Patent Application
20130318767
The invention concerns a method for purposes of supporting and aligning a component supported in a desired orientation in a supporting device at a plurality of support points; it also concerns a supporting device for purposes of supporting and aligning a component in a desired orientation.
The fuselage of an aircraft is conventionally subdivided into a plurality of fuselage sections; these are joined via transverse seams to form the aircraft fuselage. Depending upon the size of the aircraft the cross-sections and lengths of the fuselage sections vary. For purposes of joining the fuselage sections these are usually supported at four support points in a supporting device; of these support points two are located in the front field of the section and two in the rear field of the section, in each case at the side of the fuselage section. The support points can be traversed relative to one another in the longitudinal and transverse directions, so that an alteration of the orientation of the support points relative to one another is possible. The support points are in each case formed from a bearing head unit and a bearing head reception unit. The bearing head unit is, for example, a spherical head, and is releasably attached to the fuselage sections at the side. The bearing head reception unit has, for example, a spherical socket to receive the spherical head, and is arranged via a cross table on a bearing support that can be traversed in the height direction.
The object of the invention is to create a method for purposes of supporting and aligning a component supported in a desired orientation at a plurality of support points in a supporting device. In addition the object of the invention is to create a supporting device for purposes of supporting and aligning a component supported in a desired orientation at a plurality of support points in a supporting device.
In an inventive method for purposes of supporting and aligning a component supported in a desired orientation at a plurality of support points in a supporting device, an elastic deformation of at least one deformation zone of the supporting device is registered, and from a certain deviation from a desired value the at least one deformation zone is traversed relative to at least one support point orthogonally to the support plane of the component.
The inventive method allows an optimal alignment of the support points relative to one another at least orthogonally to the support plane, and thus an optimum mounting of the component in its support plane. In accordance with the invention the loading introduced by the component into the respective support point is individually registered, and if this exceeds a tolerance limit an orientation correction is undertaken. In particular a supporting force of the respective support point is determined from the respective elastic deformation. The supporting force allows a statement to be made concerning the positioning of the component in the supporting device in the support plane. With the aid of the individual supporting forces stresses can be detected in the component. In the case in which the component is mounted horizontally the component can be displaced in its horizontal support plane by a displacement of the support points relative to one another in the height direction of the supporting device, as a result of which supporting forces are individually increased or reduced. As soon as the calculated supporting force or forces are located within a certain deviation from a desired value, the component is located in a stress-free and torsion-free desired orientation, as required for assembly.
An inventive device for purposes of supporting and aligning a component in a desired orientation has at least two bearing supports, at least two bearing head units and at least two bearing head reception units to form at least two support points, whereby either the bearing head units or the bearing head reception units are arranged on the bearing supports. In accordance with the invention the device has at least one deformation zone, which can be elastically deformed in the course of active engagement of one of the bearing head units with one of the bearing head reception units. Moreover the device inventively has a measurement device for purposes of registering and evaluating an elastic deformation of the at least one deformation zone, and also at least one actuator for purposes of traversing the support points relative to one another orthogonally to the support plane of the component.
Such a supporting device allows the execution of the inventive method and thus the positioning of a component in its desired orientation. If, for example, the component is to be aligned in a desired horizontal orientation, the actuators allow traversing of the support points relative to one another in the vertical direction, i.e. in the height direction, of the supporting device.
The at least one deformation zone is preferably a section of the body of the bearing head reception unit. The deformation zone can be a separate section that is introduced into the bearing head unit at a subsequent point in time. However, it is preferable if the deformation zone is integrally designed into the bearing head reception unit in the form of a local reduction in cross-section. As a result of the integral reduction in cross-section the maximum external dimensions of the bearing head reception unit are not altered, so that a bearing head reception unit modified in this manner has, for example, the same height as a conventional bearing head reception unit.
In order to prevent the bearing head reception unit from being subjected to torsion in its deformation zone as a result of loading introduced by the component, which could falsify the measurements registered, the deformation zone is preferably orientated concentrically, i.e. coaxially, with the mounting axis. As a result of the concentricity the deformation zone is symmetrically loaded and is thus deformed free of any torsion.
In a preferred example of embodiment the at least one deformation zone has a radially outboard spring section, which is supported on a deformation-resistant side wall of the bearing head reception unit, and a radially inboard measurement section, which extends from the spring section and between which is clamped a measurement sensor of a measurement device. Such an example of embodiment is robust, can be manufactured easily and adjusted precisely.
The measurement sensor is, for example, a thin film measurement sensor, a thick film measurement sensor, or a piezoelement. Such sensors are very precise and very compact. They have small dimensions, so that the build height of the bearing head reception unit in question is not altered by the integration of the measurement sensor into the latter. In particular the measurement sensor is a thin film measurement sensor or a thick film measurement sensor, since these have high long-term stability and after an initial calibration do not have to be recalibrated. Moreover, a thin film measurement sensor typically has a high dynamic loading capacity and is very robust. Furthermore, a thin film measurement sensor or a thick film measurement sensor is in principle more sensitive than a piezoelement, so that even the smallest elastic deformations of the deformation zone can be registered. In the event of an elastic deformation of the deformation zone the measurement sensor experiences in each case an alteration in length, which corresponds to a compressive or tensile loading applied by the component onto the support point. Corresponding to the loading registered the support points can then be traversed relative to one another.
The bearing head unit can have a cylindrical section for purposes of accommodating a bearing head reception element, which extends in the direction of the mounting axis of the measurement section and is encompassed by the spring section. By this means the cylindrical section runs coaxially with the mounting axis and enables a symmetrical introduction of loading into the bearing head reception unit.
For purposes of avoiding alterations in orientation of the bearing head reception element relative to the cylindrical section in the transverse direction and in the longitudinal direction, the said bearing head reception element is preferably secured in the radial direction on the cylindrical section.
In a preferred example of of embodiment the bearing head reception element is a spherical socket and the bearing head unit is a spherical head. Such a spherical joint is very robust and enables a reliable mounting, since it enables a self-centering of the spherical head in the spherical socket. Moreover the loading is transferred over a large area and not at a point.
An actuator and also an elastic deformation zone and a measurement sensor are preferably assigned to each support point. By this means the position of each support point can be altered individually, as a result of which the greatest possible flexibility is achieved with regard to possible corrections in orientation.
Other advantageous examples of embodiment of the invention are the subject of further subsidiary claims.
In what follows preferred examples of embodiment of the invention are elucidated in more detail with the aid of schematic representations. Here:
The support points 1 are formed from a bearing head unit 4 and from a bearing head reception unit 6.
The bearing head unit 4 has a spherical head, which is arranged via an arm, not shown, on a retaining plate that can be attached to the fuselage section.
The bearing head reception unit 6 serves to accommodate the spherical head. The bearing head reception unit 6 is arranged on a cross table 8, the head of which is attached to a bearing support 10. The cross table 8 allows a displacement of the support point 1 in the longitudinal direction x and the transverse direction y. For this purpose it has in each case two dovetail-type pairs of rail guides 12, 14, of which the one pair 12 extends in the longitudinal direction x and the other pair 14 in the transverse direction y (
Moreover the supporting device 2 has a measurement device for purposes of registering and evaluating a necessary supporting force applied by each support point 1. A measurement device has a measurement sensor 16 shown in
Furthermore the supporting device 2 has a control device for purposes of automatic activation of at least the one actuator on the basis of the evaluated supporting force. The measurement device and the control device are preferably combined into one measurement and control device.
As shown in
The housing body 18 serves for the attachment of the bearing head unit 4 to the cross table 8 and the support of the bearing head reception element 20. It is a cuboid-shaped hollow body with a cylindrical wall 22 extending in the height direction z. The bearing head reception element 20 has a spherical socket 24 for purposes of accommodating the spherical head and is supported on the cylindrical wall 22.
As shown in the sectional view A-A in
Moreover the housing body 18 has a deformation zone 36. The deformation zone 36 extends approximately between the side wall 26 and the cylindrical wall 22. It is an integral housing wall and has a spring section 38 and also a measurement section 40. Under load the spring section 38 is subjected to an elastic deformation. It extends from the side wall 26 to the mounting axis L and encompasses the latter concentrically, i.e., coaxially. For purposes of enabling the elastic deformation, i.e. a spring action, the spring section 38 is reduced in cross-section in comparison to the side wall 26. In particular an annular taper in cross-section concentric with the mounting axis L is introduced into an inner surface 42 of the spring section 38 facing towards the base wall 28. An outer surface 44 opposite the inner surface 42 is of planar design, but can also be provided with tapers in cross-section for purposes of adjusting the spring action.
The measurement section 40 serves to position the measurement sensor 16, i.e., to transfer the elastic deformation of the spring section 28 onto the measurement sensor 16. It extends from the spring section 38 to the longitudinal axis L and encompasses the latter concentrically. Thus it is designed as a radially inboard collar of the spring section 38. It has an inner peripheral body edge 46, which is formed by the inner surface 42 and a peripheral inclined surface 48 extending radially outwards.
The cylindrical wall 22 of the housing body 18 is arranged in the region of transition from the spring section 38 to the measurement section 40 and runs coaxially with the longitudinal axis L. It is relatively thin-walled and has an annular support face 50 facing away from the base wall 28. Moreover the cylindrical wall 22 has an external thread 52 for purposes of securing the bearing head reception element 20 to the housing body 18.
The bearing head reception element 20 has a spherical socket 24, an axial stiffening projection 54 and an axial securing projection 56. The stiffening projection 54 serves to stiffen the bearing head reception element 20 under load and thus to stabilise the shape of the spherical socket 24. It is arranged on the rear face of the spherical socket 54 and in the assembled state extends coaxially with the longitudinal axis L.
The securing projection 56 serves to secure the bearing head reception element 20 to the housing body 18. It is arranged radially outboard of the stiffening projection 54 on the rear face of the spherical socket 24 and encompasses the latter. It is spaced apart from the stiffening projection 54 in the radial direction by an annular space 58. Compared with the stiffening projection 54 it is shorter axially and has a corresponding internal thread 60 for a releasable active engagement in a form fit with the external thread 52 of the cylindrical wall 22 over the whole of its axial length.
The annular space 58 is open on one side and is bounded via a seating face 62 at the rear of the spherical socket 54. In the assembled state shown the cylindrical wall 22 is immersed in the annular space 58, whereby the bearing head reception element 20 is supported via its seating face 62 on the annular support face 50 of the cylindrical wall 22. The threads 52, 60 are located in mutual active engagement.
The measurement sensor 16 is clamped centrally between the body edge 46 and registers an elastic deformation of the spring section 38. It is a strain gauge, which registers and amplifies the elastic deformations, i.e., the compressive and tensile stresses acting on the spring section 38, under load. For this purpose the measurement sensor 16 has an electrical resistance that alters in the event of strain. It is preferably a thick film sensor or a thin film sensor. The elastic deformation of the spring section 38 is converted via the measurement sensor 16 into an electrical voltage alteration. The electrical voltage alteration is then converted into a supporting force currently applied to the bearing head reception unit 6 and thus to the bearing support 10.
In what follows an exemplary method is explained for purposes of mounting a fuselage section in a horizontal support plane in an inventive supporting device 2. The supporting device 2 has four support points 1 and thus four bearing supports 10, to which in each case a bearing head reception unit 6 and a bearing head unit 4 are assigned. Each bearing head reception unit 6 has a spring section 38 with a measurement sensor 16, whose elastic deformations under load are accommodated by the fuselage section by means of the measurement sensor 16.
For purposes of horizontal mounting of the fuselage section the bearing head units 4 are attached to the fuselage section in the front and rear lateral regions. For this purpose the fuselage section is provided with corresponding lateral seatings. Then the mounting reception units 6 are aligned in a manner corresponding to the positioning of the bearing head units 4 on the fuselage section relative to one another in the longitudinal direction x and the transverse direction y. After that the fuselage section is laid down via the bearing head units 4 in the mounting reception units 6. The respective elastic deformation of the four spring sections 38 is registered and evaluated via the measurement sensors 16 of the measurement and control device. If the supporting force calculated in each case per support point 1 from the elastic deformation deviates from a desired value an orientation correction is made. Here “deviation” can signify both a supporting force that is too small and also a supporting force that is too large. For this purpose at least one of the actuators is activated via the measurement and control device and the positions of the support points 1 in the height direction z relative to one another are altered until a desired supporting force is applied by each bearing head reception unit 1. The fuselage section is now located in its desired horizontal orientation and is free of undesirable mounting stresses. In other words by means of the traversing of the support points 1 relative to one another orthogonally to the support plane, that is to say, in the example of embodiment shown, by means of a relative traversing of the support points 1 in the height direction z, i.e., in the direction of the mounting axes L relative to one another, the respective supporting force of the support points 1 is altered. After achievement of a desired elastic deformation, i.e., a desired measured value, the relative movement in the height direction z is complete. The fuselage section is now located in an optimally-aligned desired orientation.
Needless to say the supporting device can also be used for vertical or inclined mounting and alignment of a component.
Disclosed is a method for the mounting and alignment of a component supported in a supporting device at a plurality of support points in a desired orientation, wherein an elastic deformation of at least one deformation zone of the supporting device is registered, and from a certain deviation from a desired value of the at least one deformation zone is traversed orthogonally relative to at least one support point; also disclosed is a supporting device for purposes of executing such a method, which has at least one elastically deformable deformation zone, a measurement device for purposes of registering and evaluating the at least one elastic deformation, and at least one actuator for purposes of traversing the support points orthogonally relative to one another.
As is apparent from the foregoing specification, the invention is susceptible of being embodied with various alterations and modifications which may differ particularly from those that have been described in the preceding specification and description. It should be understood that I wish to embody within the scope of the patent warranted hereon all such modifications as reasonably and properly come within the scope of my contribution to the art.
1 Support point
2 Supporting device
4 Bearing head unit
6 Bearing head reception unit
8 Cross table
10 Bearing support
12 Guide rail pair
14 Guide rail pair
16 Measurement sensor
18 Base body
20 Bearing head reception element
22 Cylindrical wall
24 Spherical socket
26 Side wall
28 Base wall
30 Opening
32 Port
34 Plug element
36 Deformation zone
38 Spring section
40 Measurement section
42 Inner surface
44 Outer surface
46 Body edge
48 Inclined surface
50 Annular support face
52 External thread
54 Stiffening projection
56 Securing projection
58 Annular space
60 Internal thread
62 Seating face
L Mounting axis
x Longitudinal direction
y Transverse direction
Z Height direction
| Number | Date | Country | Kind |
|---|---|---|---|
| 10 2012 209 320.6 | Jun 2012 | DE | national |
This application claims the benefit of the U.S. Provisional Application No. 61/654,117, filed on Jun. 1, 2012, and of the German patent application No. 10 2012 209 320.6 filed on Jun. 1, 2012, the entire disclosures of which are incorporated herein by way of reference.
| Number | Date | Country | |
|---|---|---|---|
| 61654117 | Jun 2012 | US |
