Granted Patent B2

US 12,731,972 · App. 18/905,559 · Granted Sep 8, 2026

Inventor: Lauritz Petersen (Hamburg, DE)

Assignee: Airbus Operations GmbH

H02G3/32B64C1/406B64D47/00F16L3/1218F16L3/127F16L3/20H02G3/26H02G3/30

Abstract

Claims (72)

1 . An extendable holding device for a supply line in an aircraft, the holding device comprising:

a supply line holding unit;

a fastener; and

an adaptable spacer;

wherein the supply line holding unit comprises an at least partly enclosed holding opening for holding a supply line;

wherein the fastener is configured to mount the supply line holding unit to a support structure;

wherein the adaptable spacer is configured to be arranged between the supply line holding unit and the support structure to which the holding device is to be mounted;

wherein the adaptable spacer is extendable in a longitudinal direction of the fastener and is temporarily lockable at least at a first and a second predetermined length;

wherein the adaptable spacer is extendable by a first spacer member and a second spacer member; and

wherein the fastener extends through each of supply line holding unit, the first spacer member, and the second spacer member.

2 . The holding device according to claim 1 ,

wherein the first spacer member is lockable at the second spacer member at least at the first and the second predetermined length; and

wherein the first and the at least second spacer member have a disengaged state between at least the first and the second predetermined length and are continuously shiftable in the longitudinal direction with respect to each other.

3 . The holding device according to claim 2 , wherein at least one of the first spacer member and the at least second spacer member comprises locking elements for locking the adaptable spacer at least at the first and the second predetermined length.

4 . The holding device according to claim 3 , wherein the locking elements at the first spacer member are complementary to the locking elements at the at least second spacer member.

5 . The holding device according to claim 3 , wherein the locking elements are arranged in a staggered pattern at at least one of the first spacer member or the at least second spacer member to reinforce the locking of the first and the at least second spacer member.

6 . The holding device according to claim 3 , wherein the locking elements are configured, such that their locking is enabled by a preload force.

7 . The holding device according to claim 3 ,

wherein at least a part of the adaptable spacer encloses the fastener; and

wherein the locking elements are configured to be secured by the fastener to prevent disengagement of the locking of the first and the second spacer member.

8 . The holding device according to claim 3 ,

wherein the first spacer member is formed as a primary hollow cylinder, providing an inner volume;

wherein the at least second spacer member is formed as secondary hollow cylinder, being insertable into the inner volume of the primary hollow cylinder;

wherein the secondary hollow cylinder encloses the fastener in its inner volume;

wherein the locking elements are provided from a primary and a secondary hollow cylinder wall; and

wherein the fastener secures the locking elements of the secondary hollow cylinder wall against the locking elements of the primary hollow cylinder wall.

9 . The holding device according to claim 2 ,

wherein the first spacer member and the at least second spacer member are rotatably locked in relation to each other;

wherein the first spacer member or the at least second spacer member comprises a guiding groove and the other member comprises a guiding pin engaged with the guiding groove; and

wherein the guiding groove and guiding pin prevent a separation of the first spacer member and the at least second spacer member.

10 . The holding device according to claim 2 , wherein at least one of the first spacer member or the at least second spacer member comprise insertion aiding elements at their end portions to facilitate insertion of the at least second spacer member into the first spacer member.

11 . The holding device according to claim 1 ,

wherein the adaptable spacer comprises at least one marker element at at least one of the first or second predetermined length; and

wherein the marker element is configured for indicating a length between the supply line holding unit and the support structure.

12 . A supply line arrangement, comprising:

an extendable holding device according to claim 1 ;

the supply line; and

the support structure;

wherein the supply line is mounted onto the support structure by the extendable holding device in a distance defined by the extendable holding device.

13 . An energy supply system comprising:

at least one supply line arrangement according to claim 12 ; and

a power source;

wherein the power source is connected to the at least one supply line arrangement to supply electric energy to power consuming loads.

14 . An aircraft, comprising:

at least one energy supply system according to claim 13 ; and

at least one power consuming load;

wherein the least one power consuming load comprises at least one of a group comprising: a propulsion system, electric avionic equipment and onboard electric devices for a cabin area; and

wherein the least one power consuming load is powered by the at least one energy supply system.

15 . A method for providing an extendable holding device for a supply line in an aircraft, comprising the following steps:

providing a supply line holding unit;

providing a fastener; and

providing an adaptable spacer;

wherein the supply line holding unit comprises an at least partly enclosed holding opening for holding a supply line;

wherein the fastener is configured to mount the supply line holding unit to a support structure;

wherein the adaptable spacer is configured to be arranged between the supply line holding unit and the support structure to which the holding device is to be mounted;

wherein the adaptable spacer is extendable in a longitudinal direction of the fastener and is temporarily lockable at least at a first and a second predetermined length;

wherein the adaptable spacer is extendable by a first spacer member and a second spacer member; and

wherein the fastener extends through each of the supply line holding unit, the first spacer member, and the second spacer member.

16 . An extendable holding device for a supply line in an aircraft, the holding device comprising:

a supply line holding unit;

a fastener; and

an adaptable spacer;

wherein the supply line holding unit comprises an at least partly enclosed holding opening for holding a supply line;

wherein the fastener is configured to mount the supply line holding unit to a support structure;

wherein the adaptable spacer is configured to be arranged between the supply line holding unit and the support structure to which the holding device is to be mounted;

wherein the adaptable spacer is extendable in a longitudinal direction of the fastener and is temporarily lockable at least at a first and a second predetermined length;

wherein the adaptable spacer is extendable by a first spacer member and a second spacer member;

wherein the first spacer member is lockable at the second spacer member at least at the first and the second predetermined length;

wherein the first and the at least second spacer member have a disengaged state between at least the first and the second predetermined length and are continuously shiftable in the longitudinal direction with respect to each other;

wherein at least one of the first spacer member and the at least second spacer member comprises locking elements for locking the adaptable spacer at least at the first and the second predetermined length;

wherein at least a part of the adaptable spacer encloses the fastener; and

wherein the locking elements are configured to be secured by the fastener to prevent disengagement of the locking of the first and the second spacer member.

Assignments (1)

Priority Claims (1)

Continuity (1)

References Cited (29)