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JP2004081263A - Mechanism for obtaining perfect reclining function for seat, especially airplane seat - Google Patents

Mechanism for obtaining perfect reclining function for seat, especially airplane seat Download PDF

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Publication number
JP2004081263A
JP2004081263A JP2002242955A JP2002242955A JP2004081263A JP 2004081263 A JP2004081263 A JP 2004081263A JP 2002242955 A JP2002242955 A JP 2002242955A JP 2002242955 A JP2002242955 A JP 2002242955A JP 2004081263 A JP2004081263 A JP 2004081263A
Authority
JP
Japan
Prior art keywords
seat
pivotally supported
reclining
lever
mechanism according
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
Application number
JP2002242955A
Other languages
Japanese (ja)
Inventor
Alberto Veneruso
アルベルト ヴェネルーソ
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.)
Aviointeriors SpA
Original Assignee
Aviointeriors SpA
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 Aviointeriors SpA filed Critical Aviointeriors SpA
Priority to JP2002242955A priority Critical patent/JP2004081263A/en
Publication of JP2004081263A publication Critical patent/JP2004081263A/en
Pending legal-status Critical Current

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  • Seats For Vehicles (AREA)
  • Chairs For Special Purposes, Such As Reclining Chairs (AREA)

Abstract

<P>PROBLEM TO BE SOLVED: To provide a structurally very simple and easy, and reliable mechanism for a seat, especially airplane seat, perfectly reclining the seat into a bed state in a minimum space to form a 'bed' having no discontinuous portion in a plane wherein a passenger rests, and to do away with a guide in view. <P>SOLUTION: This seat is disposed in an actually rear position, and has a guide. The seat has a lower side member 3 fixed on a floor, and a seat back portion 1 and a seat 2 respectively in a rear part and a front part. The seat has a seat member 7 wherein a rocking lever member 12 is pivotally supported in front of the lower side member 3 above a lower part of the seat member 7 itself, and a lever member 16 wherein a rear end part 17 is pivotally supported in a connection position 12 between the seat member 7 and the seat back portion 1 and wherein a front end part 18 is pivotally supported in the rocking lever 12. The seat has an operation means 14 acting upon the rocking lever member to operate the whole mechanism for reclining or lifting the seat. <P>COPYRIGHT: (C)2004,JPO

Description

【0001】
【発明の属する技術分野】
本発明は座席シート、特に航空機用座席シートの完全なリクライニングを得るための機構に関する。
【0002】
さらに詳しくは、本発明は厳しく限られた空間にて「ベッド」状態を作り出すことのできる上述形式の機構に関する。
【0003】
本発明により提供される解決策は「ビジネス」クラスの座席シートに特に公的である。
【0004】
【従来の技術】
航空機には、エコノミック・クラス用、ビジネス・クラス用、そして多くの場合にファースト・クラス用の座席シートが備えられていることはよく知られている。
【0005】
最高の快適さを得るために、特にビジネス・クラスおよびファースト・クラスに関して、多くの技術的な解決策が研究されている。ファースト・クラスに関しては利用できる空間が大きいという理由で解決方法を見い出すことは容易であるのに対し、ビジネス・クラス用の座席シートで或る程度の結果を得ることはさらに困難であるということは明かである。
【0006】
さらに詳しくは、ビジネス・クラスでは利用できる空間が小さいという主な理由により、「ベッド」状態を得ることは容易でない。
【0007】
本発明で提供される解決策は、この点に関して含まれる。
【0008】
【発明が解決しようとする課題】
特に、本発明の主目的は、最小限の空間にてベッド状態となるまで座席シートを完全にリクライニングさせる機構を提供することである。
【0009】
本発明の他の目的は、乗客が休息する平面に不連続部分のない「ベッド」とすることのできる上述形式の解決策を提供することである。
【0010】
本発明のさらに他の目的は、構造的見地から非常に簡単であり、同時に容易且つ信頼できる機構を提供することである。
【0011】
本発明のさらに他の目的は、見えてしまうガイドの存在を排除する技術的解決策を提供することである。
【0012】
【課題を解決するための手段】
従って本発明の特別な目的は、実質的にリア・ポジションに配置され、ガイドを備え、床に固定された下側部材と、背もたれ部分およびシート座がそれぞれ後部および前部に備えられると共に、前記下側部材の前方で、自体の下部上方に揺動レバー部材が枢支されているシート部材と、シート部材および背もたれ部分の間の連結箇所に後端部が枢支され、前記揺動レバーに前端部が枢支されたレバー部材とを含み、揺動レバー部材に作用して、座席シートをリクライニングまたはリフティングさせる機構全体を作動させるための作動手段をさらに備えた座席シート、特に航空機用座席シートの完全なリクライニング機能を得るための機構である。
【0013】
本発明によれば、シート・フットレストのためのリフティング機構が提供される。
【0014】
さらに本発明によれば、各シートに異なる2つの機構を備えることができる。
【0015】
さらに、本発明によれば、前記揺動レバー作動手段は機械式、液体圧作動式、空気圧作動式、液体および空気圧作動式の作動手段で構成されることができる。
【0016】
本発明による機構の好ましい実施例では、前記シート部材は後部に背もたれ部分用の2つの手段と、シート座の連結用の2つの連結箇所、すなわちそれぞれ上側箇所および下側箇所とが備えられる。
【0017】
本発明は、添付図面を特に参照して好ましい実施例に従って以下に記載されるが、この記載は説明のためのものであり、限定する目的のものではない。
【0018】
【発明の実施の形態】
添付図面を参照すれば、図1および図2には、背もたれ部分1、およびフットレスト2’を備えたシート座2、さらには本発明による機構の他の部分が示されている。
【0019】
特に前記機構は、シート座の下側バーを床に固定するための固定箇所4,5、ならびにガイド6を備えた部材3を備えており、本発明による機構に関するそれらの機能は以下の説明で明白となるであろう。
【0020】
シート座の部材7は後部の符号8,9で示される箇所で、背もたれ部分1の箇所8’,9’に対して枢支され、また部材7は箇所10,11に対応する箇所でシート座2に連結される。さらに、部材7はピン12’を備えた後部において、部材3のガイド6に沿ってスライド可能とされる。
【0021】
前部揺動レバー12は部材3の底部且つ前部に備えられ、箇所13,13’を一致させて連結されており、また液体圧作動式、空気圧作動式、液体および空気圧作動式の作動装置とされる作動装置14が揺動レバーに作用する。
【0022】
前記揺動レバー12は部材7の箇所15’に対し、対応する符号15で示される箇所にてさらに枢支される。
【0023】
連結レバー16がさらに含まれ、この連結レバーは後端が箇所9−9’の位置にて枢支され、揺動レバー12の箇所18’にて他方の全体8が枢支される。
【0024】
図3a〜図3eも参照すれば、本発明による機構の作動が見られる。
【0025】
作動装置14を作動させることで、下側部材3上で枢支箇所13のまわりに揺動レバー12が回転を生じる。
【0026】
揺動レバー12はシート座に対して前進移動し、従って枢支箇所15,15’によりシート部材7を前方へ押圧し、下側部材3のガイド6に沿う連結レバー16の動きによって前進させる。
【0027】
この機構の動きは、図3eの「ベッド」位置を得るまで続く。
【0028】
図示された実施例では、この解決策は座席シートのリクライニングを行うためにただ1つの機構を備えればすむのであるが、本発明による二重機構が各座席シートに備えられている。
【0029】
同時に、従来形式の機構に鑑みてフットレスト2’が持ち上がるが、フットレストは本発明の特別な目的でないことから、これ以上説明することはしない。
【0030】
添付図面に示された実施例では、座席シートは同日出願された別の特許出願の主題であるさらに幾つかの構造的特徴を備えており、特にリクライニング作動時に後部本体19が開かれてシート座が移動できるようにする。
【0031】
開かれたときに、肩のためにより大きな空間が得られるようにするパネル20をさらに備えている。
【0032】
望まれるならば、隣接する座席シートと連続した空間を得るために、下げることの可能なアーム21がさらに備えられている。
【0033】
本発明は好ましい実施例に従って説明のために、非制限的な目的で記載されたが、当業者には特許請求の範囲の欄に記載された関連する範囲から逸脱することなく改良および(または)変更を行い得ることを理解しなければならない。
【図面の簡単な説明】
【図1】本発明による機構の斜視図である。
【図2】本発明による機構の部材の分解図である。
【図3a】本発明による機構を備えた座席シートのある位置を示す。
【図3b】本発明による機構を備えた座席シートの別の位置を示す。
【図3c】本発明による機構を備えた座席シートのさらに別の位置を示す。
【図3d】本発明による機構を備えた座席シートのさらに移動された位置を示す。
【図3e】本発明による機構を備えた座席シートのベッドの位置を示す。
【符号の説明】
1 背もたれ部分
2 シート座
2’ フットレスト2’
3 ガイド6を備えた部材
4,5 固定箇所
6 ガイド
7 シート座の部材
8,8’,9,9’,10,11,13,13’ 枢支箇所
15,15’,18’ 枢支箇所
12’ ピン
12 揺動レバー
14 作動装置
16 連結レバー
19 後部本体
20 パネル
[0001]
TECHNICAL FIELD OF THE INVENTION
The present invention relates to a mechanism for obtaining a complete reclining of a seat, in particular an aircraft seat.
[0002]
More particularly, the invention relates to a mechanism of the above type capable of creating a "bed" condition in a tightly confined space.
[0003]
The solution provided by the present invention is particularly public for "business" class seats.
[0004]
[Prior art]
It is well known that aircraft are equipped with seats for Economic Class, Business Class, and often First Class.
[0005]
A number of technical solutions have been studied for maximum comfort, especially for the business class and the first class. While it is easy to find a solution for First Class due to the large space available, it is more difficult to get some results with Business Class seats. It is clear.
[0006]
More specifically, it is not easy to obtain a "bed" condition, mainly because the space available in business class is small.
[0007]
The solution provided by the present invention is included in this regard.
[0008]
[Problems to be solved by the invention]
In particular, it is a primary object of the present invention to provide a mechanism for fully reclining a seat until it is in a bed with a minimum of space.
[0009]
It is another object of the present invention to provide a solution of the above type which can be a "bed" without discontinuities in the plane where the passenger rests.
[0010]
Yet another object of the invention is to provide a mechanism which is very simple from a structural point of view, while at the same time being easy and reliable.
[0011]
It is yet another object of the present invention to provide a technical solution that eliminates the presence of visible guides.
[0012]
[Means for Solving the Problems]
It is therefore a special object of the present invention to provide a lower member fixed substantially to the floor, which is arranged substantially in a rear position, provided with a guide, and a backrest portion and a seat seat are provided at a rear portion and a front portion, respectively. In front of the lower member, a seat member on which a swing lever member is pivotally supported above the lower part thereof, and a rear end portion pivotally supported at a connection point between the seat member and the backrest portion, A seat member, in particular, an aircraft seat seat, further comprising an actuation means for actuating a swinging lever member to actuate the entire mechanism for reclining or lifting the seat, the lever comprising a lever member pivotally supported at the front end. This is a mechanism for obtaining a complete reclining function.
[0013]
According to the present invention, there is provided a lifting mechanism for a seat footrest.
[0014]
Furthermore, according to the present invention, each sheet can be provided with two different mechanisms.
[0015]
Further, according to the present invention, the swing lever operating means can be constituted by mechanical, liquid pressure operated, pneumatically operated, liquid and pneumatically operated operation means.
[0016]
In a preferred embodiment of the mechanism according to the invention, the seat member is provided at the rear with two means for the backrest part and two connection points for the connection of the seat, namely an upper point and a lower point, respectively.
[0017]
The present invention is described below according to preferred embodiments, with particular reference to the accompanying drawings, which are intended to be illustrative and not limiting.
[0018]
BEST MODE FOR CARRYING OUT THE INVENTION
Referring to the accompanying drawings, FIGS. 1 and 2 show a seat back 1 and a seat 2 with a footrest 2 ', as well as other parts of the mechanism according to the invention.
[0019]
In particular, said mechanism comprises fixing points 4, 5 for fixing the lower bar of the seat to the floor, and a member 3 with a guide 6, the function of which according to the invention is described in the following description. Will be obvious.
[0020]
The seat member 7 is pivotally supported at points 8 ', 9' on the backrest portion 1 at locations indicated by reference numerals 8 and 9 at the rear, and the member 7 is seated at locations corresponding to locations 10 and 11. 2 Further, the member 7 is slidable along the guide 6 of the member 3 at the rear portion provided with the pin 12 ′.
[0021]
The front rocker lever 12 is provided at the bottom and front of the member 3 and is connected in coincidence with the points 13, 13 'and is a hydraulic, pneumatic, liquid and pneumatic actuator. Actuating device 14 acts on the swing lever.
[0022]
The rocking lever 12 is further pivotally supported at a point indicated by reference numeral 15 with respect to a point 15 ′ of the member 7.
[0023]
A connecting lever 16 is further included, which is pivoted at its rear end at the point 9-9 ′ and the other whole 8 at the point 18 ′ of the rocking lever 12.
[0024]
3a to 3e, the operation of the mechanism according to the invention can be seen.
[0025]
Activating the actuating device 14 causes the pivoting lever 12 to rotate on the lower member 3 around the pivot point 13.
[0026]
The pivoting lever 12 moves forward with respect to the seat, and thus pushes the seat member 7 forward at the pivot points 15, 15 'and moves forward by the movement of the connecting lever 16 along the guide 6 of the lower member 3.
[0027]
The movement of this mechanism continues until the "bed" position of FIG. 3e is obtained.
[0028]
In the embodiment shown, this solution requires only one mechanism for reclining the seat, but a dual mechanism according to the invention is provided for each seat.
[0029]
At the same time, the footrest 2 'is lifted in view of the conventional mechanism, but will not be described further since the footrest is not a special purpose of the present invention.
[0030]
In the embodiment shown in the accompanying drawings, the seat comprises further structural features which are the subject of another patent application filed on the same date, in particular when the rear body 19 is opened and the seat seat is opened during reclining operation. To be able to move.
[0031]
It is further provided with a panel 20 which, when opened, allows more space for the shoulder.
[0032]
If desired, a lowerable arm 21 is further provided in order to obtain a continuous space with the adjacent seat.
[0033]
Although the present invention has been described by way of non-limiting example in accordance with preferred embodiments, those skilled in the art will appreciate that modifications and / or improvements may be made without departing from the scope of the claims set forth below. You must understand that changes can be made.
[Brief description of the drawings]
FIG. 1 is a perspective view of a mechanism according to the present invention.
FIG. 2 is an exploded view of the members of the mechanism according to the invention.
FIG. 3a shows a position of a seat with a mechanism according to the invention.
FIG. 3b shows another position of the seat with the mechanism according to the invention.
FIG. 3c shows yet another position of the seat with the mechanism according to the invention.
FIG. 3d shows a further displaced position of the seat with the mechanism according to the invention.
FIG. 3e shows the position of the bed of the seat with the mechanism according to the invention.
[Explanation of symbols]
1 Backrest part 2 Seat seat 2 'Footrest 2'
3 Members 4 and 5 with guides 6 Fixing points 6 Guides 7 Seat seat members 8, 8 ', 9, 9', 10, 11, 13, 13 'Pivot points 15, 15', 18 'Pivot points 12 'pin 12 rocking lever 14 operating device 16 connecting lever 19 rear body 20 panel

Claims (6)

実質的に後方位置に配置され、ガイドを備え、床に固定された下側部材と、背もたれ部分およびシート座がそれぞれ後部および前部に備えられると共に、前記下側部材の前方で、自体の下部上方に揺動レバー部材が枢支されているシート部材と、シート部材および背もたれ部分の間の連結箇所に後端部が枢支され、前記揺動レバーに前端部が枢支されたレバー部材とを含み、揺動レバー部材に作用して、座席シートをリクライニングまたはリフティングさせる機構全体を作動させるための作動手段をさらに備えたことを特徴とする座席シート、特に航空機用座席シートの完全なリクライニング機能を得るための機構。A lower member disposed substantially in a rearward position and provided with a guide and fixed to the floor, and a backrest portion and a seat seat provided at a rear portion and a front portion, respectively, and in front of the lower member, a lower portion of itself. A seat member having a swing lever member pivotally supported upward, a lever member having a rear end pivotally supported at a connection point between the seat member and the backrest portion, and a front end pivotally supported by the swing lever; A complete reclining function of a seat, especially an aircraft seat, characterized by further comprising actuating means for acting on the rocking lever member to actuate the entire mechanism for reclining or lifting the seat. Mechanism for gaining. シート・フットレストのためのリフティング機構を備えたことを特徴とする請求項1に記載された機構。The mechanism according to claim 1, further comprising a lifting mechanism for the seat footrest. 各シートに異なる2つの機構が備えられたことを特徴とする請求項1から請求項2までのいずれか一項に記載された機構。The mechanism according to any one of claims 1 to 2, wherein two different mechanisms are provided for each seat. 前記揺動レバー作動手段が機械式、液体圧作動式、空気圧作動式、液体および空気圧作動式の作動手段を含むことを特徴とする請求項1から請求項3までのいずれか一項に記載された機構。4. The method according to claim 1, wherein the swing lever actuating means includes mechanical, liquid actuated, pneumatic, liquid and pneumatic actuating means. Mechanism. 前記シート部材が後部に背もたれ部分用の2つの手段と、シート座の連結用の2つの連結箇所、すなわちそれぞれ上側箇所および下側箇所とを備えたことを特徴とする請求項1から請求項4までのいずれか一項に記載された機構。5. The seat member according to claim 1, wherein the seat member has two means for a backrest portion at a rear portion and two connection points for connecting a seat, ie, an upper portion and a lower portion, respectively. The mechanism according to any one of the preceding claims. 実質的に図示し説明した請求項1から請求項5までのいずれか一項に記載された機構。6. A mechanism substantially as shown and described in any one of the preceding claims.
JP2002242955A 2002-08-23 2002-08-23 Mechanism for obtaining perfect reclining function for seat, especially airplane seat Pending JP2004081263A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2002242955A JP2004081263A (en) 2002-08-23 2002-08-23 Mechanism for obtaining perfect reclining function for seat, especially airplane seat

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2002242955A JP2004081263A (en) 2002-08-23 2002-08-23 Mechanism for obtaining perfect reclining function for seat, especially airplane seat

Publications (1)

Publication Number Publication Date
JP2004081263A true JP2004081263A (en) 2004-03-18

Family

ID=32051842

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2002242955A Pending JP2004081263A (en) 2002-08-23 2002-08-23 Mechanism for obtaining perfect reclining function for seat, especially airplane seat

Country Status (1)

Country Link
JP (1) JP2004081263A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016031003A1 (en) * 2014-08-28 2016-03-03 株式会社ジャムコ Passenger seat for aircraft

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016031003A1 (en) * 2014-08-28 2016-03-03 株式会社ジャムコ Passenger seat for aircraft
JP5890936B1 (en) * 2014-08-28 2016-03-22 株式会社ジャムコ Aircraft passenger seat
EP3196121A4 (en) * 2014-08-28 2017-11-22 Jamco Corporation Passenger seat for aircraft
US10093423B2 (en) 2014-08-28 2018-10-09 Jamco Corporation Passenger seat for aircraft

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