FASTENING SYSTEM FOR FASTENING AN OBJECT IN A VEHICLE

Abstract

A fastening system for fastening an object in a vehicle, in particular in an aircraft comprises at least one rail which is arranged on the vehicle side, and an object which is to be releasably fastened on the rail. The object can be positively fixed on the rail by way of at least one fastening device which is arranged on the object side. Spring means are provided on the fastening device, and these produce a non-positive fit between the fastening device and the rail, given a positive arrangement of the fastening device on the rail.

Claims

1. A fastening system in a vehicle, comprising: at least one rail arranged on a vehicle side, the at least one rail configured to releasably fasten an object; at least one fastening device arranged on an object side, the at least one fastening device configured to positively fix the object on the rail; and spring means configured to be provided on the fastening device, the-spring means, with a positive arrangement of the fastening device on the rail, configured to produce a non-positive fit between the fastening device and the rail.

2. A fastening system according to claim 1, wherein the fastening device comprises at least one receiver for the rail, wherein the rail and the receiver are configured to form a non-positive connection to one another.

3. A fastening system according to claim 2, wherein the rail in an end region facing the object comprises a widening having a cross section tapering in a wedge-shaped manner in a direction of the object, wherein the at least one receiver has a cross-sectional contour corresponding to the widening.

4. A fastening system according to claim 2, wherein two receivers for the rail and which are distanced to one another are formed on the fastening device, wherein at least one locking element which is connected via the spring means to the object is arranged in an intermediate space between the receivers.

5. A fastening system according to claim 1, further comprising_two locking hooks provided on the fastening device, the two locking hooks configured to articulate on a pivot, wherein a first side of one of the two locking hooks and a second side of the other of the two locking hooks away from the first side engage around an end region of the rail which is configured to face the object.

6. A fastening system according to claim 5, wherein the pivot includes a longitudinal extension, wherein the pivot is configured to be elastically yielding to the longitudinal extension.

7. A fastening system according to claim 5, wherein the locking hooks are each configured as a two-sided lever and each comprise an elongate hole, through which the pivot is configured to be led.

8. A fastening system according to claim 7, further comprising spreading means configured to spread force arms of the locking hooks, wherein the spreading means are arranged between the force arms.

9. A fastening system according to claim 1, wherein the object to be fastened includes a passenger service unit configured to be fastened in a passenger aircraft on two rails which are arranged above passenger seats in a supply channel.

10. A fastening device for fastening an object on a rail which is arranged in a vehicle, wherein the fastening device is configured to be connectable to the object, wherein the fastening device is configured to be positively fixed on the rail, and wherein the fastening device includes spring means, wherein the spring means are configured to create a non-positive fit between the fastening device and the rail given a positive arrangement of the fastening device on the rail.

11. A fastening device according to claim 10, further comprising at least one receiver for the rail arranged on a vehicle side, wherein the receiver is configured to form a non-positive connection to the rail.

12. A fastening device according to claim 10, further comprising two receivers which are distanced to one another and are for the rail arranged on a vehicle side, wherein at least one locking element is configured to be connected to the spring means and is arranged in a free space between the receivers.

13. A fastening device according to claim 10, further comprising two locking hooks configured to articulate on a pivot and positively encompass the rails.

14. A fastening device according to claim 13, wherein the pivot includes a longitudinal extension, wherein the pivot is configured to elastically yield transverse to the longitudinal extension.

15. A fastening device according to claim 13, wherein the locking hooks are each configured as a two-sided lever and each comprise an elongate hole, through which the pivot is configured to led.

16. A fastening device according to claim 15, further comprising spreading means configured to spread force arms of the locking hooks, wherein the spreading means are arranged between the force arms.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0017] The invention is hereinafter explained in more detail by way of embodiment examples shown in the drawing. Shown in the drawings in each case in a schematically simplified manner and in different scales are:

[0018] FIG. 1 in a lateral view, a fastening device of a fastening system for fastening an object on a rail,

[0019] FIG. 2 a sectioned view along the section line A-A in FIG. 1, with the fastening device in the fastening condition,

[0020] FIG. 3 the sectioned view according to FIG. 2, wherein the fastening device is not in the fastening condition,

[0021] FIG. 4 in a perspective view, a fastening system with a module of a passenger service unit which is fastened in an aircraft on rails.

[0022] FIG. 5 the fastening system according to FIG. 4, in a lateral view,

[0023] FIG. 6 in a perspective view, a fastening system with a panel which is fastened in an aircraft on rails,

[0024] FIG. 7 the fastening system according to FIG. 6, in a lateral view,

[0025] FIG. 8 a detail of FIG. 5, and

[0026] FIG. 9 a detail of FIG. 7.

DETAILED DESCRIPTION

[0027] FIGS. 1 to 3 show a fastening device 2 for fastening an object on a rail 4 which is arranged on a ceiling of an aircraft which is not evident from FIGS. 1 to 3, wherein this object has been omitted in FIGS. 1 to 3 for the purpose of a better overview.

[0028] The rail 4, away from the fastening device 2, comprises a strip-like section 6, onto which a widening 8 connects in the direction of the fastening device 2. As is evident from FIGS. 2 and 3, the widening 8 has an essentially triangular contour, wherein the widening 8 tapers in a wedge-like manner in the direction of the fastening device 2.

[0029] The fastening device 2 is provided with a base body 10. This base body 10 in a lateral view has a U-shaped cross-sectional profile, wherein in each case an section 14 and 16 runs normally to the section 12 in the direction of the rail 4, at the two ends of a section 12 of the base body 10 which is aligned parallel to the rail 4 in the fastened condition of the fastening device 2 on the rail 4.

[0030] A recess which in the fastened condition of the fastening device 2 on the rail 4 forms a receiver 18 for the widening 8 formed on the rail 4 is formed in each case on the sections 14 and 16 of the base body 10. The receivers 18 which are formed on the sections 14 and 16 of the base body 10 have a triangular cross-sectional contour, corresponding to the widening 8 which is formed on the rail 4.

[0031] The sections 14 and 16 of the base body 10 of the fastening device 2 moreover in each case have a through-hole 20 which is aligned parallel to the section 12 of the base body 10. A pivot 22 is led through the through-holes 20 aligned to one another, on the sections 14 and 16 of the base body 10. The pivot 22 is formed from a spring material, for example of spring steel. Two locking hooks 24 and 26 are pivotably articulated on the pivot 22 in a manner such that they can be pivoted towards one another and away from one another.

[0032] The articulation of the locking hooks 24 and 26 on the pivot 22 is effected on a projection 28 which is formed on the two locking hooks 24 and 26 and which is aligned transversely to the main longitudinal extension of the locking hook 24 and 26 respectively, wherein the projection 28 which is formed on the locking hook 24 points in the direction of the locking hook 26 and the projection 28 formed on the locking hook 26 projects in the direction of the locking hook 24. A longitudinal hole 30 is formed in each case on the projections 28 of the two locking hooks 24 and 26, for receiving the pivot 22.

[0033] The two locking hooks 24 and 26 are in each case designed as a two-sided lever, wherein a section of the locking hook 24 which is away from the rail 4 with regard to the projection 28 in the fastening condition of the fastening device 2 forms a force arm 24a, and a section of the locking hook 24 which faces the rail forms a load arm 24b. In a manner corresponding to this, a section of the locking hook 26 which in the fastening condition of the fastening device 2 is away from the rail 4 with respect to the projection 28 forms a force arm 26a and a section of the locking hook 26 which faces the rail 4 forms a load arm 26b. A projection 32 is formed in each case at the two ends of the load arms 24b and 26b of the locking hooks 24 and 26, wherein the two projections 32 face one another. The locking hooks 24 and 26 with their projection 32 in each case grip around or encompass the widening 8 formed on the rail 4, in the fastening condition of the fastening device 2 on the rail 4, by which means the fastening device 2 and the object which is connected thereto are positively fixed on the rail 4.

[0034] The movement control of the locking hooks 24 and 26 is effected via a control body 34. This control body 34 is rotatably mounted in an intermediate space between the force arms 24a and 26a of the locking hooks 24 and 26. The control body 34 can be actuated from outside the fastening device 2. For this, an opening 36, through which a shaft 38 connected to the control body 34 is led, is formed on the section 12 of the base body 10.

[0035] The control body 34, given a rounded outer contour has a significantly greater length compared to its width and can be rotated from a first position, in which its longitudinal extension runs normally to the connection direction of the two force arms 24a and 26a (FIG. 3), into a second position, in which its longitudinal extension corresponds to the connection direction of the two force arms 24a and 26a (FIG. 2). The force arms 24a and 26a of the locking hooks 24 and 26 are spread away from one another by way of the control body 34 being rotated from the first into the second position, and the load arms 24b and 26b of the locking hooks 24 and 26 are pivoted towards one another into their position positively fixing the fastening device. Hereby, apart from the pivot movement of the locking hooks 24 and 26, a pull movement of the locking hooks 24 and 26, by way of which a clamping force X is exerted onto the pivot 22 and an additional holding force Y is exerted onto the widening 8 of the rail 4 occurs due to the elongate holes 30 which are formed on the projections 28 of the two locking hooks 24 and 26. Moreover, the sections 14 and 16 of the base body 10 of the fastening device 2 are pressed with a force Z against the rails 4, by which means a non-positive fit between the fastening device 2 with the object connected thereto and the rail 4 is produced in the contact region of the widening 8 of the rail 4 and of the receivers 18 which are formed on the sections 14 and 16 of the base body 10.

[0036] FIGS. 4, 5 and 8 show the application of the previously described fastening device 2 in combination with the fastening of a module 40 of a passenger service unit in a passenger aircraft, said module being equipped with an emergency oxygen supply device. The module 40 is arranged hanging in a supply channel 42 which is formed in a passenger cabin of the passenger aircraft above the passenger seats.

[0037] The module 40 comprises a base plate 44 which faces the passenger seats. A housing 46, in which an emergency oxygen supply device is arranged, is formed on a side of the base plate 4 which faces the supply channel 42. In each case two fastening devices 2 are connected to the module 40 via connection elements 52, in the region of the two longitudinal sides 48 and 50 of the base plate 44. The fastening devices 2 correspond to the fastening devices 2 which are described by way of FIGS. 1-3.

[0038] Two longitudinal beams 56 and 58 are arranged on a wall 54 which delimits the supply channel 42 to the top, in a manner distanced to one another transversely to the longitudinal extension of the supply channel 42. A rail 4 which corresponds to the rails 4 represented in FIGS. 1-3 is arranged in each case on the longitudinal side of the beam 56 and 58 which is away from the wall 54. The module 40, with two fastening devices 2 which are arranged in the region of the longitudinal side 48 of the base plate 44, is fastened on the rail 4 arranged on the longitudinal beam 56, and the module 40, with two fastening devices 2 arranged in the region of the longitudinal side 48 of the base plate 44, is fastened on the rail 4 arranged on the longitudinal beam 58.

[0039] FIGS. 6, 7 and 9 show the application of the previously described fastening device 2, in combination with the fastening of a panel 60 which is likewise arranged in the supply channel 42 formed above the passenger seats. As is the case with the module 40, the panel 60 also comprises a base plate 62 which faces the passenger seats. In each case two fastening devices 2 are connected to the panel 60 via connection elements 52′, in the region of the two longitudinal sides 64 and 66 of the base plate 62. In FIGS. 6, 7 and 9, the fastening devices 2 also correspond to the fastening devices 2 described by way of FIG. 1-3. The panel 60 is fastened on the rail 4 arranged on the longitudinal beam 56, by two fastening devices 2 which are arranged in the region of the longitudinal side 64 of the base plate 62, and the panel 60 is fastened on the rail 4 arranged on the longitudinal beam 58, by two fastening devices 2 arranged in the region of the longitudinal side 66 of the base plate 62.

LIST OF REFERENCE NUMERALS

[0040] 2—fastening device

[0041] 4—rail

[0042] 6—section

[0043] 8—widening

[0044] 10—base body

[0045] 12—section

[0046] 14–section

[0047] 16—section

[0048] 18—receiver

[0049] 20—through-hole

[0050] 22—pivot

[0051] 24—locking

[0052] 24a—force arm

[0053] 24b—force arm

[0054] 26—locking hooks

[0055] 26a—force arm

[0056] 26b—load arm

[0057] 28—projection

[0058] 30—elongate hole

[0059] 32—projection

[0060] 34—control body

[0061] 36—opening

[0062] 38—shaft

[0063] 40—module

[0064] 42—supply channel

[0065] 44—base plate

[0066] 46—housing

[0067] 48—longitudinal side

[0068] 50—longitudinal side

[0069] 52, 52′—connection element

[0070] 54—wall

[0071] 56—longitudinal beam

[0072] 58—longitudinal beam

[0073] 60—panel

[0074] 62—base plate

[0075] 64—longitudinal side

[0076] 66—longitudinal side

[0077] X—biasing force

[0078] Y—force

[0079] Z—force