CN201587537U - Position regulating device of aero seat - Google Patents

Position regulating device of aero seat Download PDF

Info

Publication number
CN201587537U
CN201587537U CN2009202896615U CN200920289661U CN201587537U CN 201587537 U CN201587537 U CN 201587537U CN 2009202896615 U CN2009202896615 U CN 2009202896615U CN 200920289661 U CN200920289661 U CN 200920289661U CN 201587537 U CN201587537 U CN 201587537U
Authority
CN
China
Prior art keywords
support component
assembly
adjusting position
base
sliding support
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.)
Expired - Fee Related
Application number
CN2009202896615U
Other languages
Chinese (zh)
Inventor
刘进
熊彬
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
AVIC HUBEI ALI-JIATAI AIRCRAFT EQUIPMENT CO., LTD.
Original Assignee
AVIC Aerospace Life Support Industries Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by AVIC Aerospace Life Support Industries Ltd filed Critical AVIC Aerospace Life Support Industries Ltd
Priority to CN2009202896615U priority Critical patent/CN201587537U/en
Application granted granted Critical
Publication of CN201587537U publication Critical patent/CN201587537U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Landscapes

  • Chairs Characterized By Structure (AREA)

Abstract

The utility model relates to a position regulating device of an aero seat. The position regulating device comprises a sitting panel (13) and a base (2), wherein the sitting panel (13) is arranged on the base (2); and a sitting plate and a backrest of the seat are arranged above the sitting panel (13). The position regulating device also comprises a seat pan component (1), a sliding frame component (7) and a framework component (21), wherein the upper part of the base (2) is fixedly connected with the framework component (21); the framework component (21) is arranged on the sliding frame component (7) and is slidingly connected with the sliding frame component (7); the sliding frame component (7) is arranged in the seat pan component (1) and is slidingly connected with the seat pan component (1); and the sitting panel (13) is fixed at the upper part of the seat pan component (1). The position regulating device is completed by the seat pan component, the sliding frame component and the framework component that are arranged between the sitting panel and the base, and a sliding rail does not need to be arranged on the floor of an airplane, so that the occupied area of the seat on the floor of the airplane can be reduced, the seat does not need to be cleaned often, and the maintenance workload is small.

Description

A kind of apparatus for adjusting position of aero seat
Technical field
The utility model relates to seat, the apparatus for adjusting position of the aero seat that is specifically related to use aboard, particularly aero seat.
Background technology
Some aero seats have position adjustment function, seat of taking as big aircraft flight person etc., and the apparatus for adjusting position of existing aero seat adopts the carriage of seat bottom mounting strap track more.Track need be connected with floor when adopting this rail set, position, required hole is bigger than multiposition.Slide rail is exposed on the floor and damages easily, often adsorbs impurity such as a large amount of dusts because of the cause of lubricant again, needs often cleaning, and the work capacity of maintenance is big.
The utility model content
Technical problem to be solved in the utility model is: a kind of apparatus for adjusting position of aero seat is provided, and this apparatus for adjusting position makes aero seat need not to be provided with slide rail on floor.
The utility model solves the problems of the technologies described above the technical scheme that is adopted:
A kind of apparatus for adjusting position of aero seat, it comprises sits panel and base, sits panel and is arranged on the base, and the seat of seat and backrest are arranged on the top of sitting panel; Apparatus for adjusting position also comprises chair basin assembly, sliding support component and frame assembly; Captive joint with frame assembly in the top of base; Frame assembly is arranged on the sliding support component, and with the sliding support component sliding block joint; Sliding support component is arranged in the chair basin assembly, and with chair basin assembly sliding block joint; Sit panel and be fixed on chair basin assembly top.
In the such scheme, sliding support component comprises the slip steel pipe, and frame assembly comprises the sliding sleeve that is enclosed within on the slip steel pipe, and frame assembly is by slip steel pipe and sliding sleeve and sliding support component sliding block joint.
In the such scheme, the chair basin assembly is provided with slide rail, and sliding support component is provided with the pulley that is used for sliding on slide rail, and sliding support component is by pulley and slide rail and chair basin assembly sliding block joint.
In the such scheme, the slip steel pipe is vertical mutually with slide rail.
In the such scheme, the slide rail on the chair basin assembly is two, and two slide rails are parallel to each other, and two slide rails side is respectively equipped with the tooth bar parallel with slide rail, and sliding support component is provided with respectively and meshes two gears with two tooth bars, the axial connecting rod captive joint that passes through of two gears.
In the such scheme, the bottom of sitting panel is provided with limit guide rail, and the top of base is provided with the location pulley that is used for sliding on limit guide rail.
In the such scheme, described location pulley is two, and two location pulleys are separately positioned on the both sides of limit guide rail.
In the such scheme, the bottom of sitting panel also has the horizontal location hole, and the top of base is provided with the locating dowel pin assembly that cooperates with the horizontal location hole.
In the such scheme, base is tower lifting structure assembly.
In the such scheme, base inside is provided with gas spring.
Compared with prior art, the utlity model has following advantage:
1, position adjustments is finished by being arranged on chair basin assembly, sliding support component and the frame assembly sat between panel and the base, need not slide rail is set on floor, thereby has reduced the area of seat occupancy floor, need not frequent cleaning, and maintenance workload is little.
2, frame assembly is by slip steel pipe and sliding sleeve and sliding support component sliding block joint, and sliding support component is by pulley and slide rail and chair basin assembly sliding block joint, and annexation is simple, Stability Analysis of Structures.
3, the slip steel pipe is vertical mutually with slide rail, can guarantee that seat is to any horizontal direction adjustment.
4, two slide rails side is respectively equipped with the tooth bar parallel with slide rail, sliding support component is provided with respectively and meshes two gears with two tooth bars, the axial connecting rod captive joint that passes through of two gears, guarantee that pulley rotates synchronously on two slide rails, the not quite identical tight plug phenomenon that produces of avoiding sliding support component and chair basin assembly may cause by sense of motion owing to the slit of assembling generation.
5, the bottom of seat panel is provided with limit guide rail, and the direction front and back and the side-to-side movement of the seat panel limit guide rail regulation of seat are avoided carrying out simultaneously front and back and horizontally slipped.
6, the bottom of seat panel also has the horizontal location hole, and the top of base is provided with the locating dowel pin assembly that cooperates with the horizontal location hole, and people can realize the locking and unlocking of seat position by control locating dowel pin assembly.
7, base is tower lifting structure assembly, can carry out lifting to seat.
8, base inside is provided with gas spring, and gas spring can provide power upwards during the seat upward movement.
Description of drawings
Fig. 1 is the lateral plan of the utility model embodiment
Fig. 2 is the structural representation of the utility model embodiment
Fig. 3 is the utility model embodiment birds-eye view (after hiding the seat panel)
Fig. 4 is the A-A cutaway view of Fig. 3
Fig. 5 is the B-B cutaway view of Fig. 3
Fig. 6 is for sitting the upward view of panel
Fig. 7 is the structural representation of chair basin assembly
Fig. 8 is the structural representation of sliding support component and frame assembly
Fig. 9 is the structural representation of frame assembly
Wherein: 1-chair basin assembly, 2-base, three grades of towers of 3-, 4-gib block, 5-secondary tower, 6-one-level tower, 7-sliding support component, the horizontal spacing hole of 8-, 9-limit guide rail, the little location of 10-pulley, the big location of 11-pulley, 12-ball screw assembly,, 13-sit panel, 14-limiting stopper, 15-tooth bar, 16-slide rail, 17-connecting rod, 18-gear, 19-pulley, 20-slip steel pipe, 21-frame assembly, 22-gas spring, 23-locating dowel pin assembly, 24-sliding sleeve.
The specific embodiment
The utility model will be further described below in conjunction with drawings and Examples:
As shown in Figure 1, 2, the apparatus for adjusting position embodiment of the utility model aero seat comprises seat panel 13 and base 2, sits panel 13 and is arranged on the base 2, and the seat of seat and backrest are arranged on the top of sitting panel 13.
Shown in Fig. 2,3, the apparatus for adjusting position embodiment of the utility model aero seat also comprises chair basin assembly 1, sliding support component 7 and frame assembly 21; Captive joint with frame assembly 21 in the top of base 2; Frame assembly 21 is arranged on the sliding support component 7, and with sliding support component 7 sliding block joints; Sliding support component 7 is arranged in the chair basin assembly 1, and with chair basin assembly 1 sliding block joint; Sit panel 13 and be fixed on chair basin assembly 1 top.
Shown in Fig. 6,7,8,9, sliding support component 7 comprises slip steel pipe 20, frame assembly 21 comprises the sliding sleeve 24 that is enclosed within on the slip steel pipe 20, and frame assembly 21 is by slip steel pipe 20 and sliding sleeve 24 and sliding support component 7 sliding block joints, and sliding support component 7 horizontally slips on frame assembly 21.
Chair basin assembly 1 is provided with two slide rails 16, each slide rail 16 two ends is respectively equipped with limiting stopper 14, sliding support component 7 is provided with and is used for the pulley 19 that slides on slide rail 16, sliding support component 7 is by pulley 19 and slide rail 16 and chair basin assembly 1 sliding block joint, and the chair basin assembly can slide front and back on sliding support component 7.Article two, slide rail 16 is parallel to each other, and two slide rails 16 are other to be respectively equipped with the tooth bar 15 parallel with slide rail 16, sliding support component 7 be provided with respectively with 18, two gears 18 of two tooth bars, 15 two gears of engagement axially by a connecting rod 17 captive joints.
Slip steel pipe 20 is vertical mutually with slide rail 16.
Shown in Fig. 3,6, the bottom of sitting panel 13 is provided with limit guide rail 9, and limit guide rail 9 is " L " shape, and the top of base 2 is provided with and is used for the location pulley that slides on limit guide rail 9.Described location pulley is two, and one is little location pulley 10 and a big location pulley 11, and little location pulley 10 is arranged on the inboard of " L " shape limit guide rail, locatees the outside that pulley 11 is arranged on " L " shape limit guide rail greatly.
Shown in Fig. 4,5, the bottom of sitting panel 13 also has horizontal location hole 8, and the top of base 2 is provided with the locating dowel pin assembly 23 that cooperates with horizontal location hole 8.Locating dowel pin on the locating dowel pin assembly 23 can be realized locking by control cable wire up-and-down movement when locating dowel pin inserts in the horizontal spacing hole 8, otherwise, can slide.
Shown in Fig. 1,2,4,5, base 2 is tower lifting structure assembly, and base 2 inside are provided with gas spring 22.The tower lifting structure assembly of control perpendicular movement comprises one-level tower 6, secondary tower 5 and three grades of towers 3, wherein all be connected with gib block 4 on the outside four direction of secondary tower 5 and three grades of towers 3, the position-limited trough of one-level tower 6, secondary tower 5 inboards makes the gib block 4 on secondary tower 5, the three grades of towers 3 slide up and down in groove respectively.Sliding support component 7 is captiveed joint with three grades of tower 3 tops.
Base 2 central interior are provided with ball screw assembly, 12 and are the blocking device of core, realize the electrodeless adjusting of height of seat, and ball screw assembly, 12 is connected with three grades of towers 3, can be at an arbitrary position in stroke the height of tower structure be locked.The gravity that propulsive effort in the time of need moving downward is behaved, the power that makes progress that propulsive effort provides for gas spring 22 during upward movement.

Claims (10)

1. the apparatus for adjusting position of an aero seat, it comprises sits panel (13) and base (2), sits panel (13) and is arranged on the base (2), and the seat of seat and backrest are arranged on the top of seat panel (13); It is characterized in that: apparatus for adjusting position also comprises chair basin assembly (1), sliding support component (7) and frame assembly (21); Captive joint with frame assembly (21) in the top of base (2); Frame assembly (21) is arranged on the sliding support component (7), and with sliding support component (7) sliding block joint; Sliding support component (7) is arranged in the chair basin assembly (1), and with chair basin assembly (1) sliding block joint; Sit panel (13) and be fixed on chair basin assembly (1) top.
2. apparatus for adjusting position as claimed in claim 1, it is characterized in that: sliding support component (7) comprises slip steel pipe (20), frame assembly (21) comprises the sliding sleeve (24) that is enclosed within on the slip steel pipe (20), and frame assembly (21) is by slip steel pipe (20) and sliding sleeve (24) and sliding support component (7) sliding block joint.
3. apparatus for adjusting position as claimed in claim 2, it is characterized in that: chair basin assembly (1) is provided with slide rail (16), sliding support component (7) is provided with and is used for the pulley (19) that slides on slide rail (16), and sliding support component (7) is by pulley (19) and slide rail (16) and chair basin assembly (1) sliding block joint.
4. apparatus for adjusting position as claimed in claim 3 is characterized in that: slip steel pipe (20) is vertical mutually with slide rail (16).
5. apparatus for adjusting position as claimed in claim 3, it is characterized in that: the slide rail (16) on the chair basin assembly (1) is two, article two, slide rail (16) is parallel to each other, two slide rails (16) side is respectively equipped with the tooth bar (15) parallel with slide rail (16), sliding support component (7) is provided with respectively and meshes two gears (18) with two tooth bars (15), an axial connecting rod (17) captive joint that passes through of two gears (18).
6. apparatus for adjusting position as claimed in claim 1 is characterized in that: the bottom of sitting panel (13) is provided with limit guide rail (9), and the top of base (2) is provided with and is used for the location pulley that slides on limit guide rail (9).
7. apparatus for adjusting position as claimed in claim 6 is characterized in that: described location pulley is two, and two location pulleys are separately positioned on the both sides of limit guide rail (9).
8. apparatus for adjusting position as claimed in claim 6 is characterized in that: the bottom of sitting panel (13) also has horizontal location hole (8), and the top of base (2) is provided with the locating dowel pin assembly that cooperates with horizontal location hole (8).
9. apparatus for adjusting position as claimed in claim 1 is characterized in that: base (2) is tower lifting structure assembly.
10. apparatus for adjusting position as claimed in claim 9 is characterized in that: base (2) inside is provided with gas spring (22).
CN2009202896615U 2009-12-30 2009-12-30 Position regulating device of aero seat Expired - Fee Related CN201587537U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2009202896615U CN201587537U (en) 2009-12-30 2009-12-30 Position regulating device of aero seat

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2009202896615U CN201587537U (en) 2009-12-30 2009-12-30 Position regulating device of aero seat

Publications (1)

Publication Number Publication Date
CN201587537U true CN201587537U (en) 2010-09-22

Family

ID=42747302

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2009202896615U Expired - Fee Related CN201587537U (en) 2009-12-30 2009-12-30 Position regulating device of aero seat

Country Status (1)

Country Link
CN (1) CN201587537U (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103362976A (en) * 2013-07-05 2013-10-23 哈尔滨东安发动机(集团)有限公司 Automatic and manual integrated clutch
CN103359287A (en) * 2013-07-05 2013-10-23 哈尔滨东安发动机(集团)有限公司 Airplane electric seat horizontally adjusting device
CN103359286A (en) * 2013-07-05 2013-10-23 哈尔滨东安发动机(集团)有限公司 Airplane electric seat adjusting device
CN103921945A (en) * 2013-01-10 2014-07-16 塞斯纳飞行器公司 Seat Base For Aircraft

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103921945A (en) * 2013-01-10 2014-07-16 塞斯纳飞行器公司 Seat Base For Aircraft
CN103921945B (en) * 2013-01-10 2016-04-20 塞斯纳飞行器公司 For the seat base of aircraft
CN103362976A (en) * 2013-07-05 2013-10-23 哈尔滨东安发动机(集团)有限公司 Automatic and manual integrated clutch
CN103359287A (en) * 2013-07-05 2013-10-23 哈尔滨东安发动机(集团)有限公司 Airplane electric seat horizontally adjusting device
CN103359286A (en) * 2013-07-05 2013-10-23 哈尔滨东安发动机(集团)有限公司 Airplane electric seat adjusting device
CN103362976B (en) * 2013-07-05 2015-10-07 哈尔滨东安发动机(集团)有限公司 A kind of engaging and disengaging gear of auto-manual
CN103359286B (en) * 2013-07-05 2015-10-28 哈尔滨东安发动机(集团)有限公司 Aircraft adjusting device of electric seat
CN103359287B (en) * 2013-07-05 2016-06-01 哈尔滨东安发动机(集团)有限公司 The electronic seat level(l)ing device of aircraft

Similar Documents

Publication Publication Date Title
CN201587537U (en) Position regulating device of aero seat
CN105996436B (en) Multifunctional adjustable tables and chairs
CN211186451U (en) Teaching equipment for higher education
CN103863566A (en) Seating device comprising a forward-foldable backrest
CN203676622U (en) Double-motor electric lifting bed
CN203969786U (en) Hommization folding seat
CN112537329A (en) Seat capable of adjusting sitting and lying posture state in rail vehicle business area
CN214594869U (en) Desk and chair capable of correcting sitting posture
CN201668152U (en) Seat convenient for adjusting height of headrest
CN201989673U (en) Passenger grab rod in bus for standing passengers
CN105996453B (en) It stands and sits alternative expression workbench
CN217565399U (en) Seat with adjustable back of chair
CN202365352U (en) Full-gear automatic swinging bed
CN202135979U (en) Novel teacher chair
CN208510409U (en) A kind of humanized rest chair that can adjust height
CN2500184Y (en) Movable armrest of chair
CN202609000U (en) Seat height adjusting device on fitness bicycle
CN219927694U (en) Subway handrail device capable of automatically resetting
CN210783598U (en) Guardrail integrated adjustable public bench
CN108434676B (en) Folding body-building device
CN219556760U (en) Office chair with liftable chair back
CN202848815U (en) Elevator car inner wall
CN211961510U (en) Sofa with adjustable armrest
CN213598346U (en) A workstation elevation structure for cotton laminating device of bubble of touch-sensitive screen
CN114146375B (en) But height-adjusting's sports push-up apparatus

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
ASS Succession or assignment of patent right

Owner name: HUBEI HANGYU JIATAI AIRCRAFT EQUIPMENT CO., LTD.

Free format text: FORMER OWNER: AEROSPACE LIFE-SUPPORT INDUSTRIES CO., LTD.

Effective date: 20121030

C41 Transfer of patent application or patent right or utility model
COR Change of bibliographic data

Free format text: CORRECT: ADDRESS; FROM: 441003 XIANGFAN, HUBEI PROVINCE TO: 441000 XIANGFAN, HUBEI PROVINCE

TR01 Transfer of patent right

Effective date of registration: 20121030

Address after: 441000, No. 1, Catic Avenue, Fancheng District, Hubei, Xiangyang

Patentee after: AVIC HUBEI ALI-JIATAI AIRCRAFT EQUIPMENT CO., LTD.

Address before: 157 mailbox 441003, Hubei City, Xiangfan Province

Patentee before: Aerospace Life-Support Industries Co., Ltd.

CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20100922

Termination date: 20151230

EXPY Termination of patent right or utility model