CN108583904A - A kind of magnetic guidance formula aircraft seat - Google Patents
A kind of magnetic guidance formula aircraft seat Download PDFInfo
- Publication number
- CN108583904A CN108583904A CN201810347727.5A CN201810347727A CN108583904A CN 108583904 A CN108583904 A CN 108583904A CN 201810347727 A CN201810347727 A CN 201810347727A CN 108583904 A CN108583904 A CN 108583904A
- Authority
- CN
- China
- Prior art keywords
- seat
- aircraft seat
- main body
- storage tank
- backrest
- 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
- 230000035939 shock Effects 0.000 claims abstract description 19
- 238000005096 rolling process Methods 0.000 claims description 11
- 230000003028 elevating effect Effects 0.000 claims description 3
- 230000005611 electricity Effects 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 3
- 238000009434 installation 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
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
- B64D11/0639—Arrangements of seats, or adaptations or details specially adapted for aircraft seats with features for adjustment or converting of seats
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Massaging Devices (AREA)
- Percussion Or Vibration Massage (AREA)
Abstract
A kind of magnetic guidance formula aircraft seat, belongs to airplane equipment field.It is made of inlet control device, magnetic navigation system, guide wire path, aircraft seat, chassis, polishing-shoes mechanism, seat main body, backrest regulation handle, handrail, backrest, massage column, shock club, master control borad, buckle, lift adjustment handle, lifter, storage tank and connecting shaft；The device controls aircraft seat by navigation system and is moved along the guide wire path set, it does not need passenger and looks for the seat of oneself everywhere carrying thing, with very high convenience and practicability, height of seat can be adjusted according to own situation, seat is provided with shock club by back, is arranged according to human acupoint, passenger-back is set to be massaged and be loosened, apparatus structure design is rigorous, and performance is easily achieved, and has very strong practicability.
Description
Technical field
The present invention relates to a kind of magnetic guidance formula aircraft seats, belong to airplane equipment field.
Background technology
Currently, with the development of technology and the improvement of people ’ s living standards, to the comfort level and practicability of aircraft seat
It is required that it is also higher and higher, and there is no a kind of seat of magnetic guidance formula in existing aircraft seat, can root be manipulated by control system
It is moved freely according to guide line diameter, in general present aircraft seat comfort level is not high, and the function on seat is also seldom, cannot
Meets the needs of passenger.
Invention content
In view of the above-mentioned deficiencies, the present invention provides a kind of magnetic guidance formula aircraft seats.
The present invention is achieved by the following technical solutions：A kind of magnetic guidance formula aircraft seat is to be controlled to fill by inlet
It sets, magnetic navigation system, guide wire path, aircraft seat, chassis, polishing-shoes mechanism, seat main body, backrest regulation handle, handrail, lean on
What the back of the body, massage column, shock club, master control borad, buckle, lift adjustment handle, lifter, storage tank and connecting shaft formed, feature
It is：The inlet control device is arranged at passenger entrance, controls each aircraft seat and is moved along guide wire path, is led
Conductive path is laid in ground, and aircraft seat lower part is provided with chassis, and inside chassis is equipped with magnetic navigation system, magnetic navigation system
It is connected with the guide wire in ground, chassis top is provided with lifter, seat main body, seat are support at the piston of lifter
The left side of chair main body is provided with backrest regulation handle, and seat main body is ducted body, is internally provided with storage tank, storage tank handle
It is arranged on the right side of seat main body, seat main body and is provided with handrail, buckle, the seat main body is provided on the outside of handrail
Front end is provided with lift adjustment handle, and elevating control handle is connected by link mechanism with lifter, the backrest end face
For an inclined surface, be adapted with human body, backrest is connected by connecting shaft with seat main body, massage column be neatly arranged side by side by
Back, backrest are internally provided with shock club, and shock club is mounted on master control borad, and master control borad is fixed on inside backrest, shock club
Caput is close to massage column wall.
Connecting pole is provided on the handrail, handrail is connected by connecting pole with one end of a connecting rod, connecting rod it is another
End is connected with fixed pin, and fixed pin is fixedly mounted on ratchet, and the side of ratchet is provided with latch plate, and bullet is provided on latch plate
One end of spring, spring is connected to detent, and detent is installed with the tooth cooperation on ratchet, and ratchet and detent pass through axis
On the same face, the armrest rear end is provided with rotation axis for installation, and rotation axis is mounted on seat main body.
The polishing-shoes mechanism include Main Control Tank, inductor, notch board, bottom plate, piston cylinder, pedal, rolling brush, connecting rod,
First gear, second gear and motor form, the Main Control Tank is internally provided with control system, and master control lower box part is provided with
Inductor, inductor side are provided with motor, and motor is connected with first gear, and first gear engages connection with second gear,
Second gear is connected by connecting rod with rolling brush, and the both sides of rolling brush are equipped with notch board, and one end of notch board is connect with Main Control Tank,
The other end of notch board is connect with bottom plate, and the top end face centre position of bottom plate is provided with piston cylinder, and piston cylinder is connected with pedal.
Storage tank handle is provided on the storage tank outer end face, storage tank bottom is provided with sliding rail, and sliding rail is along setting
In the protrusion sliding of seat body interior, storage tank is provided with corresponding groove on two sides, supporting leg is provided on groove, props up
One end of leg is provided with fixing axle, and fixing axle is fixed on groove, and position corresponding with supporting leg one end is provided with baffle.
The baffle is arc surface, and nose circle face when being supported with supporting leg is concentric.
The storage tank upper end is provided with a concave surface, coordinates with the convex surface on seat main body and installs.
The size of the first gear and second gear is selected according to power of motor and actual conditions.
Described pedal one end is equipped with shaft, and shaft both ends are mounted on notch board, and pedal rotates shaft rotation according to pressure size
Dynamic certain angle.
The aircraft seat is equipped with number, aircraft seat proper alignment in order.
The usefulness of the invention is that the device controls aircraft seat along the guide wire path set by navigation system
It is mobile, passenger is not needed carrying thing and looks for the seat of oneself everywhere, and there is very high convenience and practicability；In aircraft seat
On be provided with lifter, passenger can adjust height of seat according to own situation；Back is provided with shock club in seat, according to
Human acupoint is arranged, and passenger-back is made to be massaged and be loosened；Armrest is adjustable, meets comfort, handrail lower part is equipped with
One ratchet mechanism can prevent handrail from gliding, and handrail height is reduced by adjusting detent, easy to use；It is provided with storing
Case facilitates the placement of carry-on articles, safety convenient；Apparatus structure design is rigorous, and performance is easily achieved, and has very strong practicality
Property.
Description of the drawings
Fig. 1 is the path planning figure of the present invention；
Fig. 2 is the axonometric drawing of the present invention；
Fig. 3 is the side view of the present invention；
Fig. 4 is the structural schematic diagram of handrail driving device；
Fig. 5 is the front view of polishing-shoes mechanism；
Fig. 6 is the axonometric drawing of polishing-shoes mechanism；
Fig. 7 is the schematic diagram of rolling brush driving mechanism；
Fig. 8 is the front view of shock club；
Fig. 9 is the axonometric drawing of shock club；
Figure 10 is the structural schematic diagram of storage tank；
Figure 11 is the side view of storage tank.
In figure, 1, inlet control device, 2, guide wire path, 3, aircraft seat, 4, chassis, 5, polishing-shoes mechanism, 6, seat
Chair main body, 7, backrest regulation handle, 8, handrail, 9, backrest, 10, massage column, 11, buckle, 12, lift adjustment handle, 13, lifting
Device, 14, storage tank, 15, connecting shaft, 16, ratchet, 17, fixed pin, 18, connecting rod, 19, connecting pole, 20, rotation axis, 21, spring
Plate, 22, spring, 23, detent, 24, Main Control Tank, 25, inductor, 26, notch board, 27, bottom plate, 28, piston cylinder, 29, roll
Brush, 30, pedal, 31, connecting rod, 32, second gear, 33, motor, 34, first gear, 35, shock club, 36, master control borad, 37,
Storage tank handle, 38, sliding rail, 39, protrusion, 40, groove, 41, supporting leg, 42, fixing axle, 43, baffle.
Specific implementation mode
A kind of magnetic guidance formula aircraft seat is by inlet control device 1, magnetic navigation system, guide wire path 2, aircraft
Seat 3, chassis 4, polishing-shoes mechanism 5, seat main body 6, backrest regulation handle 7, handrail 8, backrest 9, massage column 10, shock club 35,
What master control borad 36, buckle 11, lift adjustment handle 12, lifter 13, storage tank 14 and connecting shaft 15 formed, it is characterised in that：
The inlet control device 1 is arranged at passenger entrance, controls each aircraft seat 3 and is moved along guide wire path 2, guides
Thread path 2 is laid in ground, and 3 lower part of aircraft seat is provided with chassis 4, and chassis 4 is internally provided with magnetic navigation system, magnetic navigation system
System is connected with the guide wire in ground, and 4 top of chassis is provided with lifter 13, seat is support at the piston of lifter 13
The left side of main body 6, seat main body 6 is provided with backrest regulation handle 7, and seat main body 6 is ducted body, is internally provided with storage tank
14,14 handle of storage tank, which is arranged on the right side of seat main body 6, seat main body 6, is provided with handrail 8, and 8 outside of handrail is provided with
Buckle 11,6 front end of seat main body are provided with lift adjustment handle 12, and elevating control handle passes through link mechanism and lifting
Device 13 is connected, and 9 end face of backrest is an inclined surface, is adapted with human body, backrest 9 passes through connecting shaft 15 and seat main body
6 are connected, and massage column 10 is neat side by side to be arranged on backrest 9, and backrest 9 is internally provided with shock club 35, and shock club 35 is mounted on
On master control borad 36, master control borad 36 is fixed on inside backrest 9, and the caput of shock club 35 is close to 10 inner wall of massage column.
Connecting pole 19 is provided on the handrail 8, handrail 8 is connected by connecting pole 19 with one end of a connecting rod 18, even
The other end of bar 18 is connected with fixed pin 17, and fixed pin 17 is fixedly mounted on ratchet 16, and the side of ratchet 16 is provided with spring
Plate 21, is provided with spring 22 on latch plate 21, and one end of spring 22 is connected to detent 23, detent 23 on ratchet 16
Tooth cooperation installation, ratchet 16 and detent 23 installed on the same face by axis, and 8 rear end of handrail, which is provided with, to be turned
Moving axis 20, rotation axis 20 are mounted on seat main body 6.
The polishing-shoes mechanism 5 includes Main Control Tank 24, inductor 25, notch board 26, bottom plate 27, piston cylinder 28, pedal 30, rolling
What dynamic brush 29, connecting rod 31, first gear 34, second gear 32 and motor 33 formed, the Main Control Tank 24 is internally provided with
Control system, 24 lower part of Main Control Tank are provided with inductor 25, and 25 side of inductor is provided with motor 33, motor 33 and first gear
34 are connected, and first gear 34 engages connection with second gear 32, and second gear 32 is connected by connecting rod 31 with rolling brush 29
It connects, the both sides of rolling brush 29 are equipped with notch board 26, and one end of notch board 26 is connect with Main Control Tank 24, the other end and the bottom plate 27 of notch board 26
Connection, the top end face centre position of bottom plate 27 are provided with piston cylinder 28, and piston cylinder 28 is connected with pedal 30.
Storage tank handle 37 is provided on 14 outer end face of storage tank, 14 bottom of storage tank is provided with sliding rail 38, sliding
Rail 38 is slided along the protrusion 39 being arranged inside seat main body 6, and storage tank is provided with corresponding groove 40 on 14 two sides, recessed
Supporting leg 41 is provided on slot 40, one end of supporting leg 41 is provided with fixing axle 42, and fixing axle 42 is fixed on groove 40, with supporting leg 41
The corresponding position in one end is provided with baffle 43.
The baffle 43 is arc surface, and nose circle face when being supported with supporting leg 41 is concentric.
14 upper end of storage tank is provided with a concave surface, coordinates with the convex surface on seat main body 6 and installs.
The size of the first gear 34 and second gear 32 is selected according to 33 power of motor and actual conditions.
Described 30 one end of pedal be equipped with shaft, shaft both ends be mounted on notch board 26 on, pedal 30 according to pressure size around
Shaft turns an angle.
The aircraft seat 3 is equipped with number, the proper alignment in order of aircraft seat 3.
At work, passenger reaches at the airport of entry device, presses the seat number of oneself, the number on the touchscreen
Seat is moved to entrance along guide wire path 2, and passenger places an article in storage tank 14, and on seat to seat, seat is along path
Back to previous position, passenger adjusts the comfort of seat by own situation, by adjusting backrest regulation handle 7, to backrest 9
Gradient is adjusted, and by adjusting lift adjustment handle 12, is adjusted to the height of seat, foot is placed on polishing-shoes mechanism 5
In pedal 30 on, inductor 25 is started to work after sensing, rolling brush 29 wipes shoes, open massage button, master control
Plate 36 is started to work, and the shock club 3535 on master control borad 36 shakes, and is driven massage column 10 to shake, is massaged human body back,
By the height for pulling 11 adjustable handrail 8 of buckle.
For the ordinary skill in the art, introduction according to the present invention, do not depart from the principle of the present invention with
In the case of spirit, changes, modifications, replacement and modification that embodiment is carried out still fall within protection scope of the present invention it
It is interior.
Claims (9)
1. a kind of magnetic guidance formula aircraft seat, be by inlet control device, magnetic navigation system, guide wire path, aircraft seat,
Chassis, polishing-shoes mechanism, seat main body, backrest regulation handle, handrail, backrest, massage column, shock club, master control borad, buckle, lifting
What regulation handle, lifter, storage tank and connecting shaft formed, it is characterised in that：The inlet control device setting is multiplying
Objective inlet controls each aircraft seat and is moved along guide wire path, and guide wire path is laid in ground, aircraft seat lower part
It is provided with chassis, inside chassis is equipped with magnetic navigation system, and magnetic navigation system is connected with the guide wire in ground, chassis top
It is provided with lifter, seat main body is support at the piston of lifter, the left side of seat main body is provided with backrest regulation handle,
Seat main body is ducted body, is internally provided with storage tank, and storage tank handle is arranged on the right side of seat main body, seat main body
It is provided with handrail, is provided with buckle on the outside of handrail, the seat main body front end is provided with lift adjustment handle, elevating control handle
Hand is connected by link mechanism with lifter, and the backrest end face is an inclined surface, is adapted with human body, backrest passes through company
Spindle is connected with seat main body, and massage column is neatly arranged side by side by back, and backrest is internally provided with shock club, shock club peace
On master control borad, master control borad is fixed on inside backrest, and the caput of shock club is close to massage column wall.
2. a kind of magnetic guidance formula aircraft seat as described in claim 1, it is characterised in that：Connection is provided on the handrail
Column, handrail are connected by connecting pole with one end of a connecting rod, and the other end of connecting rod is connected with fixed pin, and fixed pin is fixedly mounted on
On ratchet, the side of ratchet is provided with latch plate, and spring is provided on latch plate, and one end of spring is connected to detent, only
Pawl is installed with the tooth cooperation on ratchet, and ratchet and detent are installed by axis on the same face, after the handrail
End is provided with rotation axis, and rotation axis is mounted on seat main body.
3. a kind of magnetic guidance formula aircraft seat as described in claim 1, it is characterised in that：The polishing-shoes mechanism includes master control
Case, inductor, notch board, bottom plate, piston cylinder, pedal, rolling brush, connecting rod, first gear, second gear and motor form,
The Main Control Tank is internally provided with control system, and master control lower box part is provided with inductor, and inductor side is provided with motor, electricity
Machine is connected with first gear, and first gear engages connection with second gear, and second gear is connected by connecting rod with rolling brush
It connects, the both sides of rolling brush are equipped with notch board, and one end of notch board is connect with Main Control Tank, and the other end of notch board is connect with bottom plate, bottom plate
Top end face centre position is provided with piston cylinder, and piston cylinder is connected with pedal.
4. a kind of magnetic guidance formula aircraft seat as described in claim 1, it is characterised in that：It is set on the storage tank outer end face
It is equipped with storage tank handle, storage tank bottom is provided with sliding rail, and sliding rail is along the protrusion sliding being arranged in seat body interior, storage tank
It is provided with corresponding groove on two sides, supporting leg is provided on groove, one end of supporting leg is provided with fixing axle, and fixing axle is fixed
On groove, position corresponding with supporting leg one end is provided with baffle.
5. a kind of magnetic guidance formula aircraft seat as claimed in claim 4, it is characterised in that：The baffle is arc surface, with
Nose circle face when supporting leg supports is concentric.
6. a kind of magnetic guidance formula aircraft seat as claimed in claim 4, it is characterised in that：The storage tank upper end is provided with
One concave surface coordinates with the convex surface on seat main body and installs.
7. a kind of magnetic guidance formula aircraft seat as claimed in claim 3, it is characterised in that：The first gear and the second tooth
The size of wheel is selected according to power of motor and actual conditions.
8. a kind of magnetic guidance formula aircraft seat as claimed in claim 3, it is characterised in that：Described pedal one end, which is equipped with, to be turned
Axis, shaft both ends are mounted on notch board, and pedal rotates around the axis certain angle according to pressure size.
9. a kind of magnetic guidance formula aircraft seat as described in claim 1, it is characterised in that：The aircraft seat, which is equipped with, to be compiled
Number, aircraft seat proper alignment in order.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810347727.5A CN108583904A (en) | 2018-04-18 | 2018-04-18 | A kind of magnetic guidance formula aircraft seat |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810347727.5A CN108583904A (en) | 2018-04-18 | 2018-04-18 | A kind of magnetic guidance formula aircraft seat |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108583904A true CN108583904A (en) | 2018-09-28 |
Family
ID=63611038
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810347727.5A Pending CN108583904A (en) | 2018-04-18 | 2018-04-18 | A kind of magnetic guidance formula aircraft seat |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108583904A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110884662A (en) * | 2019-11-17 | 2020-03-17 | 滨州学院 | Aircraft seat with comfortable backrest adjusting mechanism |
| CN113815866A (en) * | 2021-11-01 | 2021-12-21 | 吴珍桂 | Safety seat system on airplane |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2721452Y (en) * | 2004-06-11 | 2005-08-31 | 全兴工业股份有限公司 | Wired/wireless shaking and messaging device of seat for vehicle |
| CN2875876Y (en) * | 2006-03-15 | 2007-03-07 | 宋博 | Seat shoe polishing machine for vehicle |
| CN203596028U (en) * | 2013-10-24 | 2014-05-14 | 武汉理工大学 | Magnetic guide type AGV path distributor |
| CN104161405A (en) * | 2014-06-27 | 2014-11-26 | 蒋孝年 | A seat back angle adjusting device |
| CN105150884A (en) * | 2015-09-16 | 2015-12-16 | 航宇救生装备有限公司 | Lifting rotating base |
| CN106715191A (en) * | 2014-09-26 | 2017-05-24 | 庞巴迪公司 | Aircraft seat |
| US20170240283A1 (en) * | 2016-02-18 | 2017-08-24 | B/E Aerospace, Inc. | Aircraft passenger suite seating arrangements with all aisle access |
-
2018
- 2018-04-18 CN CN201810347727.5A patent/CN108583904A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2721452Y (en) * | 2004-06-11 | 2005-08-31 | 全兴工业股份有限公司 | Wired/wireless shaking and messaging device of seat for vehicle |
| CN2875876Y (en) * | 2006-03-15 | 2007-03-07 | 宋博 | Seat shoe polishing machine for vehicle |
| CN203596028U (en) * | 2013-10-24 | 2014-05-14 | 武汉理工大学 | Magnetic guide type AGV path distributor |
| CN104161405A (en) * | 2014-06-27 | 2014-11-26 | 蒋孝年 | A seat back angle adjusting device |
| CN106715191A (en) * | 2014-09-26 | 2017-05-24 | 庞巴迪公司 | Aircraft seat |
| CN105150884A (en) * | 2015-09-16 | 2015-12-16 | 航宇救生装备有限公司 | Lifting rotating base |
| US20170240283A1 (en) * | 2016-02-18 | 2017-08-24 | B/E Aerospace, Inc. | Aircraft passenger suite seating arrangements with all aisle access |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110884662A (en) * | 2019-11-17 | 2020-03-17 | 滨州学院 | Aircraft seat with comfortable backrest adjusting mechanism |
| CN113815866A (en) * | 2021-11-01 | 2021-12-21 | 吴珍桂 | Safety seat system on airplane |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180928 |