序号 专利名 申请号 申请日 公开(公告)号 公开(公告)日 发明人
201 Latching device of aircraft oxygen supply module JP54088997 1997-04-29 JP3961572B2 2007-08-22 チャールズ シー オールガー
202 Compression molded containers of aircraft oxygen supply module JP54089097 1997-04-28 JP3917186B2 2007-05-23 チャールズ シー オールガー
203 Design structure of archway for aircraft, structural member pair of archway for aircraft, and aircraft JP2006123697 2006-04-27 JP2006306388A 2006-11-09 GUARD PETER S; YOUNG DAVID A
<P>PROBLEM TO BE SOLVED: To provide a design structure of an archway for an aircraft. <P>SOLUTION: The archway structure can be positioned, individually or in pairs or other sets, along the length of the interior of the aircraft, for example, such as a commercial airliner. The archway extends across the ceiling of the interior of a cabin and downwardly extends to a point adjacent a baggage bins. In order to conform an end of the archway with the internal baggage bins, an end cap is provided. According to the design structure, a unique "look and feel" and architectural configuration are provided and no seat loss takes place. <P>COPYRIGHT: (C)2007,JPO&INPIT
204 Emergency lights of an airplane having a plurality of deck JP2006501905 2004-02-19 JP2006518685A 2006-08-17 ハンス−クリスティアン・リーロフ
飛行機事故等により、煙、火災、あるいは他のパニック状態が生じた場合、できるだけ安全に乗客を出口へ案内する。 乗客、貨物、乗員のための高さ位置の異なる複数のデッキ7と、これらのデッキをつなぐ少なくとも1つの階段1、2、3と、当該階段の各ステップ2の両側に配置された光ルミネセンス物質を含むレール状またはストリップ状のマーカー4、5と、を備えた飛行機。 マーカー4は、上方側から目視可能で、かつ本質的に連続しており、上記ステップ2の側方において、上記階段1、2、3の上り勾配に沿って配置される。
205 Cabin module for aircraft JP2004522241 2003-07-15 JP2005532952A 2005-11-04 サン−ジヤルム,ブリユノ
本発明は、2つの小壁によって連結される2つの大壁12と、モジュール10を通路8から分離する1つの壁に沿って配置されるサービスモジュール14と、1つの小壁に設けられる開口部に取り付けられたドア16と、航空機の移動方向に対して長手方向に方向付けられる少なくとも1つの構造体を有する少なくとも1つの座席18とを備える、長い矩形形状の航空機キャビンモジュールに関する。 各モジュールは、少なくとも1人の乗客のベッド面を構成するように作られた要素24、28を備える。
206 Air chiller device JP2004129760 2004-04-26 JP2005308369A 2005-11-04 OZAKI MASAJI; MAEDA SHUJI
PROBLEM TO BE SOLVED: To improve an air chiller device capable of sending cooled air to service carts loaded in an airplane for serving. SOLUTION: This air chiller device 1 has a refrigeration cycle unit loaded on a casing 10. The refrigeration cycle unit comprises a refrigerant compressor 20, a condenser 30 and an evaporator 40, and the cooled air is sent to a galley or the like by a blower device 60. The casing 10 is composed of a honeycomb panel. The compressor device 20 is supported on a base plate of the casing 10 by a pair of vibrationproof mounting devices 26. The vibration-proof mounting devices 26 respectively have a triangular prism-shaped bracket and a A-shaped vibrationproof rubber, vibration-proof function in normal times, and the vibrationproof rubber is compressed to hold the compressor device 20 with high spring constant under high load. COPYRIGHT: (C)2006,JPO&NCIPI
207 Arrangement structure of seat for aircraft cabin JP2005053681 2005-02-28 JP2005239153A 2005-09-08 MERCIER GUY
<P>PROBLEM TO BE SOLVED: To provide arrangement structure of individual seat for a passenger of an aircraft equipped with a plurality of seats which can be converted to a bed and disposed in a row. <P>SOLUTION: The two lateral groups (3a, 13a) of two contiguous rows, each group is disposed along a wall (4) of the aircraft fuselage. At least one central group (3b, 13b) of the two contiguous rows, and the central group is separated from each of the lateral groups by a gangway; each lateral group is provided with a pitch (P1) capable of allowing the traverse passage for the passengers of the other rows between two consecutive seats in a first row. At least one central group is provided with a smaller pitch (P2) than the pitch provided in the lateral groups on the two consecutive seats in the same row. <P>COPYRIGHT: (C)2005,JPO&NCIPI
208 Method and apparatus for delivering oxygen-enriched air to the passenger airplane JP2002579309 2002-02-01 JP2004523327A 2004-08-05 カゼナベ、ジャン−ミシェル; ザパタ、リシャール; ドゥアイェ、ジャン; バンドルー、オリビエ
本発明によれば、乗客は、飛行機が通常の巡航高度から中間の代替高度まで下降する下降期間中に、独立した供給手段、特に高圧のシリンダー(16)から酸素富化空気の第1の部分の供給を受ける。 さらに、圧縮空気を飛行機自体の圧縮空気源から取り出し、前記酸素富化空気の第2の部分を生成し(2において)、この酸素を、5500メートルを超える代替高度に近い高度で、少なくとも飛行機の安定飛行期間中、乗客へ配送する。
【選択図】図1
209 Respiration mask storage box JP2001246263 2001-08-14 JP2002119605A 2002-04-23 MARTINEZ PATRICE
PROBLEM TO BE SOLVED: To provide an oxygen mask storage box which can facilitate the storage of a mask without obstructing the releasing of the mask. SOLUTION: This oxygen mask storage box is equipped with a housing 10 and a door 12. In this case, the housing 10 includes a network in order to distribute oxygen which is fed from general piping or a chemical oxygen generating device. The door 12 is arranged under the storage box at a specified location. Then, on the internal surface of the door or the internal surface of the housing, at least one receiving base means 20, and at least one latch 24 are provided. The receiving base means 20 determines respective holding locations of the oxygen masks 16. The latch 24 can move from a location to constitute a mask holding socket to a location to release the mask 16 by corresponding with the closing of the door 12. COPYRIGHT: (C)2002,JPO
210 Respirator storing box for emergency equipment JP2001247407 2001-08-16 JP2002114198A 2002-04-16 MARTINEZ PATRICE
PROBLEM TO BE SOLVED: To easily open a part of a door in the inspection work with respect to a storage box for storing an oxygen mask for passenger of an airplane. SOLUTION: This oxygen mask storing box comprises a housing 10 closed by the door 12, and a piping accommodated in the housing for supplying a breathing gas through a soft tube by the first pressure. In an ordinary condition, the door 12 is held on a close position by hooks 14, 16. The hooks can be unhooked in need of touch with the mask. The opening of the door is limited to a partially opened state by transmitting an electric signal, or changing the pressure in the piping to the second pressure to prevent the dropping of the mask in unhooking. COPYRIGHT: (C)2002,JPO
211 Passenger guide device for cabin of airplane JP2001065445 2001-03-08 JP2001301698A 2001-10-31 ROMCA JENS; MUELLER JOCHEN; SCHUMACHER MARKUS
PROBLEM TO BE SOLVED: To form a passenger guide device for a cabin of an airplane so as to improve the economical efficiency of the airplane by realizing the quick boarding and while shortening the time of the airplane waiting on the ground. SOLUTION: A passenger guide device for cabin is provided with a display element, and this display element displays the line of seats and the number of seats of the seat structure inside the airplane. Each seat 15 of the airplane is provided with display elements 16 and 21, and these display elements are formed corresponding to the line of the seats and the position of the line of the seat, and arranged at a part easy to be seen by a passenger. The display element 16 for numbering the seat line is provided in an aisle side passenger seat 15 in a side surface of a backrest of the seat close to the aisle.
212 Seat unit JP32484295 1995-12-13 JPH08258796A 1996-10-08 DRYBURGH IAN; LUNN SIMON; MULCHANSINGH RUSSELL
PROBLEM TO BE SOLVED: To provide a seat unit used in a cabin of an aircraft, capable of ensuring the privacy of each passenger by comprising a housing for accomodating a seat having a recling backrest, and arranging the backrests reclinably in a state that the backrest is remained in the housing. SOLUTION: This seat unit 1 comprises a reclining seat 2 and a fixed seat 3, an unit 4 is installed adjacent to the unit 1, and the units 1, 4 are separated from one another by means of a partition wall 7. The partition wall 7 comprises a screen 8 located between the seats 2, 5 in the units 1, 4 and a screen 9 located between the seats 3, 6, and a screen 10 is extended at the back of the seats 3, 6. The seat 2 comprises a fixed housing 41 for accomodating the backrest part 42, a seat part 43 and a leg rest 44, and the backrest part 42 is remained in the housing 41 at all times, so that it does not interfere the accomodation space for a passenger behind.
213 Apparatus for draining waste water from aircraft JP5281695 1995-03-13 JPH0834399A 1996-02-06 HERUGE FURANKU
PURPOSE: To prevent freezing of a drain pipe by arranging the range of a drain pipe passing through an attachment flange and the range of a drain pipe passing through a fairing in the fairing from below an aircraft, and heating them with the hot air flowing out from a discharge port in the range of a drain pipe outlet end. CONSTITUTION: A drain apparatus 1 of the waste water discharged from a toilet wash tank is attached to the fuselage belly of an aircraft by an attachment flange 6. The drain pipe 3 of the drain apparatus 1 is enclosed by an aerodynamically shaped fairing 7, and a heating element 8 is provided on the whole inner face. The heating element 8 operated electrically, e.g. a film resistor heating element, is preferably used, and a temperature sensor 9 is provided for temperature control. The air taken into the fairing 7 from below the aircraft is heated by the heating element 8 to heat the drain pipe 3, and the hot air is discharged to the outside of the fairing 7 from the range of a drain pipe outlet end 5 after heating the drain pipe 3.
214 Hinge used for rotatable section-forming bar JP32415592 1992-12-03 JPH05248135A 1993-09-24 BUORUFUGANGU MARUKUBUARUTO; ROODERITSUHI TOOMECHIEKU; BUORUFUGANGU RITSUTONAA; ARUFUREETO ROOTAA; HORUGAA BUORUNIKU; KURISUTOFU BAUAA; KURISUTEIAN SHIYUNOORU
PURPOSE: To facilitate a hinge-connection of a section-forming bar to a container and realize a stopper for a container door in a hinge used for a rotatable section-forming bar. CONSTITUTION: A first hinge part is constituted of beads 11 integrally formed at every section in the long side of a section-forming bar 9. Slits 12 are formed at sections where beads 11 are not formed. A second hinge part is constituted of tongue pieces integrally formed at the front edge and/or the rear edge of the container correspondingly to the contour of the beads 11. The tongue piece is engaged with the inside 13 of the slit 12 and the tongue piece end 15 of the tongue piece of the container rear edge is erected so as to form a stopper restricting the rotating stroke of the container door.
215 Case door for oxygen supplying unit JP32309492 1992-12-02 JPH05212132A 1993-08-24 KURISUTEIAN SHIYUNOORU; ROODERITSUHI TOMECHIEKU; BUORUFUGANGU RITSUTONAA
PURPOSE: To improve a case door for oxygen supplying unit so as to have a high torsional rigidity with a small weight as much as possible. CONSTITUTION: In a case door 2 for closing the case of an oxygen supplying unit which is rotatable around a hinge 3, the case door has a reinforcing member 8 having a form extended at least partially along a door edge part 7 and a web 9 for connecting the door edge part. The reinforcing member and the web have fixing means to the case door and/or case edge part.
216 JPH02504250A - JP50671788 1988-07-21 JPH02504250A 1990-12-06
217 Fire fighting system capable of being accommodated in passenger region JP20748482 1982-11-26 JPS58116368A 1983-07-11 UIRUHERUMU OOGASUTO BURUENSHIT
218 Apparatus for removing combustible substance from inside airplane JP20748382 1982-11-26 JPS58116367A 1983-07-11 UIRUHERUMU OOGASUTO BURUENSHIT
219 JPS49132798A - JP11938173 1973-10-22 JPS49132798A 1974-12-19
220 シート照明システム JP2017544746 2015-02-23 JP6426297B2 2018-11-21 パオロ・ディ・トラーパニ; ダヴィデ・マガッティ
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