CN108674668A - A kind of aero seat for space shuttle with shock-absorbing function - Google Patents
A kind of aero seat for space shuttle with shock-absorbing function Download PDFInfo
- Publication number
- CN108674668A CN108674668A CN201810414383.5A CN201810414383A CN108674668A CN 108674668 A CN108674668 A CN 108674668A CN 201810414383 A CN201810414383 A CN 201810414383A CN 108674668 A CN108674668 A CN 108674668A
- Authority
- CN
- China
- Prior art keywords
- seat
- fixed
- fixedly connected
- block
- damping spring
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000013016 damping Methods 0.000 claims abstract description 66
- 239000000872 buffer Substances 0.000 claims description 54
- 239000007787 solid Substances 0.000 claims description 2
- 230000003139 buffering effect Effects 0.000 abstract description 10
- 230000000694 effects Effects 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000007812 deficiency Effects 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 230000000284 resting effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/0619—Arrangements of seats, or adaptations or details specially adapted for aircraft seats with energy absorbing means specially adapted for mitigating impact loads for passenger seats, e.g. at a crash
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Seats For Vehicles (AREA)
Abstract
The present invention provides a kind of aero seat for space shuttle with shock-absorbing function, is related to air transportation field.This has the aero seat of shock-absorbing function for space shuttle, including the cabin floor being arranged below seat plate and seat plate, it is installed with cushion at the top of the seat plate, the top of the seat plate is simultaneously fixedly connected with supporting rod in front of cushion, the one end of the supporting rod far from seat plate is fixedly connected with handrail, it is movably hinged with shaft on the left of the seat plate, the outer surface of the shaft is fixedly connected with backrest, the bottom of the seat plate is fixedly connected with fixed block, and the bottom of the fixed block is fixedly connected with support leg.This has the aero seat of shock-absorbing function for space shuttle, and by the first damping spring and the second damping spring being arranged below seat plate, damping, buffering can be had the function of to seat plate by being used in conjunction with each other by the first damping spring and the second damping spring.
Description
Technical field
The present invention relates to air transportation technology field, specially a kind of aero seat for space shuttle with shock-absorbing function
Chair.
Background technology
Aero seat is the tool that rest is taken to passenger, and aero seat provides safety to birdman in during flight and relaxes
Suitable seat.To provide the bedding device that can be used for resting in long-term during flight to passenger.For have customization cockpit with
It is suitble to the long range general aviation aircraft of particular customer demand especially true.
The aero seat used on aircraft brings high-quality feeling for taking particularly important to passenger, when passenger takes, when winged
Opportunity brings discomfort when jolting to air-flow, aero seat used at present does not have the effect of damping, buffering, encountering
Strong air-flow cannot play good riding comfort when jolting.
Invention content
（One）The technical issues of solution
In view of the deficiencies of the prior art, the present invention provides a kind of aero seat for space shuttle with shock-absorbing function, solutions
The air-flow generated due to upper-level weather of having determined is jolted the problem of bringing sense of discomfort to passenger.
（Two）Technical solution
In order to achieve the above object, the present invention is achieved by the following technical programs：One kind having damping work(for space shuttle
The cabin floor being arranged below the aero seat of energy, including seat plate and seat plate, the top of the seat plate is fixed
Cushion is installed, the top of the seat plate is simultaneously fixedly connected with supporting rod in front of cushion, and the supporting rod is separate
One end of seat plate is fixedly connected with handrail, and shaft, the appearance of the shaft are movably hinged on the left of the seat plate
Face is fixedly connected with backrest, and the bottom of the seat plate is fixedly connected with fixed block, and the bottom of the fixed block is fixed
It is connected with support leg, fixed ring is provided with below the fixed block, buffer stopper, the branch are provided with below the fixed ring
The one end of support leg far from fixed block is fixedly connected through fixed ring and with the buffer stopper being arranged below fixed ring, the buffer stopper
Lower section is provided with fixed seat, and the bottom of the fixed seat is contacted with cabin floor, is fixedly connected with down at the top of the fixed seat
Cushion block is fixedly connected with the second damping spring, the described one end of second damping spring far from fixed seat at the top of the lower cushion block
It is fixedly connected with buffer stopper, the first damping spring is fixedly connected at the top of the buffer stopper, first damping spring is separate
One end of buffer stopper is fixedly connected with cushion block, and the top of the upper cushion block contacts with fixed ring, set at the top of the fixed ring
It is equipped with fixing nut, buffer bar is fixedly connected at the top of the lower cushion block, the one end of the buffer bar far from lower cushion block is successively
The fixation spiral shell being arranged through the second damping spring, buffer stopper, the first damping spring, upper cushion block and fixed ring and with fixed ring top
Box thread connects.
Preferably, the first fixed screw bar, the screw thread of the first fixed screw bar are provided with below the fixed block
End is threadedly coupled with fixed block.
Preferably, the both sides of the fixed seat are both provided with link block, two link blocks mutually close side and fixed seat
It is fixedly connected.
Preferably, the second fixed screw bar, the screw thread of the second fixed screw bar are provided with above the link block
End is threadedly coupled with link block.
Preferably, there are two the quantity of the lower cushion block, two lower cushion blocks are symmetrical arranged by central axes of fixed seat.
Preferably, there are two the quantity of the support leg, two support legs are symmetrical arranged by central axes of seat plate.
Preferably, through-hole compatible with buffer bar is offered at the top of the buffer stopper.
（Three）Advantageous effect
The present invention provides a kind of aero seats for space shuttle with shock-absorbing function.Has following advantageous effect：
1, this, which is used for space shuttle, has the aero seat of shock-absorbing function, passes through the first damping spring being arranged below seat plate
With the second damping spring, damping can be had to seat plate by being used in conjunction with each other by the first damping spring and the second damping spring
The function of buffering, can reduce air-flow and jolt to act directly on and multiply by the damping, buffering of the first damping spring and the second damping spring
With visitor, make seating that there is good comfort.
2, this, which is used for space shuttle, has the aero seat of shock-absorbing function, by the way that the first damping spring and the second damping is arranged
The buffer bar and buffer bar of spring inner ring setting are flexibly connected respectively at buffer stopper and fixed ring, and shock-absorbing seat can be improved
Stability makes seat more stablize under state of flight.
Description of the drawings
Fig. 1 is schematic structural view of the invention；
Fig. 2 is partial enlarged view at A in structure of the invention Fig. 1.
Wherein, 1 seat plate, 2 cushions, 3 supporting rods, 4 handrails, 5 shafts, 6 backrests, 7 fixed blocks, 8 first are fixed
Lead screw, 9 support legs, 10 fixed rings, 11 buffer bars, 12 fixing nuts, cushion block, 14 first damping springs, 15 second subtract on 13
Shake spring, 16 lower cushion blocks, 17 link blocks, 18 second fixed screw bars, 19 buffer stoppers, 20 fixed seats.
Specific implementation mode
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation describes, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
The embodiment of the present invention provides a kind of aero seat for space shuttle with shock-absorbing function, as shown in Figs. 1-2, packet
The cabin floor 8 of 1 lower section setting of seat plate 1 and seat plate is included, the top of seat plate 1 is installed with cushion 2, seat
The top of bottom plate 1 is simultaneously fixedly connected with supporting rod 3 positioned at the front of cushion 2, and the one end of supporting rod 3 far from seat plate 1 is fixed
It is connected with handrail 4, the left side of seat plate 1 is movably hinged with shaft 5, and the outer surface of shaft 5 is fixedly connected with backrest 6,
Backrest 6 can be adjusted in the shaft 5 being arranged by 1 left side of seat plate, and the bottom of seat plate 1 is fixedly connected with
Determine block 7, the lower section of fixed block 7 is provided with the first fixed screw bar 8, the end of thread and 7 screw thread of fixed block of the first fixed screw bar 8
Connection, the bottom of fixed block 7 are fixedly connected with support leg 9, and there are two the quantity of support leg 9, and two support legs 9 are with seat plate
1 is symmetrical arranged for central axes, and the lower section of fixed block 7 is provided with fixed ring 10, and the lower section of fixed ring 10 is provided with buffer stopper 19, branch
The buffer stopper 19 that the one end of support leg 9 far from fixed block 7 is arranged through fixed ring 10 and with 10 lower section of fixed ring is fixedly connected, and is buffered
The lower section of block 19 is provided with fixed seat 20, and the both sides of fixed seat 20 are both provided with link block 17, and two link blocks 17 are mutually close
Side is fixedly connected with fixed seat 20, and the top of link block 17 is provided with the second fixed screw bar 18, the second fixed screw bar 18
The end of thread be threadedly coupled with link block 17, by be arranged two link blocks 17 the second lead screw 18 can be facilitated to consolidate seat
It is fixed, seat can be made more to stablize, the bottom of fixed seat 20 is contacted with cabin floor 1, and the top of fixed seat 20 is fixedly connected with down
Cushion block 16, there are two the quantity of lower cushion block 16, and two lower cushion blocks 16 are symmetrical arranged with fixed seat 20 for central axes, lower cushion block 16
Top is fixedly connected with the second damping spring 15, can be subtracted by 15 damping, bufferings of the first damping spring 14 and the second damping spring
Few air-flow, which jolts, to be acted directly on passenger, so that seating is had good comfort, the second damping spring 15 is far from fixed seat
20 one end is fixedly connected with buffer stopper 19, and the top of buffer stopper 19 is fixedly connected with the first damping spring 14, the first damping bullet
The one end of spring 14 far from buffer stopper 19 is fixedly connected with upper cushion block 13, and the top of upper cushion block 13 is contacted with fixed ring 10, fixed ring
10 top is provided with fixing nut 12, and the top of lower cushion block 16 is fixedly connected with buffer bar 11, and buffer bar 11 is far from lower cushion block
16 one end sequentially pass through the second damping spring 15, buffer stopper 19, the first damping spring 14, upper cushion block 13 and fixed ring 10 and with
The fixing nut 12 that 10 top of fixed ring is arranged is threadedly coupled, and the top of buffer stopper 19 offers lead to compatible with buffer bar 11
Hole, 14 He of the first damping spring 14 and the second damping spring 15 and the first damping spring being arranged by 1 lower section of seat plate
The buffer stopper 19 being arranged between second damping spring 15, buffer stopper 19 are flexibly connected with buffer bar 11, can make buffer stopper 19 along
Buffer bar 11 is up and down, passes through the first damping spring 14, the second damping spring 15, buffer bar 11, fixed ring 10 and fixed spiral shell
Mother 12 is used in conjunction with each other and can have the function of damping, buffering to seat plate 1, effectively increases the cushion performance of seat, makes to multiply
Thing to sit on has good comfort.
Operation principle：This has the aero seat of shock-absorbing function for space shuttle, is turned by what 1 left side of solid bottom plate was arranged
Backrest 6 can be adjusted in axis 5, the first damping spring 14 and the second damping spring being arranged by 1 lower section of seat plate
15 and first buffer stopper 19 that is arranged between damping spring 14 and the second damping spring 15, buffer stopper 19 and 11 activity of buffer bar
Connection, can make buffer stopper 19 up and down along buffer bar 11, one end of buffer bar 11 is fixedly connected and buffers with lower cushion block 16
The other end of bar 11 is threadedly coupled through fixed ring 10 with fixing nut 12, passes through the first damping spring 14, the second damping spring
15, buffer bar 11, fixed ring 10 and fixing nut 12, which are used in conjunction with each other, to have the function of damping, buffering to seat plate 1,
Air-flow can be reduced by 15 damping, bufferings of the first damping spring 14 and the second damping spring jolt act directly on passenger,
Make seating that there is good comfort.
In conclusion this, which is used for space shuttle, has the aero seat of shock-absorbing function, it is arranged by 1 lower section of seat plate
First damping spring 14 and the second damping spring 15, are used in conjunction with each other by the first damping spring 14 and the second damping spring 15
There can be damping, buffering to seat plate 1, pass through the damping, buffering of the first damping spring 14 and the second damping spring 15
It air-flow can be reduced jolts and act directly on passenger, make seating that there is good comfort.
Also, this, which is used for space shuttle, has the aero seat of shock-absorbing function, by the way that the first damping spring 14 and the is arranged
The buffer bar 11 and buffer bar 11 of two damping springs, 115 inner ring setting are flexibly connected respectively at buffer stopper 19 and fixed ring 10,
The stability that shock-absorbing seat can be improved makes seat more stablize under state of flight.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
Understanding without departing from the principles and spirit of the present invention can carry out these embodiments a variety of variations, modification, replace
And modification, the scope of the present invention is defined by the appended.
Claims (7)
1. a kind of aero seat for space shuttle with shock-absorbing function, including seat plate（1）And seat plate（1）Lower section
The cabin floor of setting（8）, it is characterised in that：The seat plate（1）Top be installed with cushion（2）, the seat
Bottom plate（1）Top and be located at cushion（2）Front be fixedly connected with supporting rod（3）, the supporting rod（3）Far from seat plate
（1）One end be fixedly connected with handrail（4）, the seat plate（1）Left side be movably hinged with shaft（5）, the shaft（5）
Outer surface be fixedly connected with backrest（6）, the seat plate（1）Bottom be fixedly connected with fixed block（7）, described solid
Determine block（7）Bottom be fixedly connected with support leg（9）, the fixed block（7）Lower section be provided with fixed ring（10）, the fixation
Ring（10）Lower section be provided with buffer stopper（19）, the support leg（9）Far from fixed block（7）One end run through fixed ring（10）And
With fixed ring（10）The buffer stopper of lower section setting（19）It is fixedly connected, the buffer stopper（19）Lower section be provided with fixed seat
（20）, the fixed seat（20）Bottom and cabin floor（1）Contact, the fixed seat（20）Top be fixedly connected with underlay
Block（16）, the lower cushion block（16）Top be fixedly connected with the second damping spring（15）, second damping spring（15）Far
From fixed seat（20）One end and buffer stopper（19）It is fixedly connected, the buffer stopper（19）Top be fixedly connected with the first damping
Spring（14）, first damping spring（14）Far from buffer stopper（19）One end be fixedly connected with cushion block（13）, it is described on
Cushion block（13）Top and fixed ring（10）Contact, the fixed ring（10）Top be provided with fixing nut（12）, under described
Cushion block（16）Top be fixedly connected with buffer bar（11）, the buffer bar（11）Far from lower cushion block（16）One end sequentially pass through
Second damping spring（15）, buffer stopper（19）, the first damping spring（14）, upper cushion block（13）And fixed ring（10）And and fixed ring
（10）The fixing nut of top setting（12）It is threadedly coupled.
2. a kind of aero seat for space shuttle with shock-absorbing function according to claim 1, it is characterised in that：Institute
State fixed block（7）Lower section be provided with the first fixed screw bar（8）, the first fixed screw bar（8）The end of thread and fixation
Block（7）It is threadedly coupled.
3. a kind of aero seat for space shuttle with shock-absorbing function according to claim 1, it is characterised in that：Institute
State fixed seat（20）Both sides be both provided with link block（17）, two link blocks（17）Mutually close side and fixed seat（20）Gu
Fixed connection.
4. a kind of aero seat for space shuttle with shock-absorbing function according to claim 3, it is characterised in that：Institute
State link block（17）Top be provided with the second fixed screw bar（18）, the second fixed screw bar（18）The end of thread and company
Connect block（17）It is threadedly coupled.
5. a kind of aero seat for space shuttle with shock-absorbing function according to claim 1, it is characterised in that：Institute
State lower cushion block（16）Quantity there are two, two lower cushion blocks（16）With fixed seat（20）It is symmetrical arranged for central axes.
6. a kind of aero seat for space shuttle with shock-absorbing function according to claim 1, it is characterised in that：Institute
State support leg（9）Quantity there are two, two support legs（9）With seat plate（1）It is symmetrical arranged for central axes.
7. a kind of aero seat for space shuttle with shock-absorbing function according to claim 1, it is characterised in that：Institute
State buffer stopper（19）Top offer and buffer bar（11）Compatible through-hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810414383.5A CN108674668A (en) | 2018-05-03 | 2018-05-03 | A kind of aero seat for space shuttle with shock-absorbing function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810414383.5A CN108674668A (en) | 2018-05-03 | 2018-05-03 | A kind of aero seat for space shuttle with shock-absorbing function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108674668A true CN108674668A (en) | 2018-10-19 |
Family
ID=63802058
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810414383.5A Pending CN108674668A (en) | 2018-05-03 | 2018-05-03 | A kind of aero seat for space shuttle with shock-absorbing function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108674668A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114771843A (en) * | 2022-06-16 | 2022-07-22 | 中国飞机强度研究所 | Seat vibration damping system in aviation aircraft manufacturing and vibration damping method thereof |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2352499C1 (en) * | 2007-09-25 | 2009-04-20 | Государственное образовательное учреждение высшего профессионального образования "Ульяновский государственный технический университет" | Method of remote control over aircraft passenger seat turn angle and device to this end |
| CN103321268A (en) * | 2013-06-25 | 2013-09-25 | 徐州徐工挖掘机械有限公司 | Adaptive seat system of excavator |
| CN105333045A (en) * | 2015-12-05 | 2016-02-17 | 重庆创隆实业有限公司 | Car seat shock absorber |
| CN205525000U (en) * | 2016-01-29 | 2016-08-31 | 河南理工大学万方科技学院 | Air -service seat |
| CN205549526U (en) * | 2016-02-04 | 2016-09-07 | 深圳市幻境科技有限公司 | Spring cylinder and active motion platform |
| CN205554601U (en) * | 2016-04-04 | 2016-09-07 | 蓝灿玉 | Comfortable safe aircraft seat |
| CN207059829U (en) * | 2017-07-26 | 2018-03-02 | 东莞宜安科技股份有限公司 | A kind of automotive seat |
| CN107902012A (en) * | 2017-11-23 | 2018-04-13 | 无锡永锋科技有限公司 | A kind of electric motor car rear seat with shock-absorbing function |
-
2018
- 2018-05-03 CN CN201810414383.5A patent/CN108674668A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2352499C1 (en) * | 2007-09-25 | 2009-04-20 | Государственное образовательное учреждение высшего профессионального образования "Ульяновский государственный технический университет" | Method of remote control over aircraft passenger seat turn angle and device to this end |
| CN103321268A (en) * | 2013-06-25 | 2013-09-25 | 徐州徐工挖掘机械有限公司 | Adaptive seat system of excavator |
| CN105333045A (en) * | 2015-12-05 | 2016-02-17 | 重庆创隆实业有限公司 | Car seat shock absorber |
| CN205525000U (en) * | 2016-01-29 | 2016-08-31 | 河南理工大学万方科技学院 | Air -service seat |
| CN205549526U (en) * | 2016-02-04 | 2016-09-07 | 深圳市幻境科技有限公司 | Spring cylinder and active motion platform |
| CN205554601U (en) * | 2016-04-04 | 2016-09-07 | 蓝灿玉 | Comfortable safe aircraft seat |
| CN207059829U (en) * | 2017-07-26 | 2018-03-02 | 东莞宜安科技股份有限公司 | A kind of automotive seat |
| CN107902012A (en) * | 2017-11-23 | 2018-04-13 | 无锡永锋科技有限公司 | A kind of electric motor car rear seat with shock-absorbing function |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114771843A (en) * | 2022-06-16 | 2022-07-22 | 中国飞机强度研究所 | Seat vibration damping system in aviation aircraft manufacturing and vibration damping method thereof |
| CN114771843B (en) * | 2022-06-16 | 2022-09-23 | 中国飞机强度研究所 | Seat vibration damping system in aviation aircraft manufacturing and vibration damping method thereof |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
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| WD01 | Invention patent application deemed withdrawn after publication | ||
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Application publication date: 20181019 |