CN105109380A - Aircraft seat armrest capable of rotating horizontally - Google Patents
Aircraft seat armrest capable of rotating horizontally Download PDFInfo
- Publication number
- CN105109380A CN105109380A CN201510507586.5A CN201510507586A CN105109380A CN 105109380 A CN105109380 A CN 105109380A CN 201510507586 A CN201510507586 A CN 201510507586A CN 105109380 A CN105109380 A CN 105109380A
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- CN
- China
- Prior art keywords
- groove
- aircraft seat
- vertical walls
- jacking system
- horizontally rotated
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Abstract
The invention discloses an aircraft seat armrest capable of rotating horizontally. The aircraft seat armrest is characterized by comprising a sliding rail (1), a sliding block (2), a lifting device (3), a vertical arm (4) and a lateral arm (5), wherein the side wall of the sliding rail (1) is fixed to a side surface of a seat; a sliding groove (6) is formed in the sliding rail (1), the opening of the sliding groove (6) is upward, and the sliding block (2) is arranged in the sliding groove (6); the lifting device (3) is arranged on the sliding block (2) and is connected with the bottom end of the vertical arm (4); the top end of the vertical arm (4) is movably connected with the lateral arm (5). The aircraft seat armrest capable of rotating horizontally provided by the invention can satisfy requirements that the aircraft seat armrest is used for supporting a head when a passenger is sleeping and supporting arms when the passenger is awake, and the aircraft seat armrest is safe, comfortable and has functions of bacteria resistance and bacteriostasis.
Description
Technical field
The present invention relates to a kind of aircraft seat handrail horizontally rotated, belong to aircraft component design field.
Background technology
At present, the armrest on aircraft has possessed automatic deploying and retracting function, is convenient to passenger like this and comes in and goes out from seat, uses also very convenient.But, also do not find that one can meet passenger's supporting head part when sleep state, support the aircraft seat handrail of arm when waking state.
Summary of the invention
Technical matters to be solved by this invention is, provides one to meet passenger's supporting head part when sleep state, supports arm when waking state, safety and comfort and have the aircraft seat handrail of fungi-proofing function.
For solving the problems of the technologies described above, the technical solution used in the present invention is:
A kind of aircraft seat handrail horizontally rotated, it is characterized in that: comprise slide rail, slide block, jacking system, vertical walls and transverse wall, the sidewall of described slide rail is fixed on seat side, described slide rail is provided with chute, described chute opening upwards and its in be provided with described slide block, described slide block is provided with described jacking system, and described jacking system is connected with the bottom of described vertical walls, and the top of described vertical walls is flexibly connected with described transverse wall.
Described jacking system is provided with lifting button.
Described transverse wall comprise one connect semicircle pipe link be connected ball, the top of described vertical walls is provided with the first groove for holding described connection ball and the second groove for holding described pipe link, described first groove is less than the diameter connecting ball at the opening diameter on the top of described vertical walls, described first groove is connected with the second groove.
The number of described second groove is 2, and 2 described second grooves are vertically arranged mutually, and the direction of described second groove is respectively to seat front with inside seat.
The direction being positioned at the second groove of the aircraft seat handrail of passageway and adjacent nacelle interior wall is respectively to seat front with inside seat, and the direction being positioned at the second groove of middle aircraft seat handrail is respectively to seat front and the outside of aircraft seat being positioned at passageway mutually.
The horizontal surface of described semicircle pipe link upwards, the bed course that the Surface coating of described semicircle pipe link has quality soft.
The material of described bed course is resin or silica gel or polyurethane.
The outside face of described jacking system, vertical walls and bed course is provided with fungistatic coating.
The material of described fungistatic coating comprises film adhesive and microbiotic.
A kind of aircraft seat handrail horizontally rotated provided by the invention, when passenger is waking state, the phase front, direction of transverse wall, arm can be taken and put on armrest by passenger; When passenger wants in bed, by the configuration of slide block and slide rail, vertical walls can be made to move to the position of passenger front, then raise semicircle pipe link and be positioned in another second groove, now semicircle pipe link is positioned at the lower head of passenger, regulates jacking system, semicircle pipe link is positioned at and is suitable for sleep, the position of supporting head part, now, passenger can go to sleep peacefully; In addition, the bed course that semicircle pipe link Surface coating has quality soft, makes passenger be more prone to fall asleep; The outside face of jacking system, vertical walls and bed course is provided with the design hommization more of fungistatic coating, make the environment of interior of aircraft more clean, avoid the cross-infection that passenger's next one that is sick or that carry pathogenic bacteria and cause takes the passenger of this position, ensure that passenger's is healthy.A kind of aircraft seat handrail horizontally rotated provided by the invention, can meet passenger's supporting head part when sleep state, supports arm when waking state, safety and comfort and have the function of antibacterial and bacteriostatic.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention;
Fig. 2 is enlarged drawing of the present invention;
Fig. 3 is the birds-eye view of part A in Fig. 2.
Detailed description of the invention
Below in conjunction with accompanying drawing, the present invention is further described.
As Figure 1-3, a kind of aircraft seat handrail horizontally rotated, it is characterized in that: comprise slide rail 1, slide block 2, jacking system 3, vertical walls 4 and transverse wall 5, the sidewall of described slide rail 1 is fixed on seat side, described slide rail 1 is provided with chute 6, described chute 6 opening upwards and its in be provided with described slide block 2, described slide block 2 is provided with described jacking system 3, described jacking system 3 is connected with the bottom of described vertical walls 4, and the top of described vertical walls 4 is flexibly connected with described transverse wall 5.
Described jacking system 3 is provided with lifting button 7.
Described transverse wall 5 comprise one connect semicircle pipe link 8 be connected ball 9, the top of described vertical walls 4 is provided with the first groove 10 for holding described connection ball 9 and the second groove 11 for holding described pipe link 8, described first groove 10 is less than the diameter connecting ball 9 at the opening diameter on the top of described vertical walls 4, described first groove 10 is connected with the second groove 11.
The number of described second groove 11 is 2, and 2 described second groove 11 vertical settings mutually, the direction of described second groove 11 is respectively to seat front with inside seat.
The horizontal surface of described semicircle pipe link 8 upwards, the bed course that the Surface coating of described semicircle pipe link 8 has quality soft.
The material of described bed course is silica gel.
The outside face of described jacking system 3, vertical walls 4 and bed course is provided with fungistatic coating.
The above is only the preferred embodiment of the present invention; be noted that for those skilled in the art; under the premise without departing from the principles of the invention, can also make some improvements and modifications, these improvements and modifications also should be considered as protection scope of the present invention.
Claims (7)
1. the aircraft seat handrail that can horizontally rotate, it is characterized in that: comprise slide rail (1), slide block (2), jacking system (3), vertical walls (4) and transverse wall (5), the sidewall of described slide rail (1) is fixed on seat side, described slide rail (1) is provided with chute (6), described chute (6) opening upwards and its in be provided with described slide block (2), described slide block (2) is provided with described jacking system (3), described jacking system (3) is connected with the bottom of described vertical walls (4), the top of described vertical walls (4) is flexibly connected with described transverse wall (5).
2. the aircraft seat handrail horizontally rotated according to claim 1, is characterized in that: described jacking system (3) is provided with lifting button (7).
3. the aircraft seat handrail horizontally rotated according to claim 1, it is characterized in that: described transverse wall (5) comprise one connect semicircle pipe link (8) be connected ball (9), the top of described vertical walls (4) is provided with the first groove (10) for holding described connection ball (9) and the second groove (11) for holding described pipe link (8), described first groove (10) is less than the diameter connecting ball (9) at the opening diameter on the top of described vertical walls (4), described first groove (10) is connected with the second groove (11).
4. the aircraft seat handrail horizontally rotated according to claim 3, it is characterized in that: the number of described second groove (11) is 2,2 described second groove (11) vertical settings mutually, the direction of described second groove (11) is respectively to seat front with inside seat.
5. the aircraft seat handrail horizontally rotated according to claim 3, is characterized in that: the horizontal surface of described semicircle pipe link (8) upwards, the bed course that the Surface coating of described semicircle pipe link (8) has quality soft.
6. the aircraft seat handrail horizontally rotated according to claim 5, is characterized in that: the material of described bed course is resin or silica gel or polyurethane.
7. the aircraft seat handrail horizontally rotated according to claim 5, is characterized in that: the outside face of described jacking system (3), vertical walls (4) and bed course is provided with fungistatic coating.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510507586.5A CN105109380B (en) | 2015-08-18 | 2015-08-18 | The aircraft seat handrail that can be rotated horizontally |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510507586.5A CN105109380B (en) | 2015-08-18 | 2015-08-18 | The aircraft seat handrail that can be rotated horizontally |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105109380A true CN105109380A (en) | 2015-12-02 |
| CN105109380B CN105109380B (en) | 2018-05-25 |
Family
ID=54657582
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510507586.5A Active CN105109380B (en) | 2015-08-18 | 2015-08-18 | The aircraft seat handrail that can be rotated horizontally |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105109380B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106333537A (en) * | 2016-09-23 | 2017-01-18 | 中国航空综合技术研究所 | Multi-freedom-degree adjusting device of seat arm support |
| CN108749669A (en) * | 2018-04-26 | 2018-11-06 | 张立新 | A kind of car multifunctional adjustable handrail |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1795114A (en) * | 2003-05-28 | 2006-06-28 | 沃尔沃建造设备控股（瑞典）有限公司 | Armrest for use with a vehicle seat |
| CN202029711U (en) * | 2011-04-17 | 2011-11-09 | 龙海市九龙座椅有限公司 | Novel chair for bloodmobiles |
| CN202071732U (en) * | 2011-05-11 | 2011-12-14 | 奇瑞汽车股份有限公司 | Multifunctional vehicle-mounted mobile device |
| CN202448864U (en) * | 2011-12-13 | 2012-09-26 | 浙江吉利汽车研究院有限公司 | Armrest box device of automobile |
| CN202753828U (en) * | 2012-06-21 | 2013-02-27 | 王阳 | Automotive elbow support |
| CN202764755U (en) * | 2012-10-09 | 2013-03-06 | 邹珺 | Safety chair suitable for buses |
| JP2013136321A (en) * | 2011-12-28 | 2013-07-11 | Daihatsu Motor Co Ltd | Seat device of vehicle |
-
2015
- 2015-08-18 CN CN201510507586.5A patent/CN105109380B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1795114A (en) * | 2003-05-28 | 2006-06-28 | 沃尔沃建造设备控股（瑞典）有限公司 | Armrest for use with a vehicle seat |
| CN202029711U (en) * | 2011-04-17 | 2011-11-09 | 龙海市九龙座椅有限公司 | Novel chair for bloodmobiles |
| CN202071732U (en) * | 2011-05-11 | 2011-12-14 | 奇瑞汽车股份有限公司 | Multifunctional vehicle-mounted mobile device |
| CN202448864U (en) * | 2011-12-13 | 2012-09-26 | 浙江吉利汽车研究院有限公司 | Armrest box device of automobile |
| JP2013136321A (en) * | 2011-12-28 | 2013-07-11 | Daihatsu Motor Co Ltd | Seat device of vehicle |
| CN202753828U (en) * | 2012-06-21 | 2013-02-27 | 王阳 | Automotive elbow support |
| CN202764755U (en) * | 2012-10-09 | 2013-03-06 | 邹珺 | Safety chair suitable for buses |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106333537A (en) * | 2016-09-23 | 2017-01-18 | 中国航空综合技术研究所 | Multi-freedom-degree adjusting device of seat arm support |
| CN108749669A (en) * | 2018-04-26 | 2018-11-06 | 张立新 | A kind of car multifunctional adjustable handrail |
| CN108749669B (en) * | 2018-04-26 | 2020-11-27 | 临沂文一诺知识产权运营有限公司 | Multifunctional adjustable handrail for passenger car |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105109380B (en) | 2018-05-25 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| CB03 | Change of inventor or designer information | ||
| CB03 | Change of inventor or designer information |
Inventor after: Lv Qiongjia Inventor before: Jiu Jianxiang |
|
| TA01 | Transfer of patent application right | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20180418 Address after: 362000 294 Mei Zhong village, pengpeng Town, Yongchun County, Quanzhou, Fujian Applicant after: Lv Qiongjia Address before: 215627 East ladian Road, Yang Shi Town, Zhangjiagang City, Suzhou, Jiangsu Applicant before: ZHANGJIAGANG ZIDONG MACHINERY TECHNOLOGY CO., LTD. |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20191204 Address after: 314406 No.187, Qingwan Road, Xieqiao Town, Haining City, Jiaxing City, Zhejiang Province Patentee after: Haining Luoxi Industrial Development Co., Ltd Address before: 362000 294 Mei Zhong village, pengpeng Town, Yongchun County, Quanzhou, Fujian Patentee before: Lv Qiongjia |