EP2356025A2 - Unité d'alimentation pour canaux d'alimentation flexibles - Google Patents

Unité d'alimentation pour canaux d'alimentation flexibles

Info

Publication number
EP2356025A2
EP2356025A2 EP09740152A EP09740152A EP2356025A2 EP 2356025 A2 EP2356025 A2 EP 2356025A2 EP 09740152 A EP09740152 A EP 09740152A EP 09740152 A EP09740152 A EP 09740152A EP 2356025 A2 EP2356025 A2 EP 2356025A2
Authority
EP
European Patent Office
Prior art keywords
supply
supply unit
channel
attachment
supply channel
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.)
Withdrawn
Application number
EP09740152A
Other languages
German (de)
English (en)
Inventor
Uwe Schneider
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.)
Airbus Operations GmbH
Original Assignee
Airbus Operations GmbH
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 Airbus Operations GmbH filed Critical Airbus Operations GmbH
Publication of EP2356025A2 publication Critical patent/EP2356025A2/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • 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
    • B64D2011/0053—Cabin passenger reading lights
    • 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
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B64D2013/003—Cabin ventilation nozzles
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R25/00—Coupling parts adapted for simultaneous co-operation with two or more identical counterparts, e.g. for distributing energy to two or more circuits
    • H01R25/14—Rails or bus-bars constructed so that the counterparts can be connected thereto at any point along their length
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining

Definitions

  • the invention relates to the supply technology of passengers.
  • the invention relates to a supply unit for mounting on a supply channel of a means of transport, a supply channel of a means of transport for receiving such a supply unit, an aircraft and a method for mounting a supply unit to a supply channel of a means of transport.
  • a supply channel (Passenger Service Channel, PSC channel) equipped with functional panels and so-called functionless intermediate panels (also called infill panels) is provided above the seat rows in the direction of flight.
  • PSC channel Passenger Service Channel
  • an intermediate rail system for attachment of any panels an intermediate rail system is common, in which the panels are slidably displaced in the direction of flight with holders.
  • the arrangement of the PSC function panels in the direction of flight must be individual for each aircraft layout the seating position is to be carried out so that the passenger can comfortably use any functionality from the seat.
  • PSUs Passenger Service Units
  • RP 0 723 91 1 Al and US 5,651,733 disclose an arrangement for supplying passengers in an aircraft cabin, in particular in an aircraft.
  • the arrangement comprises a supply unit with comfort and Whycnc, as Leslieuchtc, Sluartruftasle, speakers and air nozzle.
  • the supply unit When installing the supply unit, the supply unit must be connected to the supply lines and then mechanically fixed.
  • the described embodiments relate equally to the supply unit, the supply channel, the aircraft and the method.
  • the features described below for example, with regard to the provision of care, can also be implemented in the aircraft or the method, and vice versa.
  • a supply unit for mounting to a supply channel of a means of transport which at least one supply element for a passenger, a fastening device for fastening the supply unit to the
  • Supply channel and a connection device for automatically connecting the supply element to the supply channel act together in such a way that the attachment and the automatic connection takes place in a working step.
  • the supply element is selected from the group consisting of lighting unit, loudspeaker unit, sign and air nozzle,
  • the supply unit can also have several of these supply elements.
  • a plurality of lighting units, air nozzles, speaker units and signs can be integrated into a supply unit. All these supply elements are automatically connected to the supply channel when the supply unit is brought into its final mounting position and fastened there.
  • the supply unit has a longitudinal direction, wherein a first supply element is an electrical consumer.
  • the connection device is designed for automatically connecting the electrical load to the supply channel and has at least one longitudinal contact for the automatic electrical contact of the electrical load during the fastening of the supply unit.
  • the supply unit has an air nozzle for providing an air flow to a passenger, the supply unit furthermore having a channel for supplying the air from a pressurized region of the supply channel to the air nozzle, and the channel for automatically mechanically sealing the connection Air nozzle is executed at the pressurized area in the attachment of the supply unit.
  • the air nozzle may be provided in addition to one or more electrical consumers (speakers, signs, reading lights) or alternatively thereto. Also, a plurality of air nozzles may be provided.
  • the fastening device has a snap device extending in the longitudinal direction of the supply unit.
  • the attachment of the supply unit is done in a simple manner by the supply unit is moved toward its final mounting position, wherein the snap-in connection engages when the supply unit is in the mounting position.
  • the supply unit is completely pre-assembled prior to attachment to the supply channel, so that after the attachment and the associated automatic connection no further assembly steps are necessary.
  • the supply unit has a transverse direction and a profiling, which extends in the longitudinal direction of the supply unit and is V-shaped in cross-section, for pre-centering the supply unit in the transverse direction before attachment.
  • a pre-centering of the supply unit takes place automatically by moving the supply unit to its mounting position.
  • Supply unit a toothing for fixing the supply unit in the longitudinal direction after attachment. In this way it can be avoided that the supply unit is moved in the longitudinal direction when the aircraft is exposed to a high acceleration, for example.
  • the means of transport is an aircraft. It can also be a rail vehicle, a bus or a ship.
  • a supply channel of a transport means for receiving a supply unit described above is specified, wherein the supply channel has a receiving device for fixing the supply unit by means of the fastening device and at least one interface for automatically connecting a supply element of the supply unit to the supply channel.
  • the supply channel has a first interface for automatic electrical Contacting an electrical consumer of the supply unit in the attachment of the supply unit.
  • the supply channel to a pressurized area and a second
  • the second interface may additionally or alternatively be seen as the first interface voi.
  • an aircraft is specified with at least one supply unit described above and at least one supply channel described above.
  • a method for mounting a supply unit to a supply channel of a transport means in which the supply unit is attached to the supply channel and a first supply element to the supply channel automatically at
  • Attachment is connected The supply unit and the supply channel act together in such a way that the fastening and the automatic connection takes place in one work step.
  • an automatic connection of a second supply element to the supply channel during fastening continues to take place.
  • additional, additional supply elements can be connected automatically during fastening.
  • FIG. 1 shows a perspective view of a luggage storage compartment with a supply channel and a supply unit to be attached thereto according to an exemplary embodiment of the invention.
  • FIG. 2 shows a sectional representation of a supply channel with a supply unit attached thereto according to an exemplary embodiment of the invention.
  • Fig. 3 shows a perspective view of a luggage storage compartment
  • Supply channel and a supply unit to be attached thereto according to a further embodiment of the invention.
  • FIG. 4 shows a sectional view through the supply channel of FIG. 3 with the supply unit attached thereto.
  • FIG. 5 shows a sectional view through a partial region of a supply channel with a connected supply unit according to an exemplary embodiment of the invention.
  • FIG. 6 shows a sectional view through a partial region of a supply channel with a connected supply unit according to an exemplary embodiment of the invention.
  • FIG. 7 shows a detail from FIG. 6.
  • Fig. 9 shows an aircraft according to an embodiment of the invention.
  • FIG. 10 shows a flow chart of a method according to an embodiment of the invention
  • FIG. 1 shows a perspective view of a luggage storage compartment 210 with a supply channel 200 attached thereto and a supply unit 100 to be attached to this supply channel.
  • the supply channel 200 has a plurality of connections 204, 205, 206 which can be arranged over the entire length of the supply channel.
  • These interfaces or connections are, for example, plugs with spring contacts, which can be integrated in the fastening profile of the supply channel 200. For example, three such interfaces per luggage tray (hat rack), which runs over four frames, are provided.
  • the supply unit 100 consists of a module which is provided for the supply of one or more passengers. It has a plurality of reading lights 101, a speaker 102 and a sign (sign) 103. These
  • Supply unit (PSU panel) is equipped with a corresponding roof profile and completely pre-assembled and equipped before assembly. Alone by the movement in Z-direction 111 along the arrow 130, the supply unit 100 is mechanically locked and electrically connected.
  • the supply unit 100 For locking to the supply channel, the supply unit 100 has longitudinal profiles 105, 106, which engage in corresponding fastening profiles 208, 209 (see FIG. 2) of the supply channel.
  • the supply unit 100 For the connection of the electrical power elements, the supply unit 100 has on its upper side a connection device 107 in the form of one or more elongated electrical contacts which can be contacted by corresponding contact pins of the spring contacts 204, 205, 206 when the supply unit is installed. Due to the longitudinal extent of the contact strips 107, it is irrelevant on which X-position 109 the supply unit 100 is mounted exactly. Possibly. It can also be moved later.
  • FIG. 2 shows a cross-sectional view through a supply channel 200 and a supply unit 100 mounted thereon.
  • the supply channel 200 in turn is attached to a luggage storage compartment 210.
  • the supply channel 200 has a left and a right lateral outer Befest Whilespro fil 208, 209 and a left and a right lateral inner mounting profile 202, 203.
  • the outer Befest Whilespro file 208, 209 are used for attachment or locking of the fastening devices 105, 106 of the supply unit .
  • the fastening devices 105, 106 each have a hook or a hook-shaped fastening profile, which correspond to the fastening profiles 208, 209 of the supply channel.
  • the fastening profiles 208, 209 made of an elastic material, such as plastic, running.
  • the actuating lever 116 can be actuated.
  • the roof profile 1 17, 118 of the supply unit 100 has two V-shaped profiles 1 13, which are designed for pre-centering of the supply unit in the transverse direction 110 when the supply unit is moved in the direction of the final assembly position.
  • the inner fastening profiles 202, 203 engage in the corresponding V-shaped profiles 1 13 and guide the supply unit in its upward movement to the correct Y position.
  • the conductor tracks for contacting are integrated in the roof profile of the supply unit (see reference numeral 107).
  • Reference numeral 120 shows a possible installation space for the different supply elements.
  • FIG. 3 shows a luggage storage compartment with a supply channel 200 attached thereto and a supply unit 100 to be attached thereto according to a further exemplary embodiment of the invention.
  • the supply unit 100 has three air nozzles 104, which are connected to the supply channel solely by the movement of the supply unit in the Z direction 1 1 1.
  • Fig. 4 shows a sectional view of the embodiment of Fig. 3 with installed supply unit.
  • the reference numeral 201 denotes a pressurized portion of the supply passage.
  • This pressurized area 201 has an outlet in the form of a tubular portion 207, over which the tube 108 is slipped.
  • the sealing of the pressurized area 201 takes place.
  • corresponding sealing elements are provided at the interfaces 401, 402. Due to the elastic design of the supply 100, the interfaces 401, 402 press against each other when the supply unit 100 is in the assembly position.
  • FIG. 5 shows a partial section of the sectional view of FIG. 2 for better clarification of the electrical contacting between the supply unit 100 and the supply channel 200.
  • a plug 502 which has a plurality of spring-loaded plug pins 501 which contact the contact lines 107 of the supply unit when it is in the mounting position.
  • the V-shaped profile 113 serves to Y-position the supply unit and the tolerance recording.
  • the roof profile 118 is designed for example as a plastic extruded profile with metal inserts.
  • Electro lines extend in supply units with electrical supply elements over its entire length (see reference numeral 107).
  • the Befcst Trentsprofil 209 is designed as a plastic extruded profile.
  • the Dachprocho 1 18 abuts during the upward movement of the supply unit during assembly to the webs 202, 203 of the supply channel and presses the assembly into the catch.
  • the loading of the supply unit and the supply channel in area 106 pulls the supply unit up with the roof profile (ie in the Z direction).
  • Fig. 7 shows a cross-sectional view of the detail X of Fig. 6, which illustrates the pre-centering for mounting in the Y / Z direction. Due to the V-shaped design of the supply unit in the region 113, the web 203 automatically guides the supply unit in its movement into the correct Y position and the correct Z position.
  • Fig. 8 shows a sectional view taken along the line A-A of Fig. 7, which has a rolled fine teeth 1 12, 801 for fixing the supply unit 100 to the supply channel 200 in the X direction.
  • the assembly takes place by simple Nachobencalorie the supply unit 100.
  • the contacting takes place in the same work step.
  • the assembly fixes itself and gravity supports the positive connection.
  • the contact is protected and shielded. Easy unlocking is possible without a special tool.
  • the supply channel consists of a fastening profile arranged over the entire X-length under the hatrack, which contains a fixed plug in certain regular sections.
  • the electrified PSUs have at the top over inserted tracks in the entire X-extension of the PSUs, which are automatically zwangsAuthiert when verraslen in the mounting position.
  • each connector is programmed so that the PSU contacted underneath is actuated according to its mode of operation. This design ensures that even with a conservative system architecture (each device has its own data bus in the form of an individual wiring) a significant assembly time reduction is achieved.
  • the PSUs are positioned in the X direction by the rolled-up fine toothing for fixation, which is rolled on during the continuous casting process.
  • the contact is made via the plug from the hatrack underside, via spring contacts integrated in the plug, to the connector track, which is integrated into the roof profile of the PSU.
  • the entire framework of panel, roof profile and fastening profile results in a non-positive connection, which ensures the contact at any time.
  • the profiles allow the inclusion of an "Individual Air Channel" with appropriate sealing, without requiring a separate piping.
  • Attachment, contacting and possibly piping can be carried out in one step, at the respectively designated position.
  • the assembly is intrinsically stable, without additional closure or stiffening parts are required.
  • Gravity supports positive locking, ie the PSU panel pushes down into the catch so that the fastening is redundant.
  • the electrical contacts are against moisture, flashover and
  • the system is suitable for on-board and off-board pre-assembly.
  • the roof profile includes no inserted tracks 107, so that weight can be saved.
  • the profiles allow with appropriate sealing the inclusion of an "Individual Air Channel", without requiring a separate piping.
  • the necessary components are simplified compared to conventional components. Furthermore, functionalities are integrated multiple times, which leads to a component reduction, reduces the interfaces and uses physical effects.
  • Supply channel are suitable for preconception of large hatrack modules outside the aircraft (e.g., directly at the modulator).
  • the current Airbus system architecture (CIDS) can be retained.
  • CIDS software customization
  • FIG 9 shows an aircraft according to an embodiment of the invention, which has a plurality of supply units 100 and a plurality of supply channels 200.
  • supply channels 200 may be made longer or shorter. Also, more than two supply channels can be arranged. Likewise, further supply units 100 may be connected to the supply channels 200.
  • step 1001 the supply unit is moved toward the supply channel.
  • the movement is for example straight in the Z direction.
  • step 1002 the supply unit is attached to the supply channel in one and the same step automatic connection of several supply elements to the supply channel.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Pulmonology (AREA)
  • Installation Of Indoor Wiring (AREA)
  • Mobile Radio Communication Systems (AREA)
  • Automatic Assembly (AREA)

Abstract

Dans un exemple de réalisation de l'invention, il est fourni une unité d'alimentation pour le montage sur un canal d'alimentation d'un aéronef comprenant un dispositif de fixation et un dispositif de raccordement. Ces deux dispositifs coopèrent ensemble afin que la fixation et le raccordement automatique se fassent en une étape de travail lorsque l'unité d'alimentation est amenée dans la position de montage.
EP09740152A 2008-11-20 2009-10-26 Unité d'alimentation pour canaux d'alimentation flexibles Withdrawn EP2356025A2 (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US19981508P 2008-11-20 2008-11-20
DE102008058271A DE102008058271A1 (de) 2008-11-20 2008-11-20 Versorgungseinheit für flexible Versorgungskanäle
PCT/EP2009/064061 WO2010057744A2 (fr) 2008-11-20 2009-10-26 Unité d'alimentation pour canaux d'alimentation flexibles

Publications (1)

Publication Number Publication Date
EP2356025A2 true EP2356025A2 (fr) 2011-08-17

Family

ID=42114481

Family Applications (1)

Application Number Title Priority Date Filing Date
EP09740152A Withdrawn EP2356025A2 (fr) 2008-11-20 2009-10-26 Unité d'alimentation pour canaux d'alimentation flexibles

Country Status (4)

Country Link
US (1) US8474755B2 (fr)
EP (1) EP2356025A2 (fr)
DE (1) DE102008058271A1 (fr)
WO (1) WO2010057744A2 (fr)

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Also Published As

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WO2010057744A2 (fr) 2010-05-27
US20110240796A1 (en) 2011-10-06
WO2010057744A4 (fr) 2010-09-16
US8474755B2 (en) 2013-07-02
WO2010057744A3 (fr) 2010-07-15
DE102008058271A1 (de) 2010-05-27

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