CN103072694A - Tablet personal computer support mounted on aircraft chair and usage thereof - Google Patents
Tablet personal computer support mounted on aircraft chair and usage thereof Download PDFInfo
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- CN103072694A CN103072694A CN2013100267179A CN201310026717A CN103072694A CN 103072694 A CN103072694 A CN 103072694A CN 2013100267179 A CN2013100267179 A CN 2013100267179A CN 201310026717 A CN201310026717 A CN 201310026717A CN 103072694 A CN103072694 A CN 103072694A
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- panel computer
- trip
- travel
- safety rope
- ing rest
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Abstract
The invention relates to a tablet personal computer support mounted on an aircraft chair, which comprises a table board (1), a fixed mount (2), a movable mount (3), a tablet personal computer (4), a baffle (5) and a safety rope (9), the fixed mount (2) is mounted on the edge of a containing recess (10), the tablet personal computer (4) is mounted on the fixed mount (2), the baffle (5) is fastened on the top of the tablet personal computer (4), the movable mount (3) is articulated with the tablet personal computer (4) through tenons (6), and the safety rope (9) is connected between the tablet personal computer (4) and the table board (1). The assembly of the tablet personal computer support includes the following sub-steps: (S10) mounting of the tenons; (S12) mounting of the safety rope; (S13) fixed assembly; and (S14) inclination angle adjustment. The disassembly of the tablet personal computer support includes the following sub-steps: (S21) dismounting of the tenons; (S22) dismounting of the baffle; and (S23) dismounting of the safety rope. The tablet personal computer support has the advantages that the structure of the tablet personal computer support is simple, the tablet personal computer support is convenient to use, and a comfortable ride environment can be provided for passengers.
Description
Technical field
The present invention relates to a kind of Flat computer support frame, particularly be installed on Flat computer support frame and using method thereof on the aircraft seat.
Background technology
Along with improving constantly and scientific and technical development of people's living standard, airplane becomes the inevitable choice of people's long journey, so that the passenger can arrive the destination at short notice, this both saved time to the passenger, made again the passenger have on the road a comfortable environment of taking.But people improve constantly the requirement of quality of life, provided Secretary for the modern vehicle, the passenger is when long-time airplane, tend to feel very boring, because can not play aboard generally speaking mobile phone can not make a phone call again, and can not arbitrarily walk about, so airplane has also become passenger's journey bad dream of long journey gradually.
Panel computer is popular converter tools in modern times, its volume is little, can play games, see a film, surf the Net, that have even can make a phone call, this is undoubtedly a kind of good converter tools concerning people, if can be equipped with a panel computer on each seat aboard, bring many enjoyment will for these passengers, so that the passenger when airplane, can play single-play game or see a film, and can not feel the boring of long-distance route.But the installation site and the installation method that panel computer are installed in the seat all are the difficult problems that need to capture.
Chinese patent 201110162852.7 discloses a kind of Flat computer support frame, places panel computer at the placement plate that S. A. is flexibly connected.This device is panel computer to be placed directly in place on the plate, and can't adjust according to passenger's needs the angle of panel computer, and the passenger may be inconvenient when watching film.
Chinese patent 201110032168.7 discloses a kind of Flat computer support frame, comprise base, be installed in left rotation and right rotation support and swinging strut up and down on the base, be provided with fixed frame and the splicing ear of fixed flat planar computer on the described left rotation and right rotation support, described up and down swinging strut and base are hinged by metal rotating shaft, keep rotary support and the location of 0～75 ° of panel computer front and back by this rotating shaft; Described left rotation and right rotation support rotary connection is on swinging strut up and down, but left and right sides moving rotary and location.About the support of this programme can be realized pause in 0～75 ° of optional position in 90 ° rotation and front and back, and the rotation of energy support plate computer weight.But the complex structure of this Flat computer support frame, when being installed on the aircraft seat small table plate behind, floor area is larger.
Summary of the invention
The object of the invention is to overcome the shortcoming of prior art, provide a kind of simple in structure, esy to use, safe and reliable and can be the passenger comfortable Flat computer support frame and the using method thereof on the aircraft seat of being installed on of taking environment is provided.
Purpose of the present invention is achieved through the following technical solutions: be installed on the Flat computer support frame on the aircraft seat, table, fixed support, travel(l)ing rest, panel computer, baffle plate and safety rope, table is plank frame, the back side of table offers holding tank, edge at holding tank is equipped with fixed support, panel computer is installed on the fixed support, baffle plate is fastened on the top of panel computer, also be provided with travel(l)ing rest between panel computer and the fixed support, the top of travel(l)ing rest is provided with at least two trip mount pads, trip is installed in the trip mount pad, travel(l)ing rest and panel computer are hinged and connected by trip, are connected with safety rope between the dorsal part of panel computer and the dorsal part of table.
The middle part of described travel(l)ing rest offers ventilative opening.
Its using method comprises a use substep in place and the use substep of offing normal, and wherein, use substep in place comprises:
S10, trip are equipped: the top of panel computer is cooperated with trip mount pad on the travel(l)ing rest, with trip travel(l)ing rest and panel computer are coupled together;
S12, assembling safety rope: an end of safety rope is locked in the holding tank middle part of table, the other end of safety rope is passed the middle part of travel(l)ing rest, and be locked in the dorsal part of panel computer;
S13, fixing assembling: panel computer is fixedly mounted on the fixed support by baffle plate;
S14, adjustment angle of inclination: adjust the angle of inclination of panel computer, the angular range between panel computer and the plane, table place is 0 °～80 °;
Off normal and use substep to comprise:
S21, the dismounting trip: with panel computer with the table plane, place, limit angular adjustment be 0 °, take off trip;
S22, tear baffle plate open: with the hand steered panel computer of living, remove baffle plate, take off panel computer.
Described offing normal uses step also to comprise the substep of dismantling safety rope.
The present invention has the following advantages:
1, the present invention directly the table dorsal part on the back of cabin install fixed support additional, need not change the original structure of table, and it is simple in structure, installing/dismounting is all very convenient.
2, when the passenger wants to watch film, with the angle of hand adjustment screed computer, feel comfortable position until adjust to passenger oneself, trip can keep this angle of inclination; When the passenger wants to play games, the trip at panel computer top is taken off, panel computer is separated with fixed support, just easily amusement.
3, between table and panel computer, be connected with a safety rope, only have the crew member just can open latching device by special key, prevent that panel computer from losing, and safety rope can play prevent that panel computer from dropping on the ground simultaneously.
4, panel computer is applied in the airline traveling, except reading or newspaper, many again many entertainment way are for the passenger provides the more comfortable environment of taking when making passenger's airplane, so that the passenger can not feel boring in long route, improved the service quality of airline traveling.
Description of drawings
Fig. 1 is structural representation of the present invention;
Fig. 2 is the structural representation of travel(l)ing rest;
Among the figure: 1-table, 2-fixed support, 3-travel(l)ing rest, 4-panel computer, 5-baffle plate, 6-trip, 7-trip mount pad, the 8-opening of breathing freely, 9-safety rope, 10-holding tank.
The specific embodiment
The present invention will be further described below in conjunction with accompanying drawing, but protection scope of the present invention is not limited to the following stated.
As shown in Figure 1, be installed on the Flat computer support frame on the aircraft seat, table 1, fixed support 2, travel(l)ing rest 3, panel computer 4, baffle plate 5 and safety rope 9, table 1 is plank frame, the back side of table 1 offers holding tank 10, at the edge of holding tank 10 fixed support 2 is installed, panel computer 4 is installed on the fixed support 2, baffle plate 5 is fastened on the top of panel computer 4, also be provided with travel(l)ing rest 3 between panel computer 4 and the fixed support 2, the top of travel(l)ing rest 3 is provided with at least two trip mount pads 7, trip 6 is installed in the trip mount pad 7, travel(l)ing rest 3 is hinged and connected by trip 6 with panel computer 4, is connected with safety rope 9 between the dorsal part of the dorsal part of panel computer 4 and table 1.
As shown in Figure 2, the middle part of travel(l)ing rest 3 offers ventilative opening 8.
Its using method comprises a use substep in place and the use substep of offing normal, and wherein, use substep in place comprises:
S10, trip are equipped: the top of panel computer 4 is cooperated with trip mount pad 7 on the travel(l)ing rest 3, with trip 6 travel(l)ing rest 3 and panel computer 4 are coupled together;
S12, assembling safety rope: an end of safety rope 9 is locked in holding tank 10 middle parts of table 1, the other end of safety rope 9 is passed the middle part of travel(l)ing rest 3, and be locked in the dorsal part of panel computer 4;
S13, fixing assembling: panel computer 4 is fixedly mounted on the fixed support 2 by baffle plate 5;
S14, adjustment angle of inclination: adjust the angle of inclination of panel computer 4, the angular range between panel computer 4 and the plane, table 1 place is 0 °～80 °;
Off normal and use substep to comprise:
S21, dismounting trip: be 0 ° with the angular adjustment on panel computer 4 and table plane, 1 place, limit, take off trip 6;
S22, tear baffle plate open: with the hand steered panel computer 4 of living, remove baffle plate 5, take off panel computer 4.
Described offing normal uses step also to comprise the substep of dismantling safety rope 9.
When the passenger wants to watch film, with the angle of hand adjustment screed computer 4, feel comfortable position until adjust to passenger oneself, trip 6 can keep these angles of inclination; When the passenger wants to play games, the trip 6 at panel computer 4 tops is taken off, panel computer 6 is separated with fixed support 2, just easily amusement.When needs charged or safeguard, bus attendant was opened the blocking device at safety rope 9 two ends with private key after panel computer 6 and fixed support 2 are separated, and takes off panel computer 4.
Claims (4)
1. be installed on the Flat computer support frame on the aircraft seat, it is characterized in that: table (1), fixed support (2), travel(l)ing rest (3), panel computer (4), baffle plate (5) and safety rope (9), table (1) is plank frame, the back side of table (1) offers holding tank (10), at the edge of holding tank (10) fixed support (2) is installed, panel computer (4) is installed on the fixed support (2), baffle plate (5) is fastened on the top of panel computer (4), also be provided with travel(l)ing rest (3) between panel computer (4) and the fixed support (2), the top of travel(l)ing rest (3) is provided with at least two trip mount pads (7), trip (6) is installed in the trip mount pad (7), travel(l)ing rest (3) is hinged and connected by trip (6) with panel computer (4), is connected with safety rope (9) between the dorsal part of the dorsal part of panel computer (4) and table (1).
2. the Flat computer support frame that is installed on the aircraft seat according to claim 1, it is characterized in that: the middle part of described travel(l)ing rest (3) offers ventilative opening (8).
3. the using method that is installed on the Flat computer support frame on the aircraft seat according to claim 1, it is characterized in that: it comprises a use substep in place and the use substep of offing normal, and wherein, use substep in place comprises:
S10, trip are equipped: the top of panel computer (4) is cooperated with trip mount pad (7) on the travel(l)ing rest (3), with trip (6) travel(l)ing rest (3) and panel computer (4) are coupled together;
S12, assembling safety rope: an end of safety rope (9) is locked in holding tank (10) middle part of table (1), the other end of safety rope (9) is passed the middle part of travel(l)ing rest (3), and be locked in the dorsal part of panel computer (4);
S13, fixing assembling: panel computer (4) is fixedly mounted on the fixed support (2) by baffle plate (5);
S14, adjustment angle of inclination: adjust the angle of inclination of panel computer (4), the angular range between panel computer (4) and table (1) plane, place is 0 °～80 °;
Off normal and use substep to comprise:
S21, the dismounting trip: with panel computer (4) with the table plane, place, limit (1) angular adjustment be 0 °, take off trip (6);
S22, tear baffle plate open: with the hand steered panel computer (4) of living, remove baffle plate (5), take off panel computer (4).
4. the using method that is installed on the Flat computer support frame on the aircraft seat according to claim 3 is characterized in that: described offing normal uses step also to comprise the substep of dismounting safety rope (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310026717.9A CN103072694B (en) | 2013-01-24 | 2013-01-24 | Usage of tablet personal computer support mounted on aircraft chair |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310026717.9A CN103072694B (en) | 2013-01-24 | 2013-01-24 | Usage of tablet personal computer support mounted on aircraft chair |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103072694A true CN103072694A (en) | 2013-05-01 |
| CN103072694B CN103072694B (en) | 2014-11-12 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310026717.9A Expired - Fee Related CN103072694B (en) | 2013-01-24 | 2013-01-24 | Usage of tablet personal computer support mounted on aircraft chair |
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| Country | Link |
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| CN (1) | CN103072694B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104456023A (en) * | 2014-12-04 | 2015-03-25 | 石家庄飞机工业有限责任公司 | Mounting bracket for display in small general-purpose aircraft cabin |
| US11008103B1 (en) | 2019-10-28 | 2021-05-18 | B/E Aerospace, Inc. | Aircraft cabin apparatus including personal electronic device holder |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102121556A (en) * | 2011-01-29 | 2011-07-13 | 深圳市奋达科技股份有限公司 | Flat-panel computer bracket |
| CN102252150A (en) * | 2011-06-16 | 2011-11-23 | 陈日铃 | Tablet personal computer bracket |
| WO2012129116A2 (en) * | 2011-03-18 | 2012-09-27 | Skycast Solutions Inc. | In-flight entertainment system |
| US20120248833A1 (en) * | 2011-04-04 | 2012-10-04 | Be Aerospace, Inc. | Seatback holder for tablet computers |
| CN203172887U (en) * | 2013-01-24 | 2013-09-04 | 成都富凯飞机工程服务有限公司 | Tablet computer support installed on seat of plane |
-
2013
- 2013-01-24 CN CN201310026717.9A patent/CN103072694B/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102121556A (en) * | 2011-01-29 | 2011-07-13 | 深圳市奋达科技股份有限公司 | Flat-panel computer bracket |
| WO2012129116A2 (en) * | 2011-03-18 | 2012-09-27 | Skycast Solutions Inc. | In-flight entertainment system |
| US20120248833A1 (en) * | 2011-04-04 | 2012-10-04 | Be Aerospace, Inc. | Seatback holder for tablet computers |
| CN102252150A (en) * | 2011-06-16 | 2011-11-23 | 陈日铃 | Tablet personal computer bracket |
| CN203172887U (en) * | 2013-01-24 | 2013-09-04 | 成都富凯飞机工程服务有限公司 | Tablet computer support installed on seat of plane |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104456023A (en) * | 2014-12-04 | 2015-03-25 | 石家庄飞机工业有限责任公司 | Mounting bracket for display in small general-purpose aircraft cabin |
| US11008103B1 (en) | 2019-10-28 | 2021-05-18 | B/E Aerospace, Inc. | Aircraft cabin apparatus including personal electronic device holder |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103072694B (en) | 2014-11-12 |
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Granted publication date: 20141112 Termination date: 20180124 |
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| CF01 | Termination of patent right due to non-payment of annual fee |