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Adjustable mounting assemblies for groups of seats in aircraft or other vehicles

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Publication number
US3785600A
US3785600A US3785600DA US3785600A US 3785600 A US3785600 A US 3785600A US 3785600D A US3785600D A US 3785600DA US 3785600 A US3785600 A US 3785600A
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Prior art keywords
beams
means
mounting
seats
assembly
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Expired - Lifetime
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F Padovano
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1P Ind Chimica Arredamento S P
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/06Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B64D11/0696Means for fastening seats to floors, e.g. to floor rails
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/06Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS, WEDGES, JOINTS OR JOINTING
    • F16B37/00Nuts or like thread-engaging members
    • F16B37/04Devices for fastening nuts to surfaces, e.g. sheets, plates
    • F16B37/045Devices for fastening nuts to surfaces, e.g. sheets, plates specially adapted for fastening in channels, e.g. sliding bolts, channel nuts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS, WEDGES, JOINTS OR JOINTING
    • F16B7/00Connections of rods or tubes, e.g. of non-circular section, mutually, including resilient connections
    • F16B7/04Clamping or clipping connections
    • F16B7/044Clamping or clipping connections for rods or tubes being in angled relationship
    • F16B7/0446Clamping or clipping connections for rods or tubes being in angled relationship for tubes using the innerside thereof

Abstract

An adjustable mounting for a group of chairs or other articles comprises a pair of beams supported from a floor or other load bearing structure. The chair mountings are secured in selected positions in channels extending along the beams. The beam support are secured in selected positions in other channels extending along the beams, the positions of the floor supports being independent of the position of the floor mountings.

Description

United States Patent [191 Padovano 1 ADJUSTABLE MOUNTING ASSEMBLIES FOR GROUPS OF SEATS IN AIRCRAFT OR OTHER VEHICLES [75] Inventor:

[73] Assignee:

Felix Padovano, Rome, Italy 1P Industria Chimica per IArredamento S.p.A., Rome, Italy [22] Filed: Jan. 25, 1972 [21] Appl. No.: 220,606

[52] US. Cl. 248/188.l, 297/248 [51] Int. Cl. Fl6m 11/20 [58] Field of Search 248/188.1, 424, 429,

248/244, 245; 287/541, 52.05, 53 LK, 189.36 F; 108/64; 297/344, 346, 248; 211/182; 85/1 H; 151/41.7l

[56] References Cited UNITED STATES PATENTS 866,695 Taussig 248/245 Jan. 15, 1974 1,041,264 10/1912 Freud 248/245 2,812,800 11/1957 Eames 2,853,119 9/1958 Balfour.....

3,077,364 2/1963 Eppink 297/248 FOREIGN PATENTS OR APPLICATIONS 1,021,879 3/1966 Great Britain 248/245 Primary ExaminerMarion Parsons, Jr. AttorneyEric H. Waters et a1.

[57] ABSTRACT An adjustable mounting for a group of chairs or other articles comprises a pair of beams supported from a floor or other load bearing structure. The chair mountings are secured in selected positions in channels extending along the beams; The beam support are secured in selected positions in other channels extending along the beams, the positions of the floor supports being independent of the position of the floor mountings.

5 Claims, 12 Drawing Figures PAIENIED JAN! 5 m4 SHEET 1 0F 3 Fig.1

, tions along the beams.

1 ADJUSTABLE MOUNTING ASSEMBLIES FOR GROUPS OF SEATS IN AIRCRAFT OR OTHER VEHICLES FIELD OF THE INVENTION The invention relates to adjustable mounting assemblies for groups of articles, and more particularly to adjustable mounting assemblies for groups of'seats in aircraft or other vehicles.

In the cabin of an aircraft or other vehicle for example, it is necessary to utilise the maximum available space, and to ensure that the seats are anchored to an appropriate structure, and preferably it should be possible to adjust quickly the arrangement of the seats according to the requirements.

In the case of aircraft, the seats must be very firmly anchored and the position of the anchorage must correspond to the fixed position of load-bearing elements in the aircraft structure. Additionally it is often necessary to modify the relative position of the seats for example to totally or partially change the seats category from first class to economy class or vice-versa.

SUMMARY OF'THE INVENTION According to the invention, there is provided in a mounting assembly for a group of articles, a pair of beams, mounting means for each article of the group secured in independent selected positions along the beams, and means supporting the beams, the supporting means being secured in independent selected posi- BRIEF DESCRIPTION OF THE DRAWINGS Embodiments-of the invention will now be described, by way of example only, with reference to the accompanying diagrammatic drawings, in which: 1

FIG. 1 is a fragmentary plan view illustrating an arrangement of seats in an aircraftcabin;

FIG. 2 is a section, to an enlargedscale, taken on line ll-'-II of FIG. 1, and showing seats carried by a mounting assembly in accordance with thepresent invention;

FIG. 3 is a section taken on line lll-III of FIG. 2;

FIG. 4 is a fragmentary cross-section of the mounting assembly;

FIG. 5 is a fragmentary longitudinal section of the mounting assembly;

FIG. 6 is a cross-section of a beam of the mounting assembly;

FIG. 7 is a perspective view of a shoeof the mounting assembly; I

FIG. 8 is an underneath plan view of the shoe;

FIG. 9 is a section taken on line IXIX of FIG. 8;

FIGS. 10 and 11 are perspective views of modified forms of supports in the mounting assembly; and

FIG. 12 is an exploded perspective view of a modified form of cradle for use in the mounting assembly of three forms of anchoring assemblies.

DESCRIPTION OF THE PREFERRED EMBODIMENTS As shown in FIGS. 1 to 2, an aircraft cabin-comprises a wall 1, and a floor 3 having a load-bearing structure 3A for anchoring seats 5. The profile of the wall 1 in longitudinal and transverse section, and thus the profile of the lateral edge of the floor 3, is dependent upon the shape of the fuselage and not upon required arrangement of the seats 5. The seats 5 are in the form of armchairs having an adjustable back part and are assembled throughout the cabin in several different arrangements, i.e., in groups 5A of three seats arranged side by side, or in groups 58, 5C or SD of two seats arranged side by side and differently spaced from one another. The seats are mounted on the floor 3 through a mounting arrangement which permits independent adjustment of the lateral spacing and the position of the seats of the various groups of seats and the spacing and the position of the seat anchorage. Thus a'wide range of adjustment is possible, even although the various components may be mass produced. Each group of seats is mounted on a pair of beams 7 of identical crosssection; in the embodiment shown the beams 7 are tubular to provide light-weight beams, but could alternatively be solid. The beams 7 as shown, are generally circular in cross-section but can alternately be of other suitable shape. Each beam 7 is provided with at least two longitudinally extending undercut channels 7A, the channels 7A suitably being of dovetail section and diametrically opposed.

The beams 7 of each group of seats are anchored to the structure 3A through two supports 9, each of the supports9 being arranged to hold the two beams 7 in such a manner that the latter are laterally spaced by a distance corresponding to the lateral spacing between supports 10 provided in each seat 5. The supports 9 are assembled in any conventional manner on the floor and carry at their upper ends concave cradles 9A which receive the beams 7. The supports 10 carry cradles 10A through which the seat 5 is mounted on the beams 7.

To provide an adjustable connection between the cradles 9A and the corresponding beams 7, a shoe 12 slidable along each channel 7A and having side walls complementary to those of the channel is secured to a respective cradle 9A of screws 14. The screws 14 pass through holes in the cradles 9A and are threadedly engaged with the shoe 12; by tightening the screws 14, the shoes 12 can be firmly clamped in" wedging engagement against the side walls of the channels 7A. A similar arrangement using shoes 12A engaged with screws 14A passing through holes in thecradles 10A is provided to effect an adjustable connection between the cradles 10A and the beams 7.

It is apparent that the supports 9 can carry the beams 7 irrespective of the spacing and the position of the supports 9 with respect to the floor and irrespective of the required length of beams 7. The seats of each group can be moved laterally with respect to one another and with respect to the floor and walls of the cabin in any desired manner; it is possible to arrange a different number of seats in each group according to the requirements, and also to replace when necessary, the beams 7 by other beams of different length. In particular, the seats can be grouped as shown in FIG. 1 or can be grouped to provide different numbers of seats on either side of the central gangway of the cabin. As will be apparent, the width and position of the central gangway can be adjusted as required, by appropriately positioning the various groups of seats.

There is shown inv FIGS. 7, 8 and 9 a light-weight shoe, such as the shoe 12, which is especially suitable for use in aircraft. The shoe is hollow, is of channel section, and is reinforced by internal webs 12X. Threaded holes for the screws 14 are formed in projections extending from the base wall of the shoe.

ln FIGS. and 11 there are shown alternative embodiments of supports combined with the beams 7 to meet specific requirements, the supports comprising tubular elements to which the cradles are welded and are connected by means of webs or the like. FIG. 12 shows an exploded view of a modified form of cradle of a seat-mounting support or of a beam-mounting support. The cradle 22 shown in FIG. 12 has lugs 22A for the linkage for instance of a hydraulic cylinder for governing the inclination of the back part of the seat. The beams 7 can also be used to support seat accessories and supplementary devices.

The mounting assembly particularly described enables mass production of the seats in a desired size or sizes, and of the various components of the assembly. A wide range of adjustment is possible and the assembly can readily be demounted; the beams 7 can be replaced by beams of different lengths to vary the number of chairs. Chairs of different sizes can be used, also with the capability of adjustment of the spacing between the chairs. The supports can all be similar and arranged in several positions according to the positioning requirements in the cabin.

The positioning of the seats can readily be adjusted and a substantial reduction in cost is provided by mass producing the components and standardising the components to as high a degree as is possible.

Additionally means such as back part inclination devices, or safety belts for example can be fixed to the beams or sections.

The mounting assembly in accordance with the invention can be used for mounting objects other than seats I claim:

1. In a mounting assembly for a group of articles, a pair of beams, mounting means for each article of the group secured in selected positions along the beams, and means supporting the beams, the supporting means being secured in selected positions along the beams independent of the positions of the mounting means, each of said beams having a pair of longitudinallyextending channels, the mounting means being slidable along one channel of each of said beams, and the support means being slidable along the other channel of each of said beams.

2. An assembly as claimed in claim 1 wherein each said channel comprises outwardly convergent side walls, said assembly further comprising shoe means slidable within each channel, and

screw means connecting each said mounting means and supporting means to a respective shoe means and rotatable to selectively clamp the shoe means in wedging engagement with the side walls of the channel.

3. An assembly as claimed in claim 2 wherein each said mounting means and supporting means comprises a cradle facing each said beam, said cradles being clamped against the beams when the associated shoe means is clamped in the channel.

4. An assembly as claimed in claim 2 wherein each said beam is tubular, and the channels are diametrically opposed and are of dovetail section.

5. An assembly as claimed in claim 4 wherein the shoe means have a cross-section complementary to that of the channels and are of hollow construction, each said shoe means including transverse reinforcing ribs.

Claims (5)

1. In a mounting assembly for a group of articles, a pair of beams, mounting means for each article of the group secured in selected positions along the beams, and means supporting the beams, the supporting means being secured in selected positions along the beams independent of the positions of the mounting means, each of said beams having a pair of longitudinallyextending channels, the mounting means being slidable along one channel of each of said beams, and the support means being slidable along the other channel of each of said beams.
2. An assembly as claimed in claim 1 wherein each said channel comprises outwardly convergent side walls, said assembly further comprising shoe means slidable within each channel, and screw means connecting each said mounting means and supporting means to a respective shoe means and rotatable to selectively clamp the shoe means in wedging engagement with the side walls of the channel.
3. An assembly as claimed in claim 2 wherein each said mounting means and supporting means comprises a cradle facing each said beam, said cradles being clamped against the beams when the associated shoe means is clamped in the channel.
4. An assembly as claimed in claim 2 wherein each said beam is tubular, and the channels are diametrically opposed and are of dovetail section.
5. An assembly as claimed in claim 4 wherein the shoe means have a cross-section complementary to that of the channels and are of hollow construction, each said shoe means including transverse reinforcing ribs.
US3785600A 1972-01-25 1972-01-25 Adjustable mounting assemblies for groups of seats in aircraft or other vehicles Expired - Lifetime US3785600A (en)

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Cited By (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3893729A (en) * 1974-11-18 1975-07-08 Mc Donnell Douglas Corp Convertible passenger seat
US4277101A (en) * 1979-01-23 1981-07-07 Ignaz Vogel Vehicle seat support
US4516710A (en) * 1974-07-08 1985-05-14 Bott John Anthony Article carrier for automotive vehicles
US4748913A (en) * 1982-10-27 1988-06-07 Innovative Metal Inc. Powered desk
US4911381A (en) * 1987-12-28 1990-03-27 Simula, Inc. Energy-absorbing leg assembly for aircraft passenger seats
US5246270A (en) * 1990-12-24 1993-09-21 Ignaz Vogel Gmbh & Co. Kg Passenger seat arrangement
WO1994023996A1 (en) * 1993-04-21 1994-10-27 Flight Equipment & Engineering Limited Convertible aircraft passenger seating
US5553923A (en) * 1993-12-08 1996-09-10 Weber Aircraft, Inc. Base frame for an aircraft seat
US5575532A (en) * 1993-11-06 1996-11-19 Keiper Recaro Gmbh & Co. Vehicle seat, in particular an airplane passenger seat
EP0745532A1 (en) * 1995-05-31 1996-12-04 Societe Industrielle Et Commerciale De Materiel Aeronautique (Sicma) Societe Anonyme A profile design for the assembly of a seating structure, specially an aircraft seat , and assembly process using this profile
US5636901A (en) * 1995-06-15 1997-06-10 Aircraft Modular Products, Inc. Aircraft passenger seat frame
US5868472A (en) * 1995-06-15 1999-02-09 Grilliot; Ronald Aircraft passenger seat frame
US5997081A (en) * 1997-01-08 1999-12-07 Honda Giken Kogyo Kabushiki Kaisha Seat for a vehicle
US6746076B2 (en) * 2000-09-27 2004-06-08 Daimlerchrysler Ag Windbreak device for an open motor vehicle
US20050168031A1 (en) * 2004-01-13 2005-08-04 Olarte Alvaro M. Pew or bench with pivoting seat
US20060186723A1 (en) * 2005-02-18 2006-08-24 Eric Kawabata Troop seat
US20070080258A1 (en) * 2005-09-06 2007-04-12 Andreas Baatz Modular seat system for a vehicle
US20070138849A1 (en) * 2004-01-13 2007-06-21 Olarte Alvaro M Pew Style Seating Assembly
US20080001050A1 (en) * 2006-07-03 2008-01-03 Fabrice Morel Mounting interface systems and methods for purposes of testing seat tracks
US20090108132A1 (en) * 2006-03-31 2009-04-30 Recaro Aircraft Seating Gmbh & Co. Kg Seating Apparatus
US7562937B2 (en) * 2005-12-10 2009-07-21 Recaro Aircraft Seating Gmbh & Co. Kg Seat support apparatus with torque support
DE102009014720A1 (en) * 2009-03-27 2010-09-30 Recaro Aircraft Seating Gmbh & Co. Kg Seat frame device
DE102009014721A1 (en) * 2009-03-27 2010-10-07 Recaro Aircraft Seating Gmbh & Co. Kg Seat frame device
US20110068226A1 (en) * 2005-09-06 2011-03-24 Airbus Deutschland Gmbh Modular seat system for a vehicle
US20110101162A1 (en) * 2008-05-07 2011-05-05 Zim Gmbh Kit for seat rows in aircraft
US20120212020A1 (en) * 2011-02-23 2012-08-23 Benno Schiefer Vehicle seat, in particular passenger seat in a passenger transportation vehicle
US20160297533A1 (en) * 2015-04-13 2016-10-13 Encore Seats, Inc. Aircraft seating assembly

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US866695A (en) * 1906-07-13 1907-09-24 Maurice Taussig Adjustable support for shelving.
US1041264A (en) * 1909-12-28 1912-10-15 Maurice Freud Supporting-arm for display-cases.
US2812800A (en) * 1956-05-03 1957-11-12 Herman Miller Furniture Compan Multiple seating assembly
US2853119A (en) * 1953-09-10 1958-09-23 Balfour Lionel Maxwell Joachim Seat-supporting structures for mounting on roofs of motor cars and the like
US3077364A (en) * 1959-09-28 1963-02-12 California Church Furniture Co Stadium seating structure
GB1021879A (en) * 1963-12-24 1966-03-09 Hille & Company Ltd S Improvements in and relating to wall brackets

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US866695A (en) * 1906-07-13 1907-09-24 Maurice Taussig Adjustable support for shelving.
US1041264A (en) * 1909-12-28 1912-10-15 Maurice Freud Supporting-arm for display-cases.
US2853119A (en) * 1953-09-10 1958-09-23 Balfour Lionel Maxwell Joachim Seat-supporting structures for mounting on roofs of motor cars and the like
US2812800A (en) * 1956-05-03 1957-11-12 Herman Miller Furniture Compan Multiple seating assembly
US3077364A (en) * 1959-09-28 1963-02-12 California Church Furniture Co Stadium seating structure
GB1021879A (en) * 1963-12-24 1966-03-09 Hille & Company Ltd S Improvements in and relating to wall brackets

Cited By (50)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4516710A (en) * 1974-07-08 1985-05-14 Bott John Anthony Article carrier for automotive vehicles
US3893729A (en) * 1974-11-18 1975-07-08 Mc Donnell Douglas Corp Convertible passenger seat
US4277101A (en) * 1979-01-23 1981-07-07 Ignaz Vogel Vehicle seat support
US4748913A (en) * 1982-10-27 1988-06-07 Innovative Metal Inc. Powered desk
US4911381A (en) * 1987-12-28 1990-03-27 Simula, Inc. Energy-absorbing leg assembly for aircraft passenger seats
US5246270A (en) * 1990-12-24 1993-09-21 Ignaz Vogel Gmbh & Co. Kg Passenger seat arrangement
WO1994023996A1 (en) * 1993-04-21 1994-10-27 Flight Equipment & Engineering Limited Convertible aircraft passenger seating
US5575532A (en) * 1993-11-06 1996-11-19 Keiper Recaro Gmbh & Co. Vehicle seat, in particular an airplane passenger seat
US5553923A (en) * 1993-12-08 1996-09-10 Weber Aircraft, Inc. Base frame for an aircraft seat
EP0745532A1 (en) * 1995-05-31 1996-12-04 Societe Industrielle Et Commerciale De Materiel Aeronautique (Sicma) Societe Anonyme A profile design for the assembly of a seating structure, specially an aircraft seat , and assembly process using this profile
FR2734786A1 (en) * 1995-05-31 1996-12-06 Sicma Aero Seat Profile and method for assembling seat structure elements of aircraft, structural members, assembly and structure thus realized
US5762440A (en) * 1995-05-31 1998-06-09 Societe Industrielle Et Commerciale De Materiel Aeronautique Section member for assembling structural elements of a seat, corresponding structural elements, an assembly thereof, a seat structure including such an assembly, and a method of assembly
US5636901A (en) * 1995-06-15 1997-06-10 Aircraft Modular Products, Inc. Aircraft passenger seat frame
US5868472A (en) * 1995-06-15 1999-02-09 Grilliot; Ronald Aircraft passenger seat frame
US5997081A (en) * 1997-01-08 1999-12-07 Honda Giken Kogyo Kabushiki Kaisha Seat for a vehicle
US6746076B2 (en) * 2000-09-27 2004-06-08 Daimlerchrysler Ag Windbreak device for an open motor vehicle
US7814636B2 (en) 2004-01-13 2010-10-19 Series International, Llc Seating system and assembly
US20050168032A1 (en) * 2004-01-13 2005-08-04 Olarte Alvaro M. Seating system and assembly
WO2005069799A2 (en) * 2004-01-13 2005-08-04 Multiple Llc D/B/A Series Usa Pew and bench with pivoting seat
US20110029123A1 (en) * 2004-01-13 2011-02-03 Alvaro Mauricio Olarte Seating System and Assembly
WO2005069799A3 (en) * 2004-01-13 2006-08-31 Multiple Llc D B A Series Usa Pew and bench with pivoting seat
US20100301648A1 (en) * 2004-01-13 2010-12-02 Alvaro Mauricio Olarte Pew Style Seating Assembly
US7204553B2 (en) * 2004-01-13 2007-04-17 Multiple Llc Pew or bench with pivoting seat
US20070107178A1 (en) * 2004-01-13 2007-05-17 Olarte Alvaro M Pew And Bench With Pivoting Seat
US20070138849A1 (en) * 2004-01-13 2007-06-21 Olarte Alvaro M Pew Style Seating Assembly
US20050168031A1 (en) * 2004-01-13 2005-08-04 Olarte Alvaro M. Pew or bench with pivoting seat
US7467453B2 (en) * 2004-01-13 2008-12-23 Series International, Llc Pew and bench with pivoting seat
US7478876B2 (en) * 2004-01-13 2009-01-20 Series International, Llc Seating system and assembly
US20090105862A1 (en) * 2004-01-13 2009-04-23 Alvaro Mauricio Olarte Seating System and Assembly
US8075055B2 (en) 2004-01-13 2011-12-13 Series International Llc Pew style seating assembly
US7828380B2 (en) 2004-01-13 2010-11-09 Series International, Llc Pew style seating assembly
US20060186723A1 (en) * 2005-02-18 2006-08-24 Eric Kawabata Troop seat
US7594701B2 (en) * 2005-02-18 2009-09-29 Conax Florida Corporation Troop seat
US20070080258A1 (en) * 2005-09-06 2007-04-12 Andreas Baatz Modular seat system for a vehicle
US8870119B2 (en) 2005-09-06 2014-10-28 Airbus Operations Gmbh Modular seat system for a vehicle
US7857259B2 (en) * 2005-09-06 2010-12-28 Airbus Deutschland Gmbh Modular seat system for a vehicle
US20110068226A1 (en) * 2005-09-06 2011-03-24 Airbus Deutschland Gmbh Modular seat system for a vehicle
EP1795444A3 (en) * 2005-12-10 2012-02-08 Recaro Aircraft Seating GmbH & Co. KG Supporting device for a seat
US7562937B2 (en) * 2005-12-10 2009-07-21 Recaro Aircraft Seating Gmbh & Co. Kg Seat support apparatus with torque support
US20090108132A1 (en) * 2006-03-31 2009-04-30 Recaro Aircraft Seating Gmbh & Co. Kg Seating Apparatus
US7628370B2 (en) * 2006-07-03 2009-12-08 Weber Aircraft Llc Mounting interface systems and methods for purposes of testing seat tracks
US20080001050A1 (en) * 2006-07-03 2008-01-03 Fabrice Morel Mounting interface systems and methods for purposes of testing seat tracks
US8393680B2 (en) * 2008-05-07 2013-03-12 Zim Gmbh Kit for seat rows in aircraft
US20110101162A1 (en) * 2008-05-07 2011-05-05 Zim Gmbh Kit for seat rows in aircraft
US20120098322A1 (en) * 2009-03-27 2012-04-26 Recaro Aircraft Seating Gmbh & Co. Kg Seat frame device
DE102009014721A1 (en) * 2009-03-27 2010-10-07 Recaro Aircraft Seating Gmbh & Co. Kg Seat frame device
DE102009014720A1 (en) * 2009-03-27 2010-09-30 Recaro Aircraft Seating Gmbh & Co. Kg Seat frame device
US20120212020A1 (en) * 2011-02-23 2012-08-23 Benno Schiefer Vehicle seat, in particular passenger seat in a passenger transportation vehicle
US9764844B2 (en) * 2015-04-13 2017-09-19 Encore Seats, Inc. Aircraft seating assembly
US20160297533A1 (en) * 2015-04-13 2016-10-13 Encore Seats, Inc. Aircraft seating assembly

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