CN110304256A - It is a kind of can automatic swing backrest aircraft seat - Google Patents
It is a kind of can automatic swing backrest aircraft seat Download PDFInfo
- Publication number
- CN110304256A CN110304256A CN201910619991.4A CN201910619991A CN110304256A CN 110304256 A CN110304256 A CN 110304256A CN 201910619991 A CN201910619991 A CN 201910619991A CN 110304256 A CN110304256 A CN 110304256A
- Authority
- CN
- China
- Prior art keywords
- backrest
- turntable
- electric machine
- rotating electric
- aircraft seat
- 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
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
Abstract
The invention discloses it is a kind of can automatic swing backrest aircraft seat, it include: backrest and pedestal, the junction of the backrest and the pedestal is fixedly installed with turntable, and the turntable is internally connected with auto pendulous device, and the auto pendulous device includes: switch, rotating electric machine and controller；It is described to switch the outside for being embedded in the turntable, the rotating electric machine is connected with the turntable, and the rotating electric machine is connected with the controller and is fixed in the pedestal, the rotation of the turntable is driven by the rotating electric machine, and rotating and reverse for the rotating electric machine is controlled by the controller, through the above way, the present invention can be realized the automatic swing of backrest on aircraft seat, certain massage efficacy can not only be played, and physically sleeping can also be carried out in sleep quality.
Description
Technical field
The present invention relates to aircraft seat, in particular to it is a kind of can automatic swing backrest aircraft seat.
Background technique
Aircraft is most great one of invention early 20th century, it is recognized that is invented by American Lai Te brother.They were in 1903
The flight that December 17 carried out is international as " overweighting the controlled continuous driving force flight of the aircraft progress of air for the first time "
Aviation federation (FAI) is approved that the same year, they established " Lai Te Aircraft Company ", and after aircraft invention, aircraft is increasingly
As the indispensable tool of modern civilization, its deep change and people's lives are affected.
And aircraft seat is one of essential component in aircraft, its comfort will directly affect people's airplane
Impression, the seat on aircraft can only realize the swing of backrest by manual operation at present, and can not pass through automation
Control the automatic swing to realize backrest.
Summary of the invention
The invention mainly solves the technical problem of providing it is a kind of can automatic swing backrest aircraft seat, can be realized winged
The automatic swing of backrest on base chair can not only play certain massage efficacy, and can also carry out object in sleep quality
Reason formula sleeping.
In order to solve the above technical problems, one technical scheme adopted by the invention is that: providing one kind can automatic swing backrest
Aircraft seat, comprising: the junction of backrest and pedestal, the backrest and the pedestal is fixedly installed with turntable, the turntable
It is internally connected with auto pendulous device, the auto pendulous device includes: switch, rotating electric machine and controller；
Described switch is embedded in the outside of the turntable, and the rotating electric machine is connected with the turntable, and the rotating electric machine and
The controller is connected and is fixed in the pedestal, and the rotation of the turntable is driven by the rotating electric machine, and passes through
The controller controls rotating and reverse for the rotating electric machine.
In a preferred embodiment of the present invention, the input terminal of the rotating electric machine is also connected with governor.
In a preferred embodiment of the present invention, the switch is push-button switch.
In a preferred embodiment of the present invention, the control signal of the controller is sinusoidal signal wave.
In a preferred embodiment of the present invention, the period between the wave crest and trough of the sinusoidal signal wave is 20-
30s。
In a preferred embodiment of the present invention, the swing angle range of the turntable is no more than 30 °.
The beneficial effects of the present invention are: one kind of the present invention can automatic swing backrest aircraft seat, by backrest and bottom
The junction of seat is fixedly installed with turntable, and is internally connected with auto pendulous device in turntable, can change auto pendulous device
It is to control rotating and reverse for turntable, to realize that backrest carries out automatic swing, so that people lean against by back
Shi Bujin can play certain massage efficacy, and physically sleeping can also be carried out in sleep quality.
Detailed description of the invention
Fig. 1 is the structural scheme of mechanism of the present invention in a preferred embodiment；
The components in the drawings are labeled as follows: 1, backrest, 2, pedestal, 3, turntable, 4, switch, 5, rotating electric machine, 6, controller, 7,
Governor.
Specific embodiment
The preferred embodiments of the present invention will be described in detail with reference to the accompanying drawing, so that advantages and features of the invention energy
It is easier to be readily appreciated by one skilled in the art, so as to make a clearer definition of the protection scope of the present invention.
Referring to Fig. 1, the embodiment of the present invention includes:
It is a kind of can automatic swing backrest aircraft seat, comprising: backrest 1 and pedestal 2, the connection of the backrest 1 and the pedestal 2
Place is fixedly installed with turntable 3, and the turntable 3 is internally connected with auto pendulous device, the auto pendulous device include: switch 4,
Rotating electric machine 5 and controller 6；
The switch 4 is embedded in the outside of the turntable 3, and the rotating electric machine 5 is connected with the turntable 3, and the electric rotating
Machine 5 is connected with the controller 6 and is fixed in the pedestal 2, and turning for the turntable 3 is driven by the rotating electric machine 5
It is dynamic, and rotating and reverse for the rotating electric machine 5 is controlled by the controller 6.
Wherein, the input terminal of the rotating electric machine 5 is also connected with governor 7, by carrying out velocity of rotation to governor 7
It adjusts, to adjust the revolving speed of rotating electric machine 5, so that 1 swing speed of backrest can satisfy the demand of each crowd, use scope
Extensively.
It further illustrates, the switch 4 is push-button switch, and push-button switch operation is more easy, and people only need gently
One by the automatic operating for achieving that swing.
It further illustrating, the control signal of the controller 6 is sinusoidal signal wave, sinusoidal signal wavelength-division wave crest and trough,
When sinusoidal signal wave is located at wave crest, driving rotating electric machine 5 is rotated forward, when sinusoidal signal wave is located at trough, driving rotation
Motor 5 is inverted.
It further illustrates, the period between the wave crest and trough of the sinusoidal signal wave is 20-30s, enables to backrest
Swing speed keep more slow state, will not influence whole comfort.
It further illustrates, the swing angle range of the turntable 3 is no more than 30 °, and the swing angle of backrest 1 is enabled to protect
A reasonable range is held, will not influence and cause swing too big and not comfortable enough.
Further illustrate, present invention discloses it is a kind of can automatic swing backrest aircraft seat, specific operation is former
It manages as follows:
Firstly, pressing lower switch 4, driving rotating electric machine 5 rotates, at this point, since controller 6 sends sinusoidal signal wave, when sine is believed
When number wave is located at wave crest, driving rotating electric machine 5 is rotated forward, so that the end rotation backward of turntable 3, and then drive backrest 1
It is slowly swung backward, when sinusoidal signal wave gradually becomes trough, driving rotating electric machine 5 is inverted, so that turning
End rotation is so recycled and is run repeatedly, to realize backrest so that backrest 1 is carried forward homing position type swing disk 3 forward
1 automatic swing；In addition, can be swung when people think that hunting frequency is too fast or excessively slow by adjusting governor 7 to change
Frequency, to meet the needs of people.
Be different from the prior art, one kind of the present invention can automatic swing backrest aircraft seat, by backrest 1 and pedestal 2
Junction be fixedly installed with turntable 3, and be internally connected with auto pendulous device in turntable 3, auto pendulous device can be changed
It is to control rotating and reverse for turntable 3, to realize that backrest 1 carries out automatic swing, so that people lean against backrest 1
Stepping can play certain massage efficacy when upper, and physically sleeping can also be carried out in sleep quality.
In the description of the present invention, it should be noted that the instruction such as term " on ", "lower", "left", "right", "inner", "outside"
Orientation or positional relationship be based on the orientation or positional relationship shown in the drawings or the invention product using when usually put
Orientation or positional relationship, be merely for convenience of description of the present invention and simplification of the description, rather than the device of indication or suggestion meaning
Or element must have a particular orientation, be constructed and operated in a specific orientation, therefore be not considered as limiting the invention.
The above description is only an embodiment of the present invention, is not intended to limit the scope of the invention, all to utilize this hair
Equivalent structure or equivalent flow shift made by bright specification and accompanying drawing content is applied directly or indirectly in other relevant skills
Art field, is included within the scope of the present invention.
Claims (6)
1. one kind can automatic swing backrest aircraft seat characterized by comprising backrest and pedestal, the backrest and described
The junction of pedestal is fixedly installed with turntable, and the turntable is internally connected with auto pendulous device, the auto pendulous device packet
It includes: switch, rotating electric machine and controller；
Described switch is embedded in the outside of the turntable, and the rotating electric machine is connected with the turntable, and the rotating electric machine and
The controller is connected and is fixed in the pedestal, and the rotation of the turntable is driven by the rotating electric machine, and passes through
The controller controls rotating and reverse for the rotating electric machine.
2. it is according to claim 1 can automatic swing backrest aircraft seat, which is characterized in that the rotating electric machine it is defeated
Enter end and is also connected with governor.
3. it is according to claim 1 can automatic swing backrest aircraft seat, which is characterized in that it is described switch be push button
Switch.
4. it is according to claim 1 can automatic swing backrest aircraft seat, which is characterized in that the control of the controller
Signal is sinusoidal signal wave.
5. it is according to claim 4 can automatic swing backrest aircraft seat, which is characterized in that the sinusoidal signal wave
Period between wave crest and trough is 20-30s.
6. it is according to claim 1 can automatic swing backrest aircraft seat, which is characterized in that the angle of oscillation of the turntable
It spends range and is no more than 30 °.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910619991.4A CN110304256A (en) | 2019-07-10 | 2019-07-10 | It is a kind of can automatic swing backrest aircraft seat |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910619991.4A CN110304256A (en) | 2019-07-10 | 2019-07-10 | It is a kind of can automatic swing backrest aircraft seat |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110304256A true CN110304256A (en) | 2019-10-08 |
Family
ID=68079954
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910619991.4A Pending CN110304256A (en) | 2019-07-10 | 2019-07-10 | It is a kind of can automatic swing backrest aircraft seat |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110304256A (en) |
Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1266360A (en) * | 1997-09-30 | 2000-09-13 | 杜尔座椅科技公司 | Two platform motion seat |
| CN2529564Y (en) * | 2001-12-11 | 2003-01-08 | 陈庆全 | Electric massage rocking chair |
| CN100475173C (en) * | 1996-10-07 | 2009-04-08 | 松下电工株式会社 | Releasing device |
| CN101564344A (en) * | 2008-04-24 | 2009-10-28 | 松下电工株式会社 | Chair-type massage machine |
| CN201929432U (en) * | 2011-03-04 | 2011-08-17 | 佛山市丽江椅业有限公司 | Seat back oscillating mechanism |
| EP2168458B1 (en) * | 2008-09-25 | 2012-03-07 | Panasonic Electric Works Co., Ltd | Relaxation apparatus |
| CN203646825U (en) * | 2013-09-03 | 2014-06-18 | 吴展发 | Multifunctional rocking chair |
| US20170099949A1 (en) * | 2015-10-12 | 2017-04-13 | Steve FORTIER | Electric rocking chair |
| CN206939086U (en) * | 2017-04-01 | 2018-01-30 | 韩熠鹏 | A kind of aircraft seat |
| CN108926155A (en) * | 2018-05-08 | 2018-12-04 | 刘红华 | A kind of obstetrics pregnant woman rest rocking chair |
| CN109349845A (en) * | 2018-12-17 | 2019-02-19 | 东莞贯新幼童用品有限公司 | Electric rocking chair |
-
2019
- 2019-07-10 CN CN201910619991.4A patent/CN110304256A/en active Pending
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100475173C (en) * | 1996-10-07 | 2009-04-08 | 松下电工株式会社 | Releasing device |
| CN1266360A (en) * | 1997-09-30 | 2000-09-13 | 杜尔座椅科技公司 | Two platform motion seat |
| CN2529564Y (en) * | 2001-12-11 | 2003-01-08 | 陈庆全 | Electric massage rocking chair |
| CN101564344A (en) * | 2008-04-24 | 2009-10-28 | 松下电工株式会社 | Chair-type massage machine |
| EP2168458B1 (en) * | 2008-09-25 | 2012-03-07 | Panasonic Electric Works Co., Ltd | Relaxation apparatus |
| CN201929432U (en) * | 2011-03-04 | 2011-08-17 | 佛山市丽江椅业有限公司 | Seat back oscillating mechanism |
| CN203646825U (en) * | 2013-09-03 | 2014-06-18 | 吴展发 | Multifunctional rocking chair |
| US20170099949A1 (en) * | 2015-10-12 | 2017-04-13 | Steve FORTIER | Electric rocking chair |
| CN206939086U (en) * | 2017-04-01 | 2018-01-30 | 韩熠鹏 | A kind of aircraft seat |
| CN108926155A (en) * | 2018-05-08 | 2018-12-04 | 刘红华 | A kind of obstetrics pregnant woman rest rocking chair |
| CN109349845A (en) * | 2018-12-17 | 2019-02-19 | 东莞贯新幼童用品有限公司 | Electric rocking chair |
Non-Patent Citations (1)
| Title |
|---|
| 何希才，姜余祥: "《电动机控制电路应用实例》", 31 January 2005, 中国电力出版社 * |
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|---|---|---|---|
| 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 |
Application publication date: 20191008 |
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| RJ01 | Rejection of invention patent application after publication |