far beyond science and technology field, to politics, economic, military affairs
So that human society life is all generated extensively and far-reaching influence.
In aviation field, aircraft aero seat adjusting means is marked to adapt to various flights, can reach adjustment seat
The height and position of chair position, i.e. seat, so that the need for aircraft seat adapts to different height pilots.And can be in the electricity of driving first
, can be by adjusting aero seat manually, so as to realize that pilot is operated and passed in and out flight in the case that machine is powered off
Device, it is ensured that pilot escapes in accident.
Therefore need a kind of device for being used to adjust aero seat lifting of the electric or hand regulation of energy of research and development badly, overcome existing
In technology can not electric or hand regulation shortcoming.
Utility model content
（1）The technical problem to be solved
The utility model in order to overcome in the prior art can not electric or hand regulation shortcoming, the utility model will solve
Technical problem be to provide it is a kind of can electric or hand regulation the device for being used to adjust aero seat lifting.
（2）Technical scheme
In order to solve the above-mentioned technical problem, the utility model provides such a dress for being used to adjust aero seat lifting
Put, include bottom plate, seat leg, electric adjusting mechanism, stretch cord, screw, block, the first sliding block, support block, seat, backrest,
Manual adjustment means and the first slide rail, bottom base plate are symmetrically connected with the top of seat leg, bottom plate and are symmetrically connected with the first slide rail, the
One slide rail top is uniformly provided with screwed hole, and the first slide rail internal upper part is symmetrically connected with slidingtype connection on the inside of block, the first slide rail
There is the first sliding block, the first sliding block and the first slide rail coordinate, and bottom base plate center is connected with the outside of electric adjusting mechanism, the first slide rail
Top is connected with stretch cord, and stretch cord bottom is connected with screw, and the first slider top center is connected with the top of support block, support block
Seat is connected with, seat top left side is connected with the outside of backrest, the slide rail of left side first and is connected with manual adjustment means.
Preferably, electric adjusting mechanism include the first motor, crank, connecting rod, the second slide rail, push rod, the second sliding block and
Roller, the first slider bottom center is connected with push rod, and bottom plate top center is provided with the first motor, the output shaft of the first motor
Crank is connected with, the first slide rail lower inside on right side is connected with slidingtype on the second slide rail, the second slide rail and is connected with the second cunning
Block, the second sliding block and the second slide rail coordinate, and rotary type is connected with connecting rod, the second sliding block between crank bottom on front side of the second sliding block
Top is connected with roller, and roller is contacted with push rod bottom.
Preferably, manual adjustment means include fixed plate, bearing block, nut, guide pin bushing, guide rail, bull stick and screw mandrel, left side
It is arranged with the left of being provided with the outside of first slide rail in fixed plate, fixed plate between bearing block, bearing block and is connected with screw mandrel, on screw mandrel
Slidingtype is connected with nut, and nut coordinates with screw mandrel, and bearing block right-hand member is provided with slidingtype on guide rail, guide rail and is connected with guide pin bushing, leads
Set coordinates with guide rail, and guide pin bushing is connected with nut, and guide pin bushing right-hand member is connected with the first sliding block left end.
Preferably, pedal is also included, the first slide rail of right-hand member outer lower portion is provided with pedal.
Preferably, also include and slipmat is provided with the top of slipmat, pedal.
Preferably, the first motor is servomotor.
Operation principle：During using the present apparatus, astronaut is allowed to be sitting on seat first, when needing to be adjusted up the height of seat
When, the first sliding block and support block are driven by electric adjusting mechanism to up and down motion, and then support block promotes seat above and below
First sliding block, after lower regulation is to required height upwards, is fixed in corresponding screwed hole by motion by the screw on both sides
, fixation can be played, when needing regulation height in the event of a power failure, you can by manual adjustment means come band
Dynamic first sliding block and support block are to up and down motion, and then support block promotes seat to up and down motion, is adjusted when lower upwards to required
After height, the first sliding block is fixed in corresponding screwed hole again by the screw on both sides, plays fixation.Such as
This, it becomes possible to realization can also adjust the height of seat in the event of a power failure.
Because electric adjusting mechanism includes the first motor, crank, connecting rod, the second slide rail, push rod, the second sliding block and rolling
Wheel, the first slider bottom center is connected with push rod, and bottom plate top center, which is provided with the first motor, the output shaft of the first motor, to be connected
Crank is connected to, the first slide rail lower inside on right side is connected with slidingtype on the second slide rail, the second slide rail and is connected with the second sliding block,
Second sliding block and the second slide rail coordinate, and rotary type is connected with connecting rod, the second sliding block top between crank bottom on front side of the second sliding block
Portion is connected with roller, and roller is contacted with push rod bottom, and the first motor of control is rotated counterclockwise, and the first motor drivening rod is counterclockwise
Rotate, connecting rod promotes the second sliding block and roller to be moved upwards in the second slide rail, and then roller promotes push rod to move upwards, push rod is pushed away
Dynamic first sliding block and support block are moved upwards on the first slide rail, are pulled when the first motor drivening rod is rotated counterclockwise to connecting rod
When second sliding block is moved downward, the second sliding block drive roller move downward, when roller, which leaves, to be contacted with push rod, the first sliding block and
Support block is moved downward under gravity, after regulation is to required height up and down, and the first motor of control is stopped, then passes through
First sliding block is fixed in corresponding screwed hole by the screw on both sides.
Because manual adjustment means include fixed plate, bearing block, nut, guide pin bushing, guide rail, bull stick and screw mandrel, left side
It is arranged with the left of being provided with the outside of one slide rail in fixed plate, fixed plate between bearing block, bearing block and is connected with screw mandrel, it is sliding on screw mandrel
Dynamic formula is connected with nut, and nut coordinates with screw mandrel, and bearing block right-hand member is provided with slidingtype on guide rail, guide rail and is connected with guide pin bushing, guide pin bushing
Coordinate with guide rail, guide pin bushing is connected with nut, and guide pin bushing right-hand member is connected with the first sliding block left end, hold bull stick and rotate clockwise,
Bull stick drives screw mandrel to rotate clockwise, and then screw mandrel drives nut to move upwards, and nut drives guide pin bushing to be moved upwards on guide rail,
And then guide pin bushing drives the first sliding block to move upwards, the first sliding block drives support block to move upwards, rotates counterclockwise bull stick, bull stick band
Dynamic screw mandrel is rotated counterclockwise, and then screw mandrel drives nut to move downward, and nut drives guide pin bushing to be moved downward on guide rail, and then leads
Set drives the first sliding block to move downward, and the first sliding block drives support block to move downward, and so repeatedly, regulates up and down after height,
Stop operating bull stick, then is fixed on the first sliding block in corresponding screwed hole by the screw on both sides.
Because also including pedal, the first slide rail of right-hand member outer lower portion is provided with pedal, and pin can be placed on by astronaut
On pedal, the comfort level of this equipment is improved.
Because also including slipmat, slipmat is provided with the top of pedal, can prevent from skidding, improve the safety of this equipment
Property.
Because the first motor is servomotor, it is more convenient to adjust its rotating speed, makes its operation more accurate.
（3）Beneficial effect
The utility model is by being provided with electric adjusting mechanism, to solve the regulation of aircraft aero seat height, be in order to
Adapting to various flights will mark, so that the need for aircraft seat adapts to different height pilots, and be provided with manual adjustment means,
The regulation of aircraft aero seat height can be also solved in the event of a power failure, the need for adapting to different height pilots, and
Slipmat is provided with the footrests, can be prevented from skidding, be improved the security of this equipment.
Brief description of the drawings
Fig. 1 is the first main structure diagram of the present utility model.
Fig. 2 is the mplifying structure schematic diagram of the utility model electric adjusting mechanism.
Fig. 3 is the main structure diagram of the utility model manual adjustment means.
Fig. 4 is second of main structure diagram of the present utility model.
Mark in accompanying drawing for：1- bottom plates, 2- seat legs, 3- electric adjusting mechanisms, the motors of 301- first, 302- cranks,
303- connecting rods, the slide rails of 304- second, 305- push rods, the sliding blocks of 306- second, 307- rollers, 4- screwed holes, 5- stretch cords, 6- spiral shells
Nail, 7- blocks, the sliding blocks of 8- first, 9- support blocks, 10- seats, 11- backrests, 12- manual adjustment means, 121- fixed plates, 122-
Bearing block, 123- nuts, 124- guide pin bushings, 125- guide rails, 126- bull sticks, 127- screw mandrels, the slide rails of 13- first, 14- pedals, 15-
Slipmat.
Embodiment
The utility model is further described with reference to the accompanying drawings and examples.
Embodiment 1
A kind of device for being used to adjust aero seat lifting, as Figure 1-4, includes bottom plate 1, seat leg 2, electric adjustable
Save mechanism 3, stretch cord 5, screw 6, block 7, the first sliding block 8, support block 9, seat 10, backrest 11, the and of manual adjustment means 12
First slide rail 13, the bottom symmetrical of bottom plate 1 is connected with seat leg 2, and the top of bottom plate 1 is symmetrically connected with the first slide rail 13, the first slide rail
13 tops are uniformly provided with screwed hole 4, and the internal upper part of the first slide rail 13 is symmetrically connected with block 7, and the inner side slidingtype of the first slide rail 13 connects
The first sliding block 8 is connected to, the first sliding block 8 coordinates with the first slide rail 13, and the bottom centre of bottom plate 1 is connected with electric adjusting mechanism 3, first
The outer upper of slide rail 13 is connected with stretch cord 5, and the bottom of stretch cord 5 is connected with screw 6, and the top center of the first sliding block 8 is connected with branch
Bracer 9, the top of support block 9 is connected with seat 10, and the top left side of seat 10 is connected with backrest 11, and the outside of the first slide rail of left side 13 connects
It is connected to manual adjustment means 12.
Embodiment 2
A kind of device for being used to adjust aero seat lifting, as Figure 1-4, includes bottom plate 1, seat leg 2, electric adjustable
Save mechanism 3, stretch cord 5, screw 6, block 7, the first sliding block 8, support block 9, seat 10, backrest 11, the and of manual adjustment means 12
First slide rail 13, the bottom symmetrical of bottom plate 1 is connected with seat leg 2, and the top of bottom plate 1 is symmetrically connected with the first slide rail 13, the first slide rail
13 tops are uniformly provided with screwed hole 4, and the internal upper part of the first slide rail 13 is symmetrically connected with block 7, and the inner side slidingtype of the first slide rail 13 connects
The first sliding block 8 is connected to, the first sliding block 8 coordinates with the first slide rail 13, and the bottom centre of bottom plate 1 is connected with electric adjusting mechanism 3, first
The outer upper of slide rail 13 is connected with stretch cord 5, and the bottom of stretch cord 5 is connected with screw 6, and the top center of the first sliding block 8 is connected with branch
Bracer 9, the top of support block 9 is connected with seat 10, and the top left side of seat 10 is connected with backrest 11, and the outside of the first slide rail of left side 13 connects
It is connected to manual adjustment means 12.
Electric adjusting mechanism 3 includes the first motor 301, crank 302, connecting rod 303, the second slide rail 304, push rod 305,
Two sliding blocks 306 and roller 307, the bottom centre of the first sliding block 8 are connected with push rod 305, and the top center of bottom plate 1 is provided with the first motor
301, crank 302 is connected with the output shaft of the first motor 301, and the lower inside of the first slide rail 13 on right side is connected with the second slide rail
304, slidingtype is connected with the second sliding block 306 on the second slide rail 304, and the second sliding block 306 coordinates with the second slide rail 304, and second slides
Rotary type is connected with connecting rod 303 between the front side of block 306 and the bottom of crank 302, and the top of the second sliding block 306 is connected with roller 307, rolled
Wheel 307 is contacted with the bottom of push rod 305.
Embodiment 3
A kind of device for being used to adjust aero seat lifting, as Figure 1-4, includes bottom plate 1, seat leg 2, electric adjustable
Save mechanism 3, stretch cord 5, screw 6, block 7, the first sliding block 8, support block 9, seat 10, backrest 11, the and of manual adjustment means 12
First slide rail 13, the bottom symmetrical of bottom plate 1 is connected with seat leg 2, and the top of bottom plate 1 is symmetrically connected with the first slide rail 13, the first slide rail
13 tops are uniformly provided with screwed hole 4, and the internal upper part of the first slide rail 13 is symmetrically connected with block 7, and the inner side slidingtype of the first slide rail 13 connects
The first sliding block 8 is connected to, the first sliding block 8 coordinates with the first slide rail 13, and the bottom centre of bottom plate 1 is connected with electric adjusting mechanism 3, first
The outer upper of slide rail 13 is connected with stretch cord 5, and the bottom of stretch cord 5 is connected with screw 6, and the top center of the first sliding block 8 is connected with branch
Bracer 9, the top of support block 9 is connected with seat 10, and the top left side of seat 10 is connected with backrest 11, and the outside of the first slide rail of left side 13 connects
It is connected to manual adjustment means 12.
Electric adjusting mechanism 3 includes the first motor 301, crank 302, connecting rod 303, the second slide rail 304, push rod 305,
Two sliding blocks 306 and roller 307, the bottom centre of the first sliding block 8 are connected with push rod 305, and the top center of bottom plate 1 is provided with the first motor
301, crank 302 is connected with the output shaft of the first motor 301, and the lower inside of the first slide rail 13 on right side is connected with the second slide rail
304, slidingtype is connected with the second sliding block 306 on the second slide rail 304, and the second sliding block 306 coordinates with the second slide rail 304, and second slides
Rotary type is connected with connecting rod 303 between the front side of block 306 and the bottom of crank 302, and the top of the second sliding block 306 is connected with roller 307, rolled
Wheel 307 is contacted with the bottom of push rod 305.
Manual adjustment means 12 include fixed plate 121, bearing block 122, nut 123, guide pin bushing 124, guide rail 125, bull stick
126 and screw mandrel 127, the outside of the first slide rail of left side 13 is provided with left side in fixed plate 121, fixed plate 121 and is arranged with bearing block
122, slidingtype on screw mandrel 127, screw mandrel 127 is connected between bearing block 122 and is connected with nut 123, nut 123 and screw mandrel 127
Coordinate, the right-hand member of bearing block 122 is provided with slidingtype on guide rail 125, guide rail 125 and is connected with guide pin bushing 124, and guide pin bushing 124 is matched somebody with somebody with guide rail 125
Close, guide pin bushing 124 is connected with nut 123, and the right-hand member of guide pin bushing 124 is connected with the left end of the first sliding block 8.
Embodiment 4
A kind of device for being used to adjust aero seat lifting, as Figure 1-4, includes bottom plate 1, seat leg 2, electric adjustable
Save mechanism 3, stretch cord 5, screw 6, block 7, the first sliding block 8, support block 9, seat 10, backrest 11, the and of manual adjustment means 12
First slide rail 13, the bottom symmetrical of bottom plate 1 is connected with seat leg 2, and the top of bottom plate 1 is symmetrically connected with the first slide rail 13, the first slide rail
13 tops are uniformly provided with screwed hole 4, and the internal upper part of the first slide rail 13 is symmetrically connected with block 7, and the inner side slidingtype of the first slide rail 13 connects
The first sliding block 8 is connected to, the first sliding block 8 coordinates with the first slide rail 13, and the bottom centre of bottom plate 1 is connected with electric adjusting mechanism 3, first
The outer upper of slide rail 13 is connected with stretch cord 5, and the bottom of stretch cord 5 is connected with screw 6, and the top center of the first sliding block 8 is connected with branch
Bracer 9, the top of support block 9 is connected with seat 10, and the top left side of seat 10 is connected with backrest 11, and the outside of the first slide rail of left side 13 connects
It is connected to manual adjustment means 12.
Electric adjusting mechanism 3 includes the first motor 301, crank 302, connecting rod 303, the second slide rail 304, push rod 305,
Two sliding blocks 306 and roller 307, the bottom centre of the first sliding block 8 are connected with push rod 305, and the top center of bottom plate 1 is provided with the first motor
301, crank 302 is connected with the output shaft of the first motor 301, and the lower inside of the first slide rail 13 on right side is connected with the second slide rail
304, slidingtype is connected with the second sliding block 306 on the second slide rail 304, and the second sliding block 306 coordinates with the second slide rail 304, and second slides
Rotary type is connected with connecting rod 303 between the front side of block 306 and the bottom of crank 302, and the top of the second sliding block 306 is connected with roller 307, rolled
Wheel 307 is contacted with the bottom of push rod 305.
Manual adjustment means 12 include fixed plate 121, bearing block 122, nut 123, guide pin bushing 124, guide rail 125, bull stick
126 and screw mandrel 127, the outside of the first slide rail of left side 13 is provided with left side in fixed plate 121, fixed plate 121 and is arranged with bearing block
122, slidingtype on screw mandrel 127, screw mandrel 127 is connected between bearing block 122 and is connected with nut 123, nut 123 and screw mandrel 127
Coordinate, the right-hand member of bearing block 122 is provided with slidingtype on guide rail 125, guide rail 125 and is connected with guide pin bushing 124, and guide pin bushing 124 is matched somebody with somebody with guide rail 125
Close, guide pin bushing 124 is connected with nut 123, and the right-hand member of guide pin bushing 124 is connected with the left end of the first sliding block 8.
Also include pedal 14, the outer lower portion of the first slide rail of right-hand member 13 is provided with pedal 14.
Also include slipmat 15, the top of pedal 14 is provided with slipmat 15.
First motor 301 is servomotor.
Operation principle：During using the present apparatus, astronaut is allowed to be sitting on seat 10 first, when needing to be adjusted up the height of seat
When spending, the first sliding block 8 and support block 9 are driven by electric adjusting mechanism 3 to up and down motion, and then support block 9 promotes seat
10, to up and down motion, after lower regulation is to required height upwards, are fixed on the first sliding block 8 by the screw 6 on both sides corresponding
Screwed hole 4 in, fixation can be played, when need in the event of a power failure regulation height when, you can by manual
Governor motion 12 drives the first sliding block 8 and support block 9 to up and down motion, and then support block 9 promotes seat 10 to up and down motion,
After lower regulation is to required height upwards, the first sliding block 8 is fixed on to corresponding screwed hole 4 again by the screw 6 on both sides
It is interior, play fixation.In this way, can be realized as also adjusting the height of seat in the event of a power failure.
Because electric adjusting mechanism 3 includes the first motor 301, crank 302, connecting rod 303, the second slide rail 304, push rod
305th, the second sliding block 306 and roller 307, the bottom centre of the first sliding block 8 are connected with push rod 305, and the top center of bottom plate 1 is provided with
Crank 302 is connected with one motor 301, the output shaft of the first motor 301, the lower inside of the first slide rail 13 on right side is connected with
Slidingtype is connected with the second sliding block 306 on two slide rails 304, the second slide rail 304, and the second sliding block 306 coordinates with the second slide rail 304,
Rotary type is connected with connecting rod 303 between the front side of second sliding block 306 and the bottom of crank 302, and the top of the second sliding block 306 is connected with roller
307, roller 307 is contacted with the bottom of push rod 305, and the first motor 301 of control is rotated counterclockwise, the drivening rod 303 of the first motor 301
Rotate counterclockwise, connecting rod 303 promotes the second sliding block 306 and roller 307 to be pushed away in the second motion upwards of slide rail 304, and then roller 307
Dynamic push rod 305 is moved upwards, and push rod 305 promotes the first sliding block 8 and support block 9 to be moved upwards on the first slide rail 13, when first
The drivening rod 303 of motor 301 rotate counterclockwise to connecting rod 303 pull the second sliding block 306 move downward when, the band of the second sliding block 306
Dynamic roller 307 is moved downward, and when roller 307, which leaves, to be contacted with push rod 305, the first sliding block 8 and support block 9 are under gravity
Move downward, after regulation is to required height up and down, the first motor 301 of control is stopped, then by the screw 6 on both sides by the
One sliding block 8 is fixed in corresponding screwed hole 4.
Because manual adjustment means 12 include fixed plate 121, bearing block 122, nut 123, guide pin bushing 124, guide rail 125,
Bull stick 126 and screw mandrel 127, the outside of the first slide rail of left side 13 are provided with left side in fixed plate 121, fixed plate 121 and are arranged with bearing
Slidingtype on screw mandrel 127, screw mandrel 127, which is connected with, between seat 122, bearing block 122 is connected with nut 123, nut 123 and screw mandrel
127 coordinate, and the right-hand member of bearing block 122 is provided with slidingtype on guide rail 125, guide rail 125 and is connected with guide pin bushing 124, guide pin bushing 124 and guide rail
125 coordinate, and guide pin bushing 124 is connected with nut 123, and the right-hand member of guide pin bushing 124 is connected with the left end of the first sliding block 8, hold bull stick 126 suitable
Hour hands are rotated, and bull stick 126 drives screw mandrel 127 to rotate clockwise, and then screw mandrel 127 drives nut 123 to move upwards, nut 123
Guide pin bushing 124 is driven to be moved upwards on guide rail 125, and then guide pin bushing 124 drives the first motion upwards of sliding block 8, the first sliding block 8 drives
Support block 9 is moved upwards, rotates counterclockwise bull stick 126, bull stick 126 drives screw mandrel 127 to rotate counterclockwise, and then the band of screw mandrel 127
Dynamic nut 123 is moved downward, and nut 123 drives guide pin bushing 124 to be moved downward on guide rail 125, and then guide pin bushing 124 drives first to slide
Block 8 is moved downward, and the first sliding block 8 drives support block 9 to move downward, and so repeatedly, regulates up and down after height, is stopped operating and is turned
Bar 126, then the first sliding block 8 is fixed in corresponding screwed hole 4 by the screw 6 on both sides.
Because also including pedal 14, the outer lower portion of the first slide rail of right-hand member 13 is provided with pedal 14, and astronaut can be by pin
It is placed on pedal 14, improves the comfort level of this equipment.
Because also including slipmat 15, the top of pedal 14 is provided with slipmat 15, can prevent from skidding, improve this equipment
Security.
Because the first motor 301 is servomotor, it is more convenient to adjust its rotating speed, makes its operation more accurate.
Embodiment described above only expresses preferred embodiment of the present utility model, and it describes more specific and detailed,
But therefore it can not be interpreted as the limitation to the utility model the scope of the claims.It should be pointed out that for the common of this area
For technical staff, without departing from the inventive concept of the premise, some deformations can also be made, improves and substitutes, these are all
Belong to protection domain of the present utility model.Therefore, the protection domain of the utility model patent should be determined by the appended claims.
Claims (6)
1. a kind of device for being used to adjust aero seat lifting, it is characterised in that include bottom plate（1）, seat leg（2）, it is electronic
Governor motion（3）, stretch cord（5）, screw（6）, block（7）, the first sliding block（8）, support block（9）, seat（10）, backrest
（11）, manual adjustment means（12）With the first slide rail（13）, bottom plate（1）Bottom symmetrical is connected with seat leg（2）, bottom plate（1）Top
Portion is symmetrically connected with the first slide rail（13）, the first slide rail（13）Top is uniformly provided with screwed hole（4）, the first slide rail（13）Internal upper part
It is symmetrically connected with block（7）, the first slide rail（13）Inner side slidingtype is connected with the first sliding block（8）, the first sliding block（8）Slided with first
Rail（13）Coordinate, bottom plate（1）Bottom centre is connected with electric adjusting mechanism（3）, the first slide rail（13）Outer upper is connected with bullet
Power rope（5）, stretch cord（5）Bottom is connected with screw（6）, the first sliding block（8）Top center is connected with support block（9）, support block
（9）Top is connected with seat（10）, seat（10）Top left side is connected with backrest（11）, the slide rail of left side first（13）Outside is connected
There are manual adjustment means（12）.
2. a kind of device for being used to adjust aero seat lifting according to claim 1, it is characterised in that motorized adjustment machine
Structure（3）Include the first motor（301）, crank（302）, connecting rod（303）, the second slide rail（304）, push rod（305）, the second sliding block
（306）And roller（307）, the first sliding block（8）Bottom centre is connected with push rod（305）, bottom plate（1）Top center is provided with first
Motor（301）, the first motor（301）Output shaft on be connected with crank（302）, first slide rail on right side（13）Lower inside connects
It is connected to the second slide rail（304）, the second slide rail（304）Upper slidingtype is connected with the second sliding block（306）, the second sliding block（306）With
Two slide rails（304）Coordinate, the second sliding block（306）Front side and crank（302）Rotary type is connected with connecting rod between bottom（303）, the
Two sliding blocks（306）Top is connected with roller（307）, roller（307）With push rod（305）Bottom is contacted.
3. a kind of device for being used to adjust aero seat lifting according to claim 2, it is characterised in that adjust machine manually
Structure（12）Include fixed plate（121）, bearing block（122）, nut（123）, guide pin bushing（124）, guide rail（125）, bull stick（126）With
Screw mandrel（127）, the slide rail of left side first（13）Outside is provided with fixed plate（121）, fixed plate（121）Interior left side is arranged with bearing block
（122）, bearing block（122）Between be connected with screw mandrel（127）, screw mandrel（127）Upper slidingtype is connected with nut（123）, nut
（123）With screw mandrel（127）Coordinate, bearing block（122）Right-hand member is provided with guide rail（125）, guide rail（125）Upper slidingtype is connected with guide pin bushing
（124）, guide pin bushing（124）With guide rail（125）Coordinate, guide pin bushing（124）With nut（123）Connection, and guide pin bushing（124）Right-hand member and
One sliding block（8）Left end is connected.
4. a kind of device for being used to adjust aero seat lifting according to claim 3, it is characterised in that also include pin
Pedal（14）, the slide rail of right-hand member first（13）Outer lower portion is provided with pedal（14）.
5. a kind of device for being used to adjust aero seat lifting according to claim 4, it is characterised in that also include anti-
Skidding（15）, pedal（14）Top is provided with slipmat（15）.
6. a kind of device for being used to adjust aero seat lifting according to claim 5, it is characterised in that the first motor
（301）For servomotor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720089835.8U CN206598991U (en) | 2017-01-24 | 2017-01-24 | A kind of device for being used to adjust aero seat lifting |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720089835.8U CN206598991U (en) | 2017-01-24 | 2017-01-24 | A kind of device for being used to adjust aero seat lifting |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206598991U true CN206598991U (en) | 2017-10-31 |
Family
ID=60149481
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720089835.8U Expired - Fee Related CN206598991U (en) | 2017-01-24 | 2017-01-24 | A kind of device for being used to adjust aero seat lifting |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206598991U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113955154A (en) * | 2021-12-20 | 2022-01-21 | 中国人民解放军63919部队 | Aviation/aerospace seat |
| CN117682110A (en) * | 2024-02-02 | 2024-03-12 | 四川凌空天行科技有限公司 | Small-impact return cabin seat |
-
2017
- 2017-01-24 CN CN201720089835.8U patent/CN206598991U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113955154A (en) * | 2021-12-20 | 2022-01-21 | 中国人民解放军63919部队 | Aviation/aerospace seat |
| CN113955154B (en) * | 2021-12-20 | 2022-04-15 | 中国人民解放军63919部队 | Aviation/aerospace seat |
| CN117682110A (en) * | 2024-02-02 | 2024-03-12 | 四川凌空天行科技有限公司 | Small-impact return cabin seat |
| CN117682110B (en) * | 2024-02-02 | 2024-05-07 | 四川凌空天行科技有限公司 | Small-impact return cabin seat |
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