Connection arrangement and structure

Patent metadata

Field	Value
Publication number	US-9493224-B2
Application number	US-201414555618-A
Country	US
Kind code	B2
Filing date	Nov 27, 2014
Priority date	Dec 3, 2013
Publication date	Nov 15, 2016
Grant date	Nov 15, 2016

Abstract

An energy-absorbing connection arrangement with a multitude of connectors for joining two components, such as a transverse member and a circular frame element, of an aircraft fuselage. Each connector comprises a headed shaft and the shafts reach through component boreholes. On the shaft ends facing away from the heads, counter-bearings are provided. At least one of the components comprises a fiber-reinforced plastic material. A head and/or counter-bearing of at least one connector rests against at least one underlay device. The underlay device is received in a guide groove in the first component, with the guide groove commencing in the region of the boreholes. The underlay device, upon exceeding a mechanical threshold load, is slidable away from the boreholes. Energy absorption takes place along a longitudinal center axis of the guide groove as a result of hole-bearing-stress failure and/or the shearing of the fiber-reinforced plastic material component.

First claim

The invention claimed is:

1. An energy-absorbing connection arrangement for joining at least two components, comprising:
a multitude of connectors, wherein each connector comprises a head with a shaft, and the shafts reach through associated boreholes in the components,
counter-bearings located on ends of the shafts facing away from the heads,
a first of the components comprising a fiber-reinforced plastic material and at least one further component comprising at least one of a metallic material and a fiber-reinforced plastic material,
at least one of the heads and the counter-bearings of at least one of the connectors resting against at least one underlay device,
the at least one underlay device being received in at least one guide groove embedded at least in the first component, and
a commencement of the guide groove being in a region of the boreholes,
wherein as a result of exceeding a mechanical threshold load, the at least one underlay device is slidable in a direction facing away from the boreholes, and energy absorption takes place essentially along a longitudinal center axis of the at least one guide groove.

2. The connection arrangement according to claim 1 , wherein the underlay device is arranged to be slidable as a result of at least one of hole-bearing failure and shearing-off of the at least one component formed of fiber-reinforced plastic material.

3. The connection arrangement according to claim 1 , wherein the two components comprise a transverse member and a circular frame element of a fuselage cell structure of an aircraft.

4. The connection arrangement according to claim 1 , wherein the connectors are arranged in a matrix-like manner.

5. The connection arrangement according to claim 1 , wherein the connectors comprise at least one of rivets and threaded bolts with nuts as counter-bearings.

6. The connection arrangement according to claim 1 , wherein the underlay devices comprise an approximately rectangular circumferential contour and in each case an underlay device hole for feeding the shafts of the connectors through said holes.

7. The connection arrangement according to claim 1 , wherein a cross-sectional geometry of the underlay devices is one of rectangular, T-shaped and U-shaped.

8. The connection arrangement according to claim 1 , wherein at least one shaft of a connector comprises a reduced diameter when compared to the diameters of the remaining connectors.

9. The connection arrangement according to claim 1 , wherein the reinforcement fiber orientation within the matrix of the at least one component is selected so that maximum energy absorption is achieved as a result of materials failure.

10. The connection arrangement according to claim 1 , wherein a receiving groove is embedded, in a region of the guide groove, in at least one of the at least one guide groove and the region of an underside of the first component, which underside faces the second component.

11. The connection arrangement according to claim 10 , wherein at least one connector is positioned outside the receiving groove.

12. The connection arrangement according to claim 10 , wherein a region of at least one guide groove, which region faces away from a borehole in a receiving groove of the first component, is conical.

13. The connection arrangement according to claim 10 , wherein a depth of at least one of at least one guide groove and at least one receiving groove varies in some sections in a longitudinal direction of said grooves.

14. The connection arrangement according to claim 1 , wherein at least one transverse side of an underlay device, which transverse side extends transversely to a guide groove, comprises a recess.

15. The connection arrangement according to claim 14 , wherein the recess comprises an approximately semi-circular recess.

16. The connection arrangement according to claim 1 , wherein at least one connector is positioned in a shearing zone of the first component.

17. The connection arrangement according to claim 16 , wherein the heads of the connectors in the shearing zone are each received in associated shearing grooves whose shearing groove ends facing away from their associated boreholes are open, wherein a material thickness in the region of the shearing grooves is reduced.

18. A structure comprising at least two components that have been joined by means of an energy-absorbing connection arrangement, comprising:
a multitude of connectors, wherein each connector comprises a head with a shaft, and the shafts reach through associated boreholes in the components,
counter-bearings located on ends of the shafts facing away from the heads,
a first of the components comprising a fiber-reinforced plastic material and at least one further component comprising at least one of a metallic material and a fiber-reinforced plastic material,
at least one of the heads and the counter-bearings of at least one of the connectors resting against at least one underlay device,
the at least one underlay device being received in at least one guide groove embedded at least in the first component, and
a commencement of the guide groove being in a region of the boreholes,
wherein as a result of exceeding a mechanical threshold load, the at least one underlay device is slidable in a direction facing away from the boreholes, and energy absorption takes place essentially along a longitudinal center axis of the at least one guide groove.

Assignees

• Airbus Operations Gmbh

Inventors

• Hachenberg Dieter
• Margull Lars
• Kohlgrueber Dieter
• Waimer Matthias
• Kraft Harald

Classifications

• F16F7/127

  by a blade element cutting or tearing into a quantity of material; Pultrusion of a filling material · CPC title

• B64C1/062 Primary

  specially adapted to absorb crash loads · CPC title

• B64C1/18

  Floors · CPC title

• F16F7/08

  with friction surfaces rectilinearly movable along each other (F16F7/01 takes precedence {; one of the members being a spring F16F13/02}) · CPC title

• F16F7/124

  characterised by their special construction from fibre-reinforced plastics · CPC title