WO1988001967A1 - Pivoting seat, in particular for a crew member of an aircraft - Google Patents
Pivoting seat, in particular for a crew member of an aircraft Download PDFInfo
- Publication number
- WO1988001967A1 WO1988001967A1 PCT/DE1987/000424 DE8700424W WO8801967A1 WO 1988001967 A1 WO1988001967 A1 WO 1988001967A1 DE 8700424 W DE8700424 W DE 8700424W WO 8801967 A1 WO8801967 A1 WO 8801967A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- seat
- ribs
- plate
- shows
- milled
- Prior art date
Links
- 238000003801 milling Methods 0.000 description 12
- 238000010276 construction Methods 0.000 description 6
- 238000004519 manufacturing process Methods 0.000 description 6
- 239000002184 metal Substances 0.000 description 5
- 238000000034 method Methods 0.000 description 4
- 238000005266 casting Methods 0.000 description 3
- 238000011161 development Methods 0.000 description 2
- 230000018109 developmental process Effects 0.000 description 2
- 238000004512 die casting Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 229910001092 metal group alloy Inorganic materials 0.000 description 2
- 230000002411 adverse Effects 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000000969 carrier Substances 0.000 description 1
- 238000005253 cladding Methods 0.000 description 1
- 230000002860 competitive effect Effects 0.000 description 1
- 239000006260 foam Substances 0.000 description 1
- 230000012447 hatching Effects 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 238000005495 investment casting Methods 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 230000007257 malfunction Effects 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
- B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
- B60N2/24—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles for particular purposes or particular vehicles
- B60N2/30—Non-dismountable or dismountable seats storable in a non-use position, e.g. foldable spare seats
- B60N2/3038—Cushion movements
- B60N2/304—Cushion movements by rotation only
- B60N2/3045—Cushion movements by rotation only about transversal axis
- B60N2/3047—Cushion movements by rotation only about transversal axis the cushion being hinged at the back-rest
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B09—DISPOSAL OF SOLID WASTE; RECLAMATION OF CONTAMINATED SOIL
- B09B—DISPOSAL OF SOLID WASTE NOT OTHERWISE PROVIDED FOR
- B09B1/00—Dumping solid waste
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
- B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
- B60N2/24—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles for particular purposes or particular vehicles
- B60N2/30—Non-dismountable or dismountable seats storable in a non-use position, e.g. foldable spare seats
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
- B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
- B60N2/24—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles for particular purposes or particular vehicles
- B60N2/30—Non-dismountable or dismountable seats storable in a non-use position, e.g. foldable spare seats
- B60N2/3002—Non-dismountable or dismountable seats storable in a non-use position, e.g. foldable spare seats back-rest movements
- B60N2/3004—Non-dismountable or dismountable seats storable in a non-use position, e.g. foldable spare seats back-rest movements by rotation only
- B60N2/3018—Non-dismountable or dismountable seats storable in a non-use position, e.g. foldable spare seats back-rest movements by rotation only about vertical axis
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
- B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
- B60N2/24—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles for particular purposes or particular vehicles
- B60N2/30—Non-dismountable or dismountable seats storable in a non-use position, e.g. foldable spare seats
- B60N2/3038—Cushion movements
- B60N2/304—Cushion movements by rotation only
- B60N2/3043—Cushion movements by rotation only about longitudinal axis
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
- B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
- B60N2/24—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles for particular purposes or particular vehicles
- B60N2/30—Non-dismountable or dismountable seats storable in a non-use position, e.g. foldable spare seats
- B60N2/3038—Cushion movements
- B60N2/304—Cushion movements by rotation only
- B60N2/3045—Cushion movements by rotation only about transversal axis
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/0691—Arrangements of seats, or adaptations or details specially adapted for aircraft seats specially adapted for cabin crew
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
- B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
- B60N2/02—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable
- B60N2002/0204—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable characterised by the seat or seat part turning about or moving along a non-standard, particular axis, i.e. an axis different from the axis characterising the conventional movement
- B60N2002/022—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable characterised by the seat or seat part turning about or moving along a non-standard, particular axis, i.e. an axis different from the axis characterising the conventional movement the seat or seat part turning about or moving along a vertical axis
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Definitions
- the invention relates to a seat according to the preamble of claim 1.
- Previous seats of this type have an inner frame for receiving the loads acting on the seat and an outer cladding for appropriate shaping of the seat. It is known to manufacture the load-bearing structure, for example, as a welded structure formed from light metal pipes or profiles or as a cast part from a corresponding light metal alloy.
- the object of the invention is to design a generic seat in such a way that it can be manufactured at lower cost and less weight and has a lower risk of accident.
- the proposed seat can be produced at lower costs compared to previous seats and is of lower weight.
- the seat part automatically folds into the vertical position, which activates a spring that swivels the seat into the recess. The locking in the swiveled position takes place automatically.
- the proposed seat has the further advantage that malfunctions, such as in seats with manual swivel-in, cannot occur.
- the invention is illustrated with reference to the drawing and explained in more detail in the example description. Show it
- Figure 1 shows a seat 1, consisting of a seat part 2, a backrest 3, a headrest 4 and a belt system consisting of two shoulder straps 5, a two-part lap belt 6 with a central lock 7, which also receives the ends of the shoulder straps 5.
- the seat part 2 is mounted within the side rails so as to be foldable about an approximately horizontal axis 9.
- the backrest 3 with the seat part 2 is in turn designed to be pivotable about an approximately vertical axis 8.
- two articulated connections are provided, the upper one of which is visible in the picture.
- This upper joint consists of a fitting 11 connected to the aircraft structure and a fitting 12 on the seat side.
- the seat 1 In its ready-to-use position shown, the seat 1 is connected to the aircraft structure in three points, namely in the aforementioned joints and in a support point which is located under the position shown in FIG the right corner of the seat part 2 is located.
- the seat part 2 is detachably connected to the aircraft structure 1 'by a locking lock 13 which can be actuated by means of a lever 14. If the seat 1 is not required, it can be pivoted into a recess 15 by rotation about the axis 8. For this purpose, the locking is first released using the lever 14, so that the seat part 2 is folded into the vertical stowed position by spring force. Then the entire seat 1 is pivoted into the recess 15. If the seat 1 is fully swiveled in, a further lock automatically engages, as a result of which the seat 1 is fixed in its stowed position.
- Figure 2 shows the seat 1 in the pivoted position, the back of the backrest 3 with the cover 33 and the trough 15 are visible.
- the picture further shows the axis 8 with the upper joint, consisting of the fittings 11 and 12, and the lower joint, consisting of the fittings 16 and 17.
- the figure further shows an articulated on the backrest 3 at a point 20 at one end Stop loop 18, the other end of which has an elongated hole of length x.
- a bolt 21 is arranged which engages in the elongated hole and thus serves to guide the loop 18.
- the swivel angle of the seat 1 is defined by the length x of the elongated hole.
- a conical pin 22, which is used to fix the seat 1 in both positions, is also arranged on the structure 1 '.
- the taper pin 22 interacts with a locking lever 22a.
- the lever 22a is pressed upward, whereby the lock is released and the seat 1 can be pivoted out of the recess 15.
- Figure 3 shows the view A of Figure 1 without the surrounding structure 1 'with the backrest 3, the folded-out seat part 2, the headrest 4, the side rails 10 and 10'. the two shoulder straps 5 and the fittings 12 and 17.
- the dashed line shows the course of the invisible parts of the shoulder straps 5, each of which is connected to an automatic belt retractor 23.
- a leg spring 74 is provided, the leg 75 of which is supported against the fitting 77 and the leg 78 of which rests on the structure 1 '.
- the spring 74 is guided through the bearing pin 78.
- FIG. 4 shows the view B according to FIG. 1, in which essentially the top view of the seat part 2 with the side rails 10, 10 ′, the headrest 4 and the fitting 12 appears.
- an extension 24 is integrated, which serves to receive the locking lock 13 with the lever 14.
- FIG. 5 shows the section VV of Figure 3 with the seat part 2, the backrest 3 and the headrest 4.
- the seat part 2 consists essentially of a seat plate 25 and a seat cushion 26.
- the backrest 3 and the headrest 4 are summarized by a common support plate 27 to form an assembly, the back pad 28 and the head pad 29.
- the cushions 26, 28, 29 mentioned are made of a suitable foam.
- the locking lock 3 with the lever 14 is attached to the seat plate 25.
- the plates 25 and 27 are designed as milled parts consisting of a suitable light metal alloy.
- the side rails 10, 10 ' are also designed in the same advantageous manner.
- a belt shell 27a is designed as a sheet metal part and is screwed to both the lower edge of the back plate 27 and the side rails 10.
- Figure 6 shows in section the attachment of the fitting 12 to the backrest 3.
- four screws 30 are provided, of which the two upper ones are visible.
- the screws 30 are guided through corresponding through bores in the side rail 10 ′ and are screwed to the back plate 27 and to a fitting 32, which have corresponding internal threads 31.
- the figure also shows the back cushion 28 and a cover 33.
- FIG. 7 shows the mounting of the locking lever 22a, consisting of a pin 34 inserted into the side rail 10 ', which is supported by means of a fitting 35 screwed to the belt shell 27a.
- FIG. 8 shows, on the basis of a section, details of the mounting of the seat part 2 about the axis 9 with a pin 36 which rests in the wall 25a and a rib 25b on the part of the seat plate 25 and is inserted into the corresponding bore 10 in the rare bar 10.
- a corresponding arrangement is provided on the opposite side of the plate 25.
- the moment when the seat part 2 is folded up is applied by two leg springs 37, one of which is shown here.
- One leg of the spring 37 engages on a rib of the plat, which is not visible here te 25, whereas the other leg rests against a stop (not visible here) located on the belt shell 27a.
- the pin 36 is secured after its assembly by a split pin inserted into a bore 38.
- FIG. 9 shows in section a detail of the back plate 27 having the cushion 28 with one of the two automatic belt retractors 23 for a shoulder belt 5.
- the automatic machine 23 is fastened to the plate 27 by screws 39.
- the relevant point of the plate 27 is reinforced to accommodate the belt forces that may occur.
- FIG. 10 shows the locking lock 13 cooperating with the taper pin 22, which essentially consists of the said locking lever 14, a housing 40 and a leg spring 41, which exerts on the lever 14 a torque which rotates to the left about the pivot point 42 in the picture.
- the lock 13 is shown together with the taper pin 22. At the point of contact with the lever 14, this has a slot the thickness of the lever 14 in such a way that about half of the cross-section shown by hatching remains from the pin 14.
- the seat part 2 can simply be folded down. The lever 14 rests on the conical surface of the taper pin 22 and slides along it until the lever 14 engages in said slot. Now the seat part 2 is firmly connected to the structure 1 'and can only be released again in that the lever 14 is pivoted out of the slot by hand.
- Figure 11 shows the attachment of the stop loop 18 on the side rails 10 '.
- a bolt 43 with a washer 44 is provided, which is secured with a split pin 45.
- Figure 12 shows the locking lever 22a in a side view with the fulcrum 46.
- the lever 22a protrudes through an opening in a recess.
- a leg spring 47 gives the lever 22a, which has an arcuate region 49, a torque which rotates to the right in the figure, as a result of which it bears against a stop 48.
- the lever 22a has a conical bore 50 at its lowest point.
- the lever 22a When the seat 1 is pivoted in, the lever 22a approaches the taper pin 22 and touches it with its arcuate part, the lever 22a then evading upwards until the point of the taper bore 50 has reached the pin 22. In this position, the lever 22a jumps down again, whereby the pin 22 enters the tapered bore. The seat 1 is thus fixed in its pivoted-in position.
- FIG. 13 shows the support plate 27 designed as a milled part in view XIII according to FIG. 5.
- the production of high-strength lightweight components by milling is common in the aerospace industry, the advantage being taken that the parts in question can be optimally adapted to the existing loads.
- conventional components of this type always have an open or closed milling skin that is stiffened in a suitable manner by ribs.
- a milling construction as a further development of a sheet metal construction, the individual elements of the component, such as the skin and the ribs, being made of sheet metal and connected to one another by riveting.
- the milling construction is now advantageous compared to the sheet metal construction in that rivet overlaps and the point-like force transmissions in the area of the individual rivets are eliminated.
- milled parts are also called integral components, integral parts or integral plates.
- a finished milled part of this type only contains around 10% of the originally available material and was previously considered to be quite expensive compared to parts produced in another way due to the required mechanical outlay. It is only since a larger number of identical milled parts can be produced simultaneously in a numerically controlled milling process that milling is competitive in terms of manufacturing costs with casting or die casting.
- the support plate 27 shown consists of a milling skin 51 with stiffening ribs 52.
- the ribs 52 'diagonally crossed for the backrest in the lower region 63 have upper straps 53 according to the invention.
- the ribs 52 'standing on the skin 51 have a T-shaped cross section.
- Another top flange, designated 57, is integrated on one side of the rib in question, so that the cross section of this rib has an inverted L-shape.
- the integrated head part of the seat is later formed by the upper region 64 of the integral plate 27.
- Guide elements 58 and a belt deflection 59 are integrated here.
- the elements 58 are used in the arrangement of automatic belt retractors, whereas the deflection 59 is provided for permanently mounted shoulder belts, the fixed ends of which are held by an integrated bracket 65.
- Threaded insert holes 56 are provided as a precaution for fastening the automatic belt retractors and for fastening carriers. Due to holes 60, the plate 27 can be screwed to the side rails 10, 10 '.
- the threaded bores 61 and the through bores 62 serve to fasten the belt shell.
- Recesses 54 and bores 55 are provided to lighten the weight. 5 shows, the plate 27 is installed such that the milling skin 51 faces the upholstery.
- the rear end of the plate 27 is formed by the straps 53 and 57 of the ribs 52 and 52 '.
- An essential feature of this plate is that, apart from the stiffening ribs, all of these are still required Has elements or precautions for mounting the plate itself and for mounting all other components related to the plate.
- FIG. 14 shows a section through a rib 52 ′ according to FIG. 13.
- the T-shaped cross section of this rib appears, which results from the integration of the belt 53.
- the milled part qasi forms a double-T beam with the milling skin 51 as the lower belt, the rib 52 'as the web and the upper belt 53.
- FIG. 15 shows the milled seat plate 25.
- the ribs 52 are provided with belts 53 and thus have a T-shaped cross section.
- the milling skin 51 and the corner nodes have bores 55 to lighten the weight.
- the plate 25 is delimited by the load-bearing sides 66, 67, 68 and 71 and is provided with axle bores 70, the skin 69 serving to cover the axle spring.
- the threaded bores 72 and the pin bores 73 on the extension 24 are provided for fastening the locking lock 13, the extension 24 being integrated with the plate 25 in the manner described above.
- FIG. 16 shows the view XVI according to FIG. 14. This shows the thickness d of the plate 25 and the position of the bores 70 and the skin 69.
- the possibilities of the milling process are used here to remove all elements such as skin, ribs, edge supports, as well as all elements required for assembly, such as threaded holes, through holes, ridges, etc. insert in one piece into the relevant components.
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Environmental & Geological Engineering (AREA)
- Seats For Vehicles (AREA)
- Body Structure For Vehicles (AREA)
Description
Claims
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8810304A GB2207345B (en) | 1986-09-19 | 1987-09-19 | A swivelling seat for an aircraft |
DE3790556A DE3790556C1 (de) | 1986-09-19 | 1987-09-19 | Schwenkbarer Sitz für ein Flugzeug |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEP3631726.8 | 1986-09-19 | ||
DE19863631726 DE3631726A1 (de) | 1986-09-19 | 1986-09-19 | Schwenkbarer begleitersitz in integralbauweise fuer einen begleiter, insbesondere in einem luftfahrzeug |
DEP3632288.1 | 1986-09-23 | ||
DE19863632288 DE3632288A1 (de) | 1986-09-19 | 1986-09-23 | Verfahren zum fraesen eines integralbauteils und bauteil |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1988001967A1 true WO1988001967A1 (en) | 1988-03-24 |
Family
ID=25847589
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/DE1987/000424 WO1988001967A1 (en) | 1986-09-19 | 1987-09-19 | Pivoting seat, in particular for a crew member of an aircraft |
Country Status (6)
Country | Link |
---|---|
US (1) | US4993666A (de) |
EP (1) | EP0282541B1 (de) |
CH (1) | CH671000A5 (de) |
DE (4) | DE3631726A1 (de) |
GB (1) | GB2207345B (de) |
WO (1) | WO1988001967A1 (de) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0636511A1 (de) * | 1993-07-26 | 1995-02-01 | Georg Rechter | Klappsitz |
FR2724139A1 (fr) * | 1994-09-06 | 1996-03-08 | Renault | Siege escamotable pour vehicules |
WO1998042532A1 (en) * | 1997-03-25 | 1998-10-01 | Lear Corporation | Storable and removable seat assembly |
WO2000064699A1 (de) * | 1999-04-21 | 2000-11-02 | Kueper Wolfgang | Klappsitz |
EP1777100A1 (de) | 2005-10-19 | 2007-04-25 | Apener Maschinenbau und Förderanlagen Gustav Bruns GmbH & Co. KG | Lehnenanordnung |
EP1634765A3 (de) * | 2004-09-10 | 2007-05-09 | Euromotive GmbH & Co. KG | Rücklehne für einen Sitz, insbesondere einen Rücksitz eines Kraftfahrzeuges |
FR2980773A1 (fr) * | 2011-09-30 | 2013-04-05 | Airbus Operations Sas | Strapontin pour cockpit d'aeronef et partie avant d'aeronef equipee d'un tel strapontin |
EP2484589A3 (de) * | 2011-02-04 | 2015-05-27 | AMI Industries, Inc | Selbstverstauender Klappsitz für ein Flugzeug |
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---|---|---|---|---|
DE4125959C1 (de) * | 1991-08-06 | 1992-10-15 | Deutsche Airbus Gmbh, 2000 Hamburg, De | |
US5489141A (en) * | 1993-07-20 | 1996-02-06 | The C. E. White Co. | Pivotable and slidable storable seat |
US5385384A (en) * | 1993-08-06 | 1995-01-31 | Douglas & Lomason Co | Child safety seat |
CA2129266C (en) * | 1993-09-22 | 1999-09-21 | Karl E. Gierman | Integral child seat and seat frame combination |
US5498062A (en) * | 1993-10-18 | 1996-03-12 | Douglas & Lomason Company | Child restraint seat |
US5588700A (en) * | 1994-02-28 | 1996-12-31 | Douglas & Lomason Company | Child safety seat with side bolsters |
GB2316607A (en) * | 1996-08-29 | 1998-03-04 | Johnson Controls Automotive Uk | Folding seats for motor vehicles |
US5797649A (en) * | 1996-12-02 | 1998-08-25 | Case Corporation | Folding auxiliary seat for a vehicle |
FR2761309B1 (fr) * | 1997-03-28 | 1999-06-11 | Peugeot | Siege d'appoint pour vehicule automobile |
US6460922B1 (en) * | 1997-10-02 | 2002-10-08 | Robert L. Demick | Flexible seat system |
US6012771A (en) * | 1998-08-06 | 2000-01-11 | Chrysler Corporation | Seat fold mechanism |
US6231103B1 (en) * | 1999-03-15 | 2001-05-15 | General Motors Corporation | Seat for motor vehicle |
NL1012772C2 (nl) * | 1999-08-03 | 2001-02-06 | Pe We Venlo Auto Interieur B V | Voor de inbouw in een voertuig bestemde opklapbare stoel. |
DE19937231C2 (de) * | 1999-08-06 | 2001-07-12 | Lufthansa Technik Ag | Flugzeug-Kindersitz |
DE10007995C2 (de) * | 2000-02-22 | 2002-03-07 | Airbus Gmbh | Strukturbauteil, insbesondere für ein Flugzeug und Verfahren zur Herstellung eines Strukturbauteils |
DE10008259B4 (de) * | 2000-02-23 | 2005-03-10 | Deutsche Lufthansa | Flugzeugpassagierkabine mit mindestens einer Passagierstützvorrichtung |
US7922635B2 (en) * | 2000-03-10 | 2011-04-12 | Nautilus, Inc. | Adjustable-load unitary multi-position bench exercise unit |
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EP1225088A1 (de) * | 2001-01-18 | 2002-07-24 | Pewe Enschede Holding B.V. | Zum Einbau in ein Fahrzeug bestimmter, hochklappbarer Stuhl |
US7070545B2 (en) * | 2002-07-01 | 2006-07-04 | Nautilus, Inc. | Leg press and abdominal crunch exercise machine |
US7115080B2 (en) * | 2002-08-01 | 2006-10-03 | Nautilus, Inc. | Collapsible seat for combination hack squat and leg press machine |
CA2454590C (en) * | 2003-01-06 | 2007-07-03 | Faurecia Automotive Seating Canada Limited | Stowable rear seat for vehicle passenger compartments |
GB2399281B (en) * | 2003-03-08 | 2006-10-11 | Phoenix Seating Ltd | Seat and a vehicle including a seat |
DE10314039A1 (de) * | 2003-03-28 | 2004-10-07 | Airbus Deutschland Gmbh | Spantbauteil für ein Flugzeug |
US7490906B2 (en) * | 2004-05-27 | 2009-02-17 | Airbus Deutschland Gmbh | Seat backrest for the crew rest compartment of an aircraft |
US7201349B2 (en) * | 2004-09-09 | 2007-04-10 | Airbus | Medical unit in an aircraft |
DE102005020224A1 (de) * | 2005-04-30 | 2006-11-02 | Vogelsitze Gmbh | Fahrgastsitz für Personenbeförderungsfahrzeuge |
US7517008B2 (en) * | 2006-02-07 | 2009-04-14 | Toyota Motor Engineering & Manufacturing North America, Inc. | Remote release seat cushion lock with one hand operation |
DE102007015550B4 (de) * | 2007-03-30 | 2012-03-08 | Airbus Operations Gmbh | Treppenhaus für ein Luftfahrzeug mit klappbarer Leiter |
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US8109554B2 (en) * | 2010-02-24 | 2012-02-07 | Hedemora Anpassning Ab | Method and apparatus for supporting a wheelchair in a vehicle |
US9592753B2 (en) * | 2010-12-27 | 2017-03-14 | Agco Corporation | Seat latching and storage mechanism |
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DE102011109627B4 (de) * | 2011-08-05 | 2020-09-17 | Adient Engineering and IP GmbH | Fahrzeugsitz |
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US4460215A (en) * | 1981-09-30 | 1984-07-17 | The Boeing Company | Folding seat assembly |
EP0170116A1 (de) * | 1984-07-12 | 1986-02-05 | Robert A. Nordskog | Klappsitz |
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GB2312593A (en) * | 1996-04-26 | 1997-10-29 | Ibm | Voice mail with remote voice processing |
-
1986
- 1986-09-19 DE DE19863631726 patent/DE3631726A1/de not_active Withdrawn
- 1986-09-23 DE DE19863632288 patent/DE3632288A1/de not_active Withdrawn
-
1987
- 1987-09-19 CH CH1971/88A patent/CH671000A5/de not_active IP Right Cessation
- 1987-09-19 DE DE3790556A patent/DE3790556C1/de not_active Expired - Fee Related
- 1987-09-19 WO PCT/DE1987/000424 patent/WO1988001967A1/de active IP Right Grant
- 1987-09-19 GB GB8810304A patent/GB2207345B/en not_active Expired - Lifetime
- 1987-09-19 EP EP87906071A patent/EP0282541B1/de not_active Expired - Lifetime
- 1987-09-19 DE DE19873790556 patent/DE3790556D2/de not_active Expired
- 1987-09-19 US US07/214,722 patent/US4993666A/en not_active Expired - Fee Related
Patent Citations (3)
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FR804010A (fr) * | 1935-07-05 | 1936-10-14 | Salvaor | Disposition de siège avant pour véhicules automobiles ou autres |
US4460215A (en) * | 1981-09-30 | 1984-07-17 | The Boeing Company | Folding seat assembly |
EP0170116A1 (de) * | 1984-07-12 | 1986-02-05 | Robert A. Nordskog | Klappsitz |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0636511A1 (de) * | 1993-07-26 | 1995-02-01 | Georg Rechter | Klappsitz |
FR2724139A1 (fr) * | 1994-09-06 | 1996-03-08 | Renault | Siege escamotable pour vehicules |
EP0704340A1 (de) * | 1994-09-06 | 1996-04-03 | Société Anonyme dite: REGIE NATIONALE DES USINES RENAULT | Klappsitz für Fahrzeuge |
WO1998042532A1 (en) * | 1997-03-25 | 1998-10-01 | Lear Corporation | Storable and removable seat assembly |
WO2000064699A1 (de) * | 1999-04-21 | 2000-11-02 | Kueper Wolfgang | Klappsitz |
EP1634765A3 (de) * | 2004-09-10 | 2007-05-09 | Euromotive GmbH & Co. KG | Rücklehne für einen Sitz, insbesondere einen Rücksitz eines Kraftfahrzeuges |
EP1777100A1 (de) | 2005-10-19 | 2007-04-25 | Apener Maschinenbau und Förderanlagen Gustav Bruns GmbH & Co. KG | Lehnenanordnung |
EP2484589A3 (de) * | 2011-02-04 | 2015-05-27 | AMI Industries, Inc | Selbstverstauender Klappsitz für ein Flugzeug |
FR2980773A1 (fr) * | 2011-09-30 | 2013-04-05 | Airbus Operations Sas | Strapontin pour cockpit d'aeronef et partie avant d'aeronef equipee d'un tel strapontin |
US9340293B2 (en) | 2011-09-30 | 2016-05-17 | Airbus Operations (S.A.S.) | Aircraft flight deck comprising a folding seat |
Also Published As
Publication number | Publication date |
---|---|
GB2207345B (en) | 1990-11-14 |
DE3790556D2 (de) | 1988-10-27 |
DE3632288A1 (de) | 1988-04-07 |
CH671000A5 (de) | 1989-07-31 |
EP0282541A1 (de) | 1988-09-21 |
EP0282541B1 (de) | 1991-08-14 |
US4993666A (en) | 1991-02-19 |
DE3790556C1 (de) | 1996-10-31 |
GB2207345A (en) | 1989-02-01 |
GB8810304D0 (en) | 1988-06-29 |
DE3631726A1 (de) | 1988-03-24 |
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