Service device, passenger service unit, fuselage of an aircraft, method for installing the service device
The invention relates to a service device having a system of a gasper module and a lighting module for a passenger service unit of an aircraft, comprising: a lighting source in a housing of the lighting module for providing light and a gasper orifice in a housing of the gasper module for supply of gasper air, wherein the lighting module and the gasper module are assembled in a housing assembly of the service device, wherein the housing assembly is adapted to hold the lighting module and the gasper module essentially around an axis (Z) of the housing assembly. According to the invention the lighting module and the gasper module are separated from each other by a housing assembly bearing part, and a force transmission is applicable to the lighting module and the gasper module for independent movement of at least one of the lighting module and the gasper module relative to the bearing part, and wherein the gasper module housing and the lighting module housing are separately form fitted to the bearing part by a positive locking.
1. A service device having a gasper module and a lighting module for a passenger service unit of an aircraft, the service device comprising:
a lighting source in a lighting module housing for providing light; and
a gasper orifice in a gasper module housing for supplying gasper air, wherein
the lighting module and the gasper module are assembled in a housing assembly of the service device, wherein the housing assembly is adapted to hold the lighting module and the gasper module substantially around an axis of the housing assembly,
wherein:
the lighting module and the gasper module are separated from each other by a housing assembly bearing part;
a force transmission is applicable to the lighting module and the gasper module for independent movement of at least one of the lighting module and the gasper module relative to the housing assembly bearing part;
the gasper module housing and the lighting module housing are separately form fitted to the housing assembly bearing part by a positive locking; and
wherein the housing assembly comprises an outer ring housing and an inner ring housing, the inner ring housing having the housing assembly bearing part and the outer ring housing having a further housing assembly bearing part, the further housing assembly bearing part having an inner bearing ring surface engaging an outer curved ring surface of the lighting module housing.
2. The service device according to claim 1 wherein the form fitting of the gasper module housing and the lighting module housing to the housing assembly bearing part is at:
an outer curved ring surface of the gasper module housing such that the form fitting follows at least partially along a length of an inner bearing ring surface of the housing assembly bearing part; and
an inner curved ring surface of the lighting module housing such that the form fitting follows at least partially along a length of an outer bearing ring surface of the housing assembly bearing part; and
wherein
a distance part is positioned between at least one of the inner and outer bearing ring surfaces of the housing assembly bearing part and the respective curved ring surface.
3. The service device according to claim 1 wherein at least one of:
a single engagement line of an engaging ring surface of the gasper module housing extends without spacing to the housing assembly bearing part at least partially along a length of the axis of the housing assembly;
a single engagement line of an inner engaging ring surface of the lighting module housing extends without spacing to the housing assembly bearing part at least partially along the length of the axis of the housing assembly; and
a single engagement line of an outer engaging ring surface of the lighting module housing extends without spacing to the further housing assembly bearing part at least partially along the length of the axis of the housing assembly.
4. The service device according to claim 1 wherein the positive locking makes use of:
an extremal point of an outer curved ring surface of the gasper module housing, wherein the extremal point exceeds an inlet of an inner bearing ring of the housing assembly bearing part, wherein the extremal point of the outer curved ring surface of the gasper module housing corresponds to a widest part of the gasper module housing; and
an extremal point of the outer curved ring surface of the lighting module housing, wherein the extremal point exceeds an inlet part of an outer bearing ring surface of the housing assembly bearing part, wherein the extremal point of the outer curved ring surface of the lighting module housing corresponds to a widest part of the lighting module housing.
5. The service device according to claim 1 wherein a middle engagement line between an outer curved ring surface of the gasper module housing and an inner bearing ring surface of the housing assembly bearing part and an outermost engagement line between an outer curved ring surface of the lighting module housing and an inner bearing ring surface of the further housing assembly bearing part form a two sided conically closing intake between the housing assembly bearing part and the further housing assembly bearing part for acceptance of the lighting module housing.
6. The service device according to claim 1 wherein the lighting and gasper modules comprise a pivot line in the housing assembly for adapting a rotary movement of the form fitted modules.
7. The service device according to claim 1 wherein the gasper module housing comprises a pivot point for adapting a pivoting movement of the form fitted gasper module and a slew round with an angle of from of approximately −60° to approximately +60° relative to the axis of the housing assembly for producing an air gasper volume in a deflected position by the force transmission and such that the gasper module can be rotated upon the axis.
8. The service device according to claim 1 wherein the lighting module housing comprises a pivot point in the housing assembly for adapting a pivoting movement of the form fitted lighting module and a slew round with an angle of from approximately −45° to approximately +45° relative to the axis of the housing assembly for producing a light cone in a deflected position by the force transmission.
9. The service device according to claim 1 wherein the lighting module comprises a reading light unit and a color light unit for signalling an attendant call, wherein the reading light and color light units are arranged on a printed circuit board.
10. The service device according to claim 1 wherein the lighting module comprises a translucent inner ring for allowing the emission of light from an attendant call light integrated in the lighting module.
11. The service device according to claim 1 wherein the gasper module comprises a die exit arranged in an inner part of the inner ring housing of the housing assembly.
12. A method for installing the service device as claimed in claim 1 in connection with at least one passenger seat in the aircraft.
13. Passenger service unit comprising the service device according to claim 1 wherein the service device is integrated in the passenger service unit.
14. A fuselage of an aircraft comprising a passenger cabin and a number of the service devices according to claim 1 .
15. The service device according to claim 1 wherein the positive locking is accomplished without any additional fixing elements.
16. The service device according to claim 1 wherein a surface of a translucent inner ring abuts an outer bearing ring curved surface of the housing assembly bearing part, the housing assembly bearing part having an extremal point that coincides with a reversal point of the surface of the translucent inner ring when the lighting module and the gasper module are aligned along the axis of the housing assembly, wherein the extremal point of the housing assembly bearing part corresponds to a widest part of the housing assembly bearing part.
17. A service device having a gasper module and a lighting module for a passenger service unit of an aircraft, the service device comprising:
a lighting source in a lighting module housing for providing light; and
a gasper orifice in a gasper module housing of the gasper module for supplying gasper air, wherein:
the lighting module and the gasper module are assembled in a housing assembly of the service device substantially around an axis of the housing assembly;
the lighting module and the gasper module are separated from each other by a housing assembly bearing part;
at least one of the lighting module and the gasper module is configured to move independently relative to the housing assembly bearing part; and
the gasper module housing and the lighting module housing are separately form fitted to the housing assembly bearing part by a positive locking at:
an outer curved ring surface of the gasper module housing such that the form fitting follows at least partially along a length of an inner bearing ring surface of the housing assembly bearing part; and
an inner curved ring surface of the lighting module housing such that the form fitting follows at least partially along a length of an outer bearing ring surface of the housing assembly bearing part, and
wherein a distance part is positioned between at least one of the inner and outer bearing ring surfaces of the housing assembly bearing part and the respective curved ring surface.
18. The service device according to claim 17 wherein the distance part is positioned between the outer curved ring surface of the gasper module housing and the inner bearing ring surface of the housing assembly bearing part.
19. The service device according to claim 17 wherein the distance part is positioned between the inner curved ring surface of the lighting module housing and the outer bearing ring surface of the housing assembly bearing part.
20. The service device according to claim 17 wherein the distance part is a translucent ring.
21. The service device according to claim 17 wherein the positive locking is accomplished without any additional fixing elements.
22. A service device having a gasper module and a lighting module for a passenger service unit of an aircraft, the service device comprising:
a lighting source in a lighting module housing for providing light; and
a gasper orifice in a gasper module housing of the gasper module for supplying gasper air, wherein:
the lighting module and the gasper module are assembled in a housing assembly of the service device substantially around an axis of the housing assembly;
the lighting module and the gasper module are separated from each other by a housing assembly bearing part;
at least one of the lighting module and the gasper module is configured to move independently relative to the housing assembly bearing part;
the gasper module housing and the lighting module housing are separately form fitted to the housing assembly bearing part by a positive locking; and
a surface of a translucent inner ring engages an outer bearing ring curved surface of the housing assembly bearing part, the housing assembly bearing part having an extremal point that coincides with a reversal point of the surface of the translucent inner ring when the lighting module and the gasper module are aligned along the axis of the housing assembly, wherein the extremal point of the housing assembly bearing part corresponds to a widest part of the housing assembly bearing part.
23. The service device according to claim 22 wherein the positive locking is accomplished without any additional fixing elements.
24. The method of claim 12 further comprising using a die-tool to form fit the gasper module housing and the lighting module housing in the housing assembly.
25. The service device according to claim 2 wherein the distance part is positioned between the outer curved ring surface of the gasper module housing and the inner bearing ring surface of the housing assembly bearing part.
26. The service device according to claim 2 wherein the distance part is positioned between the inner curved ring surface of the lighting module housing and the outer bearing ring surface of the housing assembly bearing part.
27. The service device according to claim 2 wherein the distance part is a translucent ring.