Fastening device for releasably fastening a mechanism in the region of a floor of an aircraft or space craft and arrangement for a cargo loading system

Patent metadata

Field	Value
Publication number	US-10071796-B2
Application number	US-201615089909-A
Country	US
Kind code	B2
Filing date	Apr 4, 2016
Priority date	Jan 24, 2013
Publication date	Sep 11, 2018
Grant date	Sep 11, 2018

Abstract

A fastening device is disclosed for releasably fastening a mechanism in the region of a floor of an aircraft or spacecraft and includes a base component and a latch component. The latch component includes at least one holding portion including a latch-component-side holding face and is movably coupled to the base component between an unlocked and a locked position. When positioned in a predefined mounting position on the floor component and/or on the base component, the holding portion of the latch component engages a fastening portion, and the latch-component-side holding face faces the mechanism-side holding face. During passage of the latch component from locked position into unlocked position a gap between the latch-component-side holding face and the mechanism-side holding face continuously widens. The invention further relates to an arrangement for a cargo loading system.

First claim

What is claimed is:

1. A fastening device for releasably fastening a mechanism in a region of a cargo hold floor of an aircraft or spacecraft, the fastening device comprising:
a base component configured to be rigidly coupled to a floor component formed for introducing a load into the floor; and
a latch component which comprises at least one holding portion comprising a latch-component-side holding face and is coupled to the base component such that the latch component is movable between an unlocked position and a locked position with respect to the base component;
wherein the latch component is formed such that, when the mechanism is positioned in part in a predefined mounting position on the floor component and/or on the base component, the holding portion engages around a fastening portion, which is formed on the mechanism and comprises at least one mechanism-side holding face, in a region of the mechanism-side holding face during passage of the latch component into the locked position, such that the latch-component-side holding face faces the mechanism-side holding face;
wherein the latch component is formed such that the latch-component-side holding face can be brought into engagement with the mechanism-side holding face in a manner of a thread when the mechanism is positioned in the mounting position on the floor component and/or on the base component and the latch component is passing from the unlocked position into the locked position;
wherein the mechanism-side holding face forms a portion of a screw face; and
wherein the latch-component-side holding face is formed such that, during passage of the latch component from the locked position into the unlocked position, a gap between the latch-component-side holding face and the mechanism-side holding face continuously widens.

2. The fastening device of claim 1 , wherein the passage of the latch component into the locked position allows the latch-component-side holding face to be brought into planar contact with the mechanism-side holding face.

3. The fastening device of claim 1 , wherein the latch-component-side holding face forms a portion of a screw face.

4. The fastening device of claim 1 , wherein the latch component is rotatably mounted on the base component about an axis of rotation, the latch component being movable between the unlocked position and the locked position by a rotational movement about the axis of rotation.

5. The fastening device of claim 4 , wherein the passage of the latch component from the locked position into the unlocked position or from the unlocked position into the locked position can be brought about by twisting the latch component about the axis of rotation through an angle of less than 180 degrees or through an angle of substantially 90 degrees.

6. The fastening device of claim 1 , comprising a first resilient element, in particular a first spring, which is coupled to the base component and the latch component such that the first resilient element counters the passage of the latch component from the locked position into the unlocked position.

7. The fastening device of claim 6 , wherein the latch component and the base component are coupled to one another such that the latch component latches releasably at least in the locked position; and
the fastening device comprising a second resilient element, in particular a second spring, by which an engagement element, displaceably guided in the latch component, is resiliently coupled to the latch component, wherein at least one engagement recess associated with the locked position, and preferably additionally a further engagement recess associated with the unlocked position, is provided on the base component or on a part rigidly connected to the base component, the engagement element being configured to engage in the engagement recess or engagement recesses for releasable engagement under an action of the second resilient element.

8. The fastening device of claim 1 , wherein the latch component and the base component are coupled to one another such that the latch component latches releasably at least in the locked position.

9. The fastening device of claim 8 , comprising a resilient element, in particular a spring, by which an engagement element, displaceably guided in the latch component, is resiliently coupled to the latch component, wherein at least one engagement recess associated with the locked position, and preferably additionally a further engagement recess associated with the unlocked position, is provided on the base component or on a part rigidly connected to the base component, the engagement element being configured to engage in the engagement recess or engagement recesses for releasable engagement under an action of the resilient element.

10. The fastening device of claim 1 , wherein the base component comprises at least one support portion comprising at least one support face, and wherein, when in the unlocked position of the latch component, the fastening portion of the mechanism can be laid in part on the support face.

11. The fastening device of claim 1 , wherein the base component is formed such that it can be brought into positive engagement with the fastening portion of the mechanism when the mechanism is laid in part on the floor component and/or on the base component in the predefined mounting position, such that tensile loads can be transferred between the mechanism and the base component in a first direction, the first direction extending substantially perpendicular to a second direction, along which the fastening portion of the mechanism can be fixed by cooperation of the latch-component-side holding face and the mechanism-side holding face.

12. The fastening device of claim 11 , wherein the base component comprises a projection, which is formed and arranged such that the projection can be introduced into an associated opening of the mechanism when the mechanism is laid on the floor component and/or on the base component, so as to bring about the positive engagement, the projection preferably being formed such that it only fills up the associated opening of the mechanism in part upon engagement.

13. An arrangement for a cargo loading system of an aircraft or spacecraft, the arrangement comprising:
at least one mechanism, in particular a roller track, configured for moving, conveying, handling, or movably supporting cargo, in particular packaged goods cargo, cargo pallets, and/or cargo containers; and
at least one fastening device according to claim 1 for releasably fastening the mechanism in a region of a cargo hold floor of the aircraft or spacecraft;
wherein the fastening portion is formed with the at least one mechanism-side holding face on the mechanism.

14. The arrangement for a cargo loading system of claim 13 , wherein the mechanism is reversible, the fastening portion comprising an upper side and an underside and the mechanism-side holding face being formed in a same manner in each case in a region of the upper side and the underside of the fastening portion.

15. The arrangement for a cargo loading system of claim 13 , wherein the base component is formed such that it can be brought into positive engagement with the fastening portion of the mechanism when the mechanism is laid in part on the floor component and/or on the base component in the predefined mounting position, such that tensile loads can be transferred between the mechanism and the base component in a first direction, the first direction extending substantially perpendicular to a second direction, along which the fastening portion of the mechanism can be fixed by cooperation of the latch-component

Assignees

• Airbus Operations Gmbh

Inventors

• Esser Markus
• Lohmann Ali
• Pump Jörg
• Hager Sönke
• Völker Johannes

Classifications

• B65G13/11

  Roller frames · CPC title

• B64C1/20 Primary

  specially adapted for freight · CPC title

• B65G21/02

  consisting essentially of struts, ties, or like structural elements · CPC title

• B60R11/00

  Arrangements for holding or mounting articles, not otherwise provided for · CPC title

• B65G39/12

  mounted on framework · CPC title