# US 10,871,013 B2 · Load transfer interface for a vehicle door, in particular for an aircraft cabin door > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 10,871,013 B2 - Document ID: US10871013B2 - Status: Granted - Kind: B2 - Application number: 15/647,477 - Filed: 2017-07-12 - Published: 2018-02-01 - Granted: 2020-12-22 - Earliest claimed: 2016-07-29 - Assignees: Airbus Helicopters Deutschland GmbH - Applicants: Airbus Helicopters Deutschland GmbH - Inventors: Matthias Schwab - Web page: https://patentgrep.com/patent/US10871013B2 ## CPC - E05B 85/24: Bolts rotating about an axis - B64C 1/1407: {Doors; surrounding frames} - B64C 1/1423: {Passenger doors} - E05B 79/12: using connecting rods - E05B 83/36: Locks for passenger or like doors - E05Y 2900/502: for aircraft or spacecraft - E05B: LOCKS; ACCESSORIES THEREFOR; HANDCUFFS - B64C: AEROPLANES; HELICOPTERS - E05Y: INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF ## Abstract A load transfer interface for a vehicle door that comprises an outer skin and at least one beam that is connected to the outer skin, wherein the outer skin and the at least one beam define a vehicle door plane, the load transfer interface comprising at least one door stop fitting that is provided to transfer pressure loads from the vehicle door to an associated vehicle structural frame, the at least one door stop fitting being provided for rotation in an associated rotation plane, wherein the associated rotation plane is at least approximately parallel to the vehicle door plane. The invention is further related to an aircraft cabin door having such a load transfer interface, as well as to an aircraft having such an aircraft cabin door. ## Claims ### Claim 1 A load transfer interface for a pressurized vehicle door that comprises an outer skin and a plurality of beams spaced parallel and connected to the outer skin, wherein the outer skin and the plurality of beams define a vehicle door plane, each beam having at least two door stop fittings to transfer pressure loads from the vehicle door to a vehicle structural frame, wherein the plurality of beams are arranged in parallel and the door stop fittings are rotatable in a rotation plane, substantially parallel to the vehicle door plane, each of the door stop fittings being mounted in a non-rotatable manner to an actuating lever, each actuating lever connected by a lateral linkage to at least another of the door stop fittings of another of the beams, each lateral linkage connected to at least two door stop fittings from two different beams, each lateral linkage arranged in parallel, the lateral linkage providing mechanical linkages actuatable via a handle, the handle being rotatable so that rotation of the handle results in movement of the lateral linkages into movement directions, which force the door stop fittings arranged in parallel to rotate. ### Claim 2 (depends on 1) The load transfer interface according to claim 1, wherein each of the door stop fittings comprise a rotating arm that defines a rotation axis for each respective door stop fitting, the rotation axis substantially perpendicular to the vehicle door plane. ### Claim 3 (depends on 2) The load transfer interface according to claim 2, wherein each rotating arm is mounted to at least one of the beams by at least one bearing adapted to allow rotation of the rotating arm around the rotation axis. ### Claim 4 (depends on 3) The load transfer interface according to claim 3, wherein the at least one bearing comprises a first bearing that is mounted to at least one of the beams by a lug bracket, the lug bracket retaining the first bearing at the at least one beam. ### Claim 5 (depends on 4) The load transfer interface according to claim 4, wherein the lug bracket is detachably mounted to the at least one beam by means of at least one fastener. ### Claim 6 (depends on 4) The load transfer interface according to claim 4, wherein the at least one bearing comprises a second bearing that is accommodated in a longitudinal beam extension of the at least one beam. ### Claim 7 (depends on 4) The load transfer interface according to claim 4, wherein the at least one bearing is a slide bearing. ### Claim 8 (depends on 2) The load transfer interface according to claim 2, wherein the rotating arm is connected to at least one actuating lever that is provided for rotating the rotating arm between open and close positions. ### Claim 9 (depends on 8) The load transfer interface according to claim 8, wherein the at least one actuating lever is connected to at least one mechanical linkage that is actuatable via a handle. ### Claim 10 (depends on 8) The load transfer interface according to claim 8, wherein the rotating arm is provided with an adjustment member that is adapted for adjusting a longitudinal extension of the rotating arm. ### Claim 11 (depends on 10) The load transfer interface according to claim 10, wherein the adjustment member is connected to the at least one beam via a washer. ### Claim 12 (depends on 10) The load transfer interface according to claim 10, wherein a filler is provided for filling out space in the at least one beam adjacent to the adjustment member. ### Claim 13 (depends on 1) The load transfer interface according to claim 1, wherein each of the door stop fittings comprise a stopper that is adapted to be pressed against a contra-stop fitting provided on the vehicle structural frame to which the vehicle door is mountable. ### Claim 14 An aircraft with an aircraft fuselage structure and a pressurized aircraft cabin door mounted to the aircraft fuselage structure, wherein the aircraft comprises at least one load transfer interface, the pressurized aircraft cabin door comprises an outer skin and a plurality of beams spaced parallel and connected to the outer skin, wherein the outer skin and the plurality of beams define an aircraft cabin door plane, each beam having at least two door stop fittings to transfer pressure loads from the door to the aircraft fuselage structure, wherein the plurality of beams are arranged in parallel and the door stop fittings are rotatable in a rotation plane, substantially parallel to the vehicle door plane, each of the door stop fittings being mounted in a non-rotatable manner to an actuating lever, each actuating lever connected by a lateral linkage to at least another of the door stop fittings of another of the beams, each lateral linkage connected to at least two door stop fittings from two different beams, each lateral linkage arranged in parallel, the lateral linkage providing mechanical linkages actuatable via a handle, the handle being rotatable so that rotation of the handle results in movement of the lateral linkages into movement directions, which force the door stop fittings arranged in parallel to rotate. ### Claim 15 (depends on 1) The load transfer interface according to claim 1, wherein the load transfer interface is located on the vehicle door. ### Claim 16 (depends on 1) The load transfer interface according to claim 1, wherein the door stop fittings are mounted to the beams. ### Claim 17 (depends on 2) The load transfer interface according to claim 2, wherein each of the rotating arms is mounted to a respective one of the beams. ### Claim 18 A load transfer interface for a pressurized vehicle door, the pressurized vehicle door comprising an outer skin and a plurality of beams, the beams being spaced parallel to each other and connected to the outer skin, the outer skin and the plurality of beams defining a vehicle door plane, each of the beams having two door stop fittings to transfer pressure loads from the vehicle door to a vehicle structural frame, the door stop fittings being rotatable in a rotation plane substantially parallel to the vehicle door plane, each of the door stop fittings mounted in a non-rotatable manner to an actuating lever, each actuating lever connected by a lateral linkage to at least another of the door stop fittings on another of the beams, each lateral linkage connected to spaced door stop fittings from different beams, each lateral linkage arranged in parallel, the lateral linkage providing mechanical linkages actuatable via a rotatable handle so that rotation of the handle results in movement of the lateral linkages to rotate the door stop fittings. ### Claim 19 (depends on 18) The load transfer interface according to claim 18, wherein each of the door stop fittings comprise a rotating arm that defines a rotation axis for each respective door stop fitting. ### Claim 20 (depends on 18) The load transfer interface according to claim 18, wherein each of the door stop fittings are mounted to the beams and comprise a stopper that is adapted to be pressed against an associated a contra-stop fitting provided on the vehicle structural frame to which the vehicle door is mountable.