CN102774500A - Airplane cabin curtain assembly - Google Patents
Airplane cabin curtain assembly Download PDFInfo
- Publication number
- CN102774500A CN102774500A CN2012102676039A CN201210267603A CN102774500A CN 102774500 A CN102774500 A CN 102774500A CN 2012102676039 A CN2012102676039 A CN 2012102676039A CN 201210267603 A CN201210267603 A CN 201210267603A CN 102774500 A CN102774500 A CN 102774500A
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- China
- Prior art keywords
- guide rail
- distance
- stake body
- curtain
- sliding sleeve
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- 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.)
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Abstract
The invention discloses an airplane cabin curtain assembly, which comprises a middle curtain assembly and a left and right curtain assembly, wherein the middle curtain assembly comprises a guide rail A (1), a guide rail B (2) and a middle curtain support (3), and the guide rail A (1) and the guide rail B (2) are arranged on a big luggage carrier (4) of the cabin; the middle curtain support (3) comprises a support body A (5), a sliding sleeve A (6), a fixed support rod (7), a sliding support rod (8), a sliding sleeve B (9) and a locking device (10); the sliding sleeve A (6) is movably sheathed on the guide rail A (1), and the sliding sleeve B (9) is movably sheathed on the guide rail B (2); and the left and right curtain assembly comprises a pre-installed base (13) and a left and right curtain support (14). The airplane cabin curtain assembly has the beneficial effects that the airplane cabin curtain assembly is conveniently installed on an airplane on the basis that the original structure of the airplane is not damaged, so that the influence on the airplane safety is reduced, and the construction difficulty is reduced; and the installation structure is simple and convenient and is easily regulated, and the installation structure is firmly and stably fixed.
Description
Technical field
The present invention relates to a kind of aircraft passenger compartment at a distance from curtain component.
Background technology
In the existing aircaft configuration, be not provided with in the aircraft passenger compartment that has, influence the comfort level of passenger's travelling at a distance from curtain structure; And in existing aircaft configuration, set up at a distance from curtain structure; Just must transform the existing structure arrangement of aircraft, operation easier is big, and the separated curtain limited amount that can increase; Can not satisfy passenger's demand, and the transformation of aircaft configuration also can be threatened to the safe operation of aircraft.
Summary of the invention
The objective of the invention is to overcome the shortcoming of prior art, providing a kind of provides multi-faceted aircraft passenger compartment at a distance from curtain separated curtain component for the passenger on the basis that does not change the aircraft existing structure.
The object of the invention is realized through following technical scheme: aircraft passenger compartment is at a distance from curtain component, during it comprises at a distance from curtain component with about at a distance from curtain component, described at a distance from curtain component comprise guide rail A, guide rail B and at a distance from the curtain support; Guide rail A and guide rail B are symmetrical set, and guide rail A is arranged on the big baggage container of main cabin one side, and guide rail B is arranged on the big baggage container of opposite side in main cabin; In comprise stake body A, sliding sleeve A, fixing branch strut, sliding supporting bar, sliding sleeve B and latching device at a distance from the curtain support; Be provided with the strut bar guide rail in the stake body A, fixing branch strut and sliding supporting bar all are arranged in the strut bar guide rail of stake body A, and fixing branch strut and sliding supporting bar are divided into the both sides of stake body A; The fixing branch strut is captiveed joint with stake body A; Latching device is fixedly installed in the end that stake body A connects sliding supporting bar, and sliding supporting bar passes latching device and is movably set in stake body A, and the outside of stake body A is provided with and latching device bonded assembly operating handle; The end of fixing branch strut connects sliding sleeve A; Sliding sleeve A movable set is on guide rail A, and the end of movable support rod connects sliding sleeve B, and sliding sleeve B movable set is on guide rail B;
About described at a distance from curtain component comprise the prepackage base with about at a distance from the curtain support; The two ends of prepackage base are respectively arranged with row's latch hook; Also be provided with two connecting bores on the prepackage base; The latch hook of prepackage base through both sides is installed on the PSU panel mounting guide rail, about comprise stake body B and be fixedly arranged on the attaching parts on the stake body B that at a distance from the curtain support attaching parts is provided with two joint pins that cooperate with connecting bore; Attaching parts is connected with the prepackage base through joint pin, and the below of described stake body A and stake body B all is equipped with at a distance from curtain.
Described guide rail A and guide rail B constitute by a front slideway, several stage casing guide rails and an end rails; Between front slideway and stage casing guide rail, between the guide rail of adjacent stage casing, all be connected between stage casing guide rail and end rails through connecting pin; The leading section of front slideway is equipped with the front position-arresting sheet, and the rearward end of end rails is equipped with the rear position-arresting sheet.
Described front slideway, stage casing guide rail and end rails are by track base and be fixed in track base upper rail portion formation, and track base is installed on big baggage container top through bolt.
Described joint pin is made up of guidepost and the tenon that is arranged at guidepost top, and tenon and guidepost are set for the eccentric, and also are provided with control handle on the attaching parts, and control handle is connected with tenon through driving device.
The present invention has the following advantages: the present invention can be installed on the aircraft on the basis of not destroying original structure on the aircraft easily, thereby has reduced the influence to aircraft safety, has reduced the difficulty of construction; Can be simultaneously for the passenger in whole main cabin provide multi-faceted separated curtain, thus the comfort level of passenger's airplane improved, be beneficial to passenger's rest; Mounting structure is simple and convenient, is prone to regulate, and is fixed firm.
Description of drawings
Fig. 1 be of the present invention at a distance from the structural representation of curtain component
Fig. 2 be of the present invention at a distance from the plan structure scheme drawing of curtain component
Fig. 3 is the structural representation of guide rail of the present invention
Fig. 4 be of the present invention about at a distance from the structural representation of curtain component
Fig. 5 is the structural representation of prepackage base of the present invention
Among the figure, 1-guide rail A, 2-guide rail B, separated curtain support among the 3-, the big baggage container of 4-, 5-stake body A, 6-sliding sleeve A; 7-fixing branch strut, the 8-sliding supporting bar, 9-sliding sleeve B, the 10-latching device, 11-strut bar guide rail, the 12-operating handle, 13-pre-installs base; Separated curtain support about 14-, 15-latch hook, 16-connecting bore, 17-stake body B, 18-attaching parts, 19-joint pin; 20-is at a distance from curtain, 21-front slideway, 22-stage casing guide rail, 23-end rails, 24-connecting pin, 25-front position-arresting sheet; 26-rear position-arresting sheet, 27-track base, 28-rail portion, 29-guidepost, 30-tenon, 31-control handle.
The specific embodiment
Below in conjunction with accompanying drawing the present invention is done further description, protection scope of the present invention is not limited to the following stated:
Like Fig. 1, shown in Figure 2, aircraft passenger compartment is at a distance from curtain component, during it comprises at a distance from curtain component with about at a distance from curtain component; In described at a distance from curtain component comprise guide rail A1, guide rail B2 and at a distance from curtain support 3, guide rail A1 and guide rail B2 are symmetrical set, guide rail A1 is arranged on the big baggage container 4 of main cabin one side; Guide rail B2 is arranged on the big baggage container 4 of opposite side in main cabin, in comprise stake body A5, sliding sleeve A6, fixing branch strut 7, sliding supporting bar 8, sliding sleeve B9 and latching device 10 at a distance from curtain support 3, be provided with strut bar guide rail 11 in the stake body A5; Fixing branch strut 7 all is arranged in the strut bar guide rail 11 of stake body A5 with sliding supporting bar 8; And fixing branch strut 7 and sliding supporting bar 8 are divided into the both sides of stake body A5, and fixing branch strut 7 is captiveed joint with stake body A5, and latching device 10 is fixedly installed in the end that stake body A5 connects sliding supporting bar 8; Sliding supporting bar 8 passes latching device 10 and is movably set in stake body A5's; The outside of stake body A5 is provided with and latching device 10 bonded assembly operating handles 12, and the end of fixing branch strut 7 connects sliding sleeve A6, and sliding sleeve A6 movable set is on guide rail A1; The end of movable support rod connects sliding sleeve B9, and sliding sleeve B movable set is on guide rail B2;
Like Fig. 4, shown in Figure 5; About described at a distance from curtain component comprise prepackage base 13 with about at a distance from curtain support 14; The two ends of prepackage base 13 are respectively arranged with row's latch hook 15, also are provided with two connecting bores 16 on the prepackage base 13, and prepackage base 13 is installed on the PSU panel mounting guide rail through the latch hook 15 of both sides; About comprise stake body B17 and be fixedly arranged on the attaching parts 18 on the stake body B17 at a distance from curtain support 14; Attaching parts 18 is provided with two joint pins 19 that cooperate with connecting bore 16, and attaching parts 18 is connected with prepackage base 13 through joint pin 19, and the below of described stake body A5 and stake body B17 all is equipped with at a distance from curtain 20.
As shown in Figure 3; Described guide rail A1 and guide rail B2 constitute by a front slideway 21, several stage casing guide rails 22 and an end rails 23; Front slideway 21 all is connected through connecting pin 24 with 23 of end rails with 22 on stage casing guide rail, 22 on adjacent stage casing guide rail, stage casing guide rail 22; Connecting pin 24 comprises a front end and the rear end that diameter is bigger that diameter is less; The end that is positioned at the guide rail of connecting pin 24 front ends has a pin-and-hole A who cooperates with connecting pin 24 front ends, and the front end that is positioned at the guide rail of connecting pin 24 rear ends has a pin-and-hole B who cooperates with connecting pin 24 rear ends, and is provided with a spring between pin-and-hole B and connecting pin 24 rear ends; The leading section of front slideway 21 is equipped with front position-arresting sheet 25; The rearward end of end rails 23 is equipped with rear position-arresting sheet 26, and described front slideway 21, stage casing guide rail 22 and end rails 23 are by track base 27 and be fixed in track base 27 upper rail portions 28 and constitute, and track base 27 is installed on big baggage container 4 tops through bolt.
As shown in Figure 4, described joint pin 19 is made up of guidepost 29 and the tenon 30 that is arranged at guidepost 29 tops, and tenon 30 is set for the eccentric with guidepost 29, also is provided with control handle 31 on the attaching parts 18, and control handle 31 is connected with tenon 30 through driving device.When control handle 31 was opened, tenon 30 rotated under the driving of control handle 31, and final tenon 30 is positioned at same cylinder with guidepost 29; The joint pin 19 of attaching parts 18 is deeply pre-installed in the connecting bore 16 of base 13, and tenon 30 exceeds the upper surface of pre-installing base 13, at this moment; Control handle 31 is closed; Control handle 31 is through 30 rotations of driving device control tenon, and final tenon 30 moves to and guidepost 29 accentric positions, and the lower surface of tenon 30 compresses the upper surface with prepackage base 13; Tenon 30 will be pre-installed base 13 and be pressed on the attaching parts 18, realize connecting fixing.
During use, at a distance from curtain component, through operating handle 12 unlatching-locking apparatus 10; The length that the adjustment movable support rod stretches out stake body A5 is set with sliding sleeve A6 and sliding sleeve B9 on guide rail A1 and guide rail B2, slides along guide rail A1 and guide rail B2 at a distance from curtain support 3 in the promotion; It is central when curtain support 3 reaches the desired location; The adjustment movable support rod makes fixing branch strut 7 and sliding supporting bar 8 produce a squeese pressure to sliding sleeve A6 and sliding sleeve B9 respectively, makes sliding sleeve A6 and sliding sleeve B9 compress track A and track B respectively, pulls operating handle 12 then; Close latching device 10, fixing at a distance from curtain component in the realization.And for about at a distance from curtain component, during use, at first will pre-install the latch hook 15 of base 13 through both sides to be installed on the PSU panel mounting guide rail, then through joint pin 19 with about be installed at a distance from curtain support 14 and pre-install on the base 13.
Claims (4)
1. aircraft passenger compartment is at a distance from curtain component; It is characterized in that: during it comprises at a distance from curtain component with about at a distance from curtain component; In described at a distance from curtain component comprise guide rail A (1), guide rail B (2) with in separated curtain support (3); Guide rail A (1) and guide rail B (2) are symmetrical set, and guide rail A (1) is arranged on the big baggage container of main cabin one side (4), and guide rail B (2) is arranged on the big baggage container of opposite side (4) in main cabin; In comprise stake body A (5), sliding sleeve A (6), fixing branch strut (7), sliding supporting bar (8), sliding sleeve B (9) and latching device (10) at a distance from curtain support (3); Be provided with strut bar guide rail (11) in the stake body A (5), fixing branch strut (7) and sliding supporting bar (8) all are arranged in the strut bar guide rail (11) of stake body A (5), and fixing branch strut (7) and sliding supporting bar (8) are divided into the both sides of stake body A (5); Fixing branch strut (7) is captiveed joint with stake body A (5); Latching device (10) is fixedly installed in the end that stake body A (5) connects sliding supporting bar (8), and sliding supporting bar (8) passes latching device (10) and is movably set in stake body A (5), and the outside of stake body A (5) is provided with and latching device (10) bonded assembly operating handle (12); The end of fixing branch strut (7) connects sliding sleeve A (6); Sliding sleeve A (6) movable set is on guide rail A (1), and the end of movable support rod connects sliding sleeve B (9), and sliding sleeve B (9) movable set is on guide rail B (2);
About described at a distance from curtain component comprise prepackage base (13) with about separated curtain support (14); The two ends of prepackage base (13) are respectively arranged with row's latch hook (15); Also be provided with two connecting bores (16) on the prepackage base (13); Prepackage base (13) is installed on the PSU panel mounting guide rail through the latch hook (15) of both sides; About comprise stake body B (17) and be fixedly arranged on the attaching parts (18) on the stake body B (17) at a distance from curtain support (14); Attaching parts (18) is provided with two joint pins (19) that cooperate with connecting bore (16), and attaching parts (18) is connected with prepackage base (13) through joint pin (19), and the below of described stake body A (5) and stake body B (17) all is equipped with at a distance from curtain (20).
2. aircraft passenger compartment according to claim 1 is at a distance from curtain component; It is characterized in that: described guide rail A (1) and guide rail B (2) constitute by a front slideway (21), several stage casing guide rails (22) and an end rails (23); Between front slideway (21) and stage casing guide rail (22), between adjacent stage casing guide rail (22), all be connected between stage casing guide rail (22) and end rails (23) through connecting pin (24); The leading section of front slideway (21) is equipped with front position-arresting sheet (25), and the rearward end of end rails (23) is equipped with rear position-arresting sheet (26).
3. aircraft passenger compartment according to claim 2 is at a distance from curtain component; It is characterized in that: described front slideway (21), stage casing guide rail (22) and end rails (23) are by track base (27) and be fixed in track base (27) upper rail portion (28) formation, and track base (27) is installed on big baggage container (4) top through bolt.
4. aircraft passenger compartment according to claim 1 is at a distance from curtain component; It is characterized in that: described joint pin (19) is made up of guidepost (29) and the tenon (30) that is arranged at guidepost (29) top; Tenon (30) is set for the eccentric with guidepost (29); Also be provided with control handle (31) on the attaching parts (18), control handle (31) is connected with tenon (30) through driving device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012102676039A CN102774500A (en) | 2012-07-30 | 2012-07-30 | Airplane cabin curtain assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012102676039A CN102774500A (en) | 2012-07-30 | 2012-07-30 | Airplane cabin curtain assembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102774500A true CN102774500A (en) | 2012-11-14 |
Family
ID=47119657
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012102676039A Pending CN102774500A (en) | 2012-07-30 | 2012-07-30 | Airplane cabin curtain assembly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102774500A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103863564A (en) * | 2012-12-12 | 2014-06-18 | 波音公司 | Divider curtain |
| EP3290340A1 (en) * | 2016-08-30 | 2018-03-07 | Airbus Operations GmbH | Lateral linear moving curtain rail |
| CN108137156A (en) * | 2015-10-23 | 2018-06-08 | 庞巴迪公司 | For the freight space separator in birdman main cabin |
| US20190118947A1 (en) * | 2017-10-20 | 2019-04-25 | The Boeing Company | Systems and methods for adaptively positioning a cross-aisle curtain header assembly within a vehicle |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5086540A (en) * | 1989-07-10 | 1992-02-11 | Messerschmitt-Boelkow-Blohm Gmbh | Support mechanism for room dividers |
| DE4119623C1 (en) * | 1991-06-14 | 1992-10-15 | Deutsche Airbus Gmbh, 2000 Hamburg, De | Aircraft cabin partitions between seat groups - has fixed partition guide rails for manual handling, receiving partition fitted holders |
| EP0754621A1 (en) * | 1995-07-20 | 1997-01-22 | DaimlerChrysler Aerospace Airbus Gesellschaft mit beschränkter Haftung | Device to divide an aircraft cabin |
| DE10017410A1 (en) * | 2000-04-07 | 2001-10-18 | Eads Airbus Gmbh | Installation of furnishing components in an aircraft passenger cabin has carriers with holders to secure the components at each end for easy fitting and removal |
| FR2893002A1 (en) * | 2005-11-10 | 2007-05-11 | Adder Sa Sa | ASSEMBLY FOR GUIDING AN AIRCRAFT CABIN SPACE DIVISION HAVING ELECTRIC POWER SUPPLY MEANS |
| US20080229547A1 (en) * | 2005-11-10 | 2008-09-25 | Adder | Assembly for Guiding the Longitudinal Sliding Movement of a Sub-Assembly |
| WO2010102932A1 (en) * | 2009-03-12 | 2010-09-16 | Airbus Operations Gmbh | Ceiling panel having curtain rail in a transport means cabin |
| CN102317156A (en) * | 2009-01-23 | 2012-01-11 | 空中客车营运有限公司 | Screen for a passenger cabin |
| CN202765294U (en) * | 2012-07-30 | 2013-03-06 | 成都富凯飞机工程服务有限公司 | Air plane passenger cabin partition curtain assembly |
-
2012
- 2012-07-30 CN CN2012102676039A patent/CN102774500A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5086540A (en) * | 1989-07-10 | 1992-02-11 | Messerschmitt-Boelkow-Blohm Gmbh | Support mechanism for room dividers |
| DE4119623C1 (en) * | 1991-06-14 | 1992-10-15 | Deutsche Airbus Gmbh, 2000 Hamburg, De | Aircraft cabin partitions between seat groups - has fixed partition guide rails for manual handling, receiving partition fitted holders |
| EP0754621A1 (en) * | 1995-07-20 | 1997-01-22 | DaimlerChrysler Aerospace Airbus Gesellschaft mit beschränkter Haftung | Device to divide an aircraft cabin |
| DE10017410A1 (en) * | 2000-04-07 | 2001-10-18 | Eads Airbus Gmbh | Installation of furnishing components in an aircraft passenger cabin has carriers with holders to secure the components at each end for easy fitting and removal |
| FR2893002A1 (en) * | 2005-11-10 | 2007-05-11 | Adder Sa Sa | ASSEMBLY FOR GUIDING AN AIRCRAFT CABIN SPACE DIVISION HAVING ELECTRIC POWER SUPPLY MEANS |
| US20080229547A1 (en) * | 2005-11-10 | 2008-09-25 | Adder | Assembly for Guiding the Longitudinal Sliding Movement of a Sub-Assembly |
| CN102317156A (en) * | 2009-01-23 | 2012-01-11 | 空中客车营运有限公司 | Screen for a passenger cabin |
| WO2010102932A1 (en) * | 2009-03-12 | 2010-09-16 | Airbus Operations Gmbh | Ceiling panel having curtain rail in a transport means cabin |
| CN202765294U (en) * | 2012-07-30 | 2013-03-06 | 成都富凯飞机工程服务有限公司 | Air plane passenger cabin partition curtain assembly |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103863564A (en) * | 2012-12-12 | 2014-06-18 | 波音公司 | Divider curtain |
| CN103863564B (en) * | 2012-12-12 | 2018-01-05 | 波音公司 | Separator curtain |
| CN108137156A (en) * | 2015-10-23 | 2018-06-08 | 庞巴迪公司 | For the freight space separator in birdman main cabin |
| EP3290340A1 (en) * | 2016-08-30 | 2018-03-07 | Airbus Operations GmbH | Lateral linear moving curtain rail |
| US20190118947A1 (en) * | 2017-10-20 | 2019-04-25 | The Boeing Company | Systems and methods for adaptively positioning a cross-aisle curtain header assembly within a vehicle |
| US10737788B2 (en) * | 2017-10-20 | 2020-08-11 | The Boeing Company | Systems and methods for adaptively positioning a cross-aisle curtain header assembly within a vehicle |
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| PB01 | Publication | ||
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Application publication date: 20121114 |