Cargo hold component system for convertible cargo hold

Patent metadata

Field	Value
Publication number	US-11117645-B2
Application number	US-201815949727-A
Country	US
Kind code	B2
Filing date	Apr 10, 2018
Priority date	Apr 11, 2017
Publication date	Sep 14, 2021
Grant date	Sep 14, 2021

Abstract

A cargo hold component system for a cargo hold of an aircraft, the cargo hold component system including floor elements and fixing elements. The floor elements can at least partially be fixed releasably by the fixing elements to fixing sites provided on or in the hold floor, such that in a state fixed to the fixing sites, the floor elements support a loading of the hold with cargo containers, and that in a state in which a first group of the floor elements has been removed from the fixing sites by release of the fixing elements and a second group of the floor elements has been partially removed from the fixing sites by release of the fixing elements, the hold is sealed gas-tightly.

First claim

The invention claimed is:

1. A cargo hold component system for a cargo hold of an aircraft, the cargo hold component system comprising:
a plurality of floor elements for transporting and securing cargo in the cargo hold; and
a plurality of fixing elements;
wherein the floor elements are at least partially releasably fixable by the fixing elements to fixing sites on or in a cargo hold floor, such that, when fixed to the fixing sites, the floor elements support a loading of the cargo hold with cargo containers and, when a first group of the floor elements is removed from the fixing sites by release of the fixing elements and a second group of the floor elements is partially removed from the fixing sites by release of the fixing elements, the cargo hold is configured for sealing in a gas-tight manner.

2. The cargo hold component system according to claim 1 , wherein at least one of the floor elements is configured as part of a roller conveyor, which is fixable in a longitudinal direction of the cargo hold and on which the cargo containers are movable.

3. The cargo hold component system according to claim 2 , wherein the roller conveyor is formed multipiece, and wherein a first part of the roller conveyor is fixedly attachable on or in the cargo hold floor and a second part of the roller conveyor is releasably fixable to the first part.

4. The cargo hold component system according to claim 2 , wherein the roller conveyor has a counter fixing element configured to cooperate with one of the fixing elements such that, in a fixed state, the fixing element and the counter fixing element are form fit together to prevent movement of the roller conveyor in at least two directions.

5. The cargo hold component system according to claim 4 , wherein the counter fixing element is configured to cooperate with one of the fixing elements such that, in a fixed state, the fixing element and the counter fixing element are form fit together to prevent movement of the roller conveyor in at least a longitudinal direction and a height direction of the cargo hold and, in a released state, at least one part of the roller conveyor is movable in at least one direction of the cargo hold.

6. The cargo hold component system according to claim 5 , wherein the at least one direction is the longitudinal direction of the cargo hold.

7. The cargo hold component system according to claim 1 , wherein at least one of the floor elements is a ball mat that is releasably fixable at one of the fixing sites, which is in a region of a loading opening of the cargo hold.

8. The cargo hold component system according to claim 7 , wherein the ball mat comprises, on an outer face, at least one of the fixing elements, which comprises at least one protrusion that protrudes from the outer face and is configured to cooperate with at least one counter fixing element, which comprises an associated opening, of a roller conveyor that is fixable in the longitudinal direction of the cargo hold, such that, in a fixed state, the fixing element and the counter fixing element are form fit together to prevent movement of the ball mat in at least a longitudinal direction and a height direction of the cargo hold and, in a released state, the ball mat is movable in at least the height direction of the cargo hold.

9. The cargo hold component system according to claim 7 , wherein the ball mat comprises, on an outer face, a counter fixing element configured to cooperate with one of the fixing elements at an associated lock, such that, in a fixed state, the one of the fixing elements and the counter fixing element are form fit together to prevent movement of the ball mat in longitudinal, transverse, and height directions of the cargo hold and, in a released state, the ball mat is movable in at least the height direction of the cargo hold.

10. The cargo hold component system according to claim 1 , wherein one or more of the floor elements is a loading hatch lock and/or an inlet guide, which is/are each releasably fixable at one of the fixing sites, which is in a region of a loading opening of the cargo hold.

11. The cargo hold component system according to claim 10 , wherein the one or more of the floor elements each comprise, on at least one outer face, at least one of the fixing elements, which comprises a protrusion that protrudes from the at least one outer face and is configured to cooperate with a counter fixing element, which comprises an associated opening, of a roller conveyor that is fixable in the longitudinal direction of the cargo hold, such that, in a fixed state, the fixing element and the counter fixing element are form fit together to prevent movement of the one or more of the floor elements in at least a longitudinal direction and a height direction of the cargo hold and, in a released state, the one or more of the floor elements are movable in at least the height direction of the cargo hold.

12. The cargo hold component system according to claim 10 , wherein the one or more of the floor elements each comprise, on an underside, an undercut protrusion configured to engage in a guide rail that is firmly fixable in the cargo hold, such that, in a fixed state, the undercut protrusion and the guide rail are form fit together to prevent movement of the one or more of the floor elements in at least a transverse direction or a height direction of the cargo hold and, in a released state, the one or more of the floor elements are movable in at least the transverse direction of the cargo hold.

13. The cargo hold component system according to claim 10 , wherein the loading hatch lock and/or the inlet guide is/are each fixedly connected to, or formed integrally with, a ball mat.

14. The cargo hold component system according to claim 1 , wherein at least one of the floor elements is configured as a two-piece lock.

15. The cargo hold component system according to claim 14 , wherein a first part of the two-piece lock is fixedly attachable to the cargo hold floor or to a primary structure of the aircraft and a second part of the two-piece lock is releasably fixable to the first part.

16. The cargo hold component system according to claim 14 , wherein:
the two-piece lock comprises a protrusion configured to cooperate with a counter fixing element of one of the floor elements such that, in a fixed state, the protrusion and the counter fixing element are form fit together to prevent a movement of the one of the floor elements in longitudinal, transverse and height directions of the cargo hold and, in a released state, the one of the floor elements is movable in at least the height direction of the cargo hold, and/or
the two-piece lock comprises at least one roller, which supports loading and unloading of the cargo hold with cargo containers.

17. An aircraft with a cargo hold component system, the cargo hold component system comprising:
a plurality of floor elements for transporting and securing cargo in the cargo hold; and
a plurality of fixing elements;
wherein the floor elements are at least partially releasably fixable by the fixing elements to fixing sites on or in a cargo hold floor, such that, when fixed to the fixing sites, the floor elements support a loading of the cargo hold with cargo containers and, when a first group of the floor elements is removed from the fixing sites by release of the fixing elements and a second group of the floor elements is partially removed from the fixing sites by release of the fixing elements, the cargo hold is configured for sealing in a gas-tight manner.

Assignees

• Airbus Operations Gmbh

Inventors

• Nowarre Sascha
• Scherenberger Sven
• Kahle Stephan
• Behrens Rasmus

Classifications

• Y02T50/40

  Weight reduction · CPC title

• B64C2211/00

  Modular constructions of airplanes or helicopters · CPC title

• B64D9/003

  Devices for retaining pallets or freight containers · CPC title

• B65G13/11

  Roller frames · CPC title

• B64C1/20 Primary

  specially adapted for freight · CPC title