Centring arrangement for a component carrier
09604734 ยท 2017-03-28
Assignee
Inventors
Cpc classification
B23Q1/25
PERFORMING OPERATIONS; TRANSPORTING
Y10T29/53687
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
Y10T29/53978
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
Y10T29/53983
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
Y10T29/49998
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
Y10T29/5177
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B64F5/10
PERFORMING OPERATIONS; TRANSPORTING
Y10T29/53091
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
Y10T29/53961
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
International classification
B64F5/00
PERFORMING OPERATIONS; TRANSPORTING
B23Q1/25
PERFORMING OPERATIONS; TRANSPORTING
Abstract
The invention relates to a centring arrangement for a component carrier, in particular for a mounting frame for structural aircraft components, having a centring pin, a centring receptacle for the centring pin, and a rotary drive for rotating the centring pin about a longitudinal axis of the centring pin, so that the centring pin can be brought into centring engagement with the centring receptacle as a result of the rotation. The invention further relates to a method for centring and locking a centring receptacle.
Claims
1. A centring arrangement for a component carrier, having a centring pin, a centring receptacle for the centring pin, and a rotary drive for rotating the centring pin about a longitudinal axis of the centring pin, so that the centring pin is brought into centring engagement with the centring receptacle as a result of contact between the centring pin and the receptacle during a rotation of the centring pin.
2. The centring arrangement according to claim 1, wherein the centring pin has a closing contour and the centring receptacle has a mating contour for establishing the centring engagement.
3. The centring arrangement according to claim 2, wherein the closing contour forms a polygon.
4. The centring arrangement according to claim 3, wherein the mating contour has inwardly projecting contact projections, wherein the number of edges of the polygon corresponds to at least the number of contact projections.
5. The centring arrangement according to claim 4, wherein the number of edges of the polygon corresponds to precisely the number of contact projections.
6. The centring arrangement according to claim 2, wherein the closing contour defines a maximum outer closing radius and the mating contour defines a minimum inner contact radius about the longitudinal axis, wherein the closing radius does not exceed the contact radius.
7. The centring arrangement according to claim 3, wherein the closing contour forms a square.
8. The centring arrangement according to claim 1, wherein the centring engagement between the centring pin and the centring receptacle is established in a centring direction, which centring direction runs radially in relation to the longitudinal axis and intersects the longitudinal axis.
9. The centring arrangement according to claim 8, wherein, in the event of centring engagement, there is a free space between the centring pin and the centring receptacle in a direction of play, wherein the direction of play runs radially in relation to the longitudinal axis and intersects the longitudinal axis.
10. The centring arrangement according to claim 9, wherein, the direction of play is perpendicular to the centring direction.
11. The centring arrangement according to claim 8, wherein the centring engagement between the centring pin and the centring receptacle is established in a further centring direction, which further centring direction runs radially in relation to the longitudinal axis and perpendicularly in relation to the centring direction and intersects the longitudinal axis.
12. The centring arrangement according to claim 1, wherein the centring arrangement has a clamping area which is arranged perpendicular to the longitudinal axis, and the centring arrangement has a locking apparatus for locking the centring receptacle with respect to a movement relative to the clamping area.
13. The centring arrangement according to claim 12, wherein the locking apparatus comprises an engagement contour on the centring pin for engaging behind the centring receptacle.
14. The centring arrangement according to claim 13, wherein the engagement contour has gripping projections which extend from the longitudinal axis in the radial direction and are designed to engage behind the contact projections when the centring pin is brought into centring engagement with the centring receptacle as a result of the rotation.
15. The centring arrangement according to claim 12, wherein the centring arrangement has a pretensioning spring which is designed to exert a force onto the centring pin in a direction which points towards the clamping area.
16. The centring arrangement according to claim 12, wherein the centring arrangement has a linear drive for moving the centring pin along the longitudinal axis.
17. The centring arrangement according to claim 1, wherein the rotary drive has a deflection arm on the centring pin, which deflection arm is arranged radially in relation to the longitudinal axis.
18. The centring arrangement according to claim 1, wherein the centring arrangement comprises a guide which is designed to orient the centring receptacle to the longitudinal axis of the centring pin.
19. A method for centring and locking a centring receptacle on a clamping area, using a centring pin, comprising: moving the centring pin through the centring receptacle, so that gripping projections of an engagement contour of the centring pin are guided through cutouts in a mating contour of the centring receptacle, rotating the centring pin about a longitudinal axis of the centring pin, as a result of which a closing contour of the centring pin is brought into centring engagement with the mating contour of the centring receptacle due to contact between the centring pin and the receptacle during the rotation, and at the same time the gripping projections engage behind the mating contour, and pushing the centring receptacle against the clamping area as a result of a movement of the centring pin.
20. The centring arrangement according to claim 1, wherein the centring arrangement has a clamping area which is arranged perpendicular to the longitudinal axis, and the centring arrangement has a locking apparatus for locking the centring receptacle with respect to a perpendicular movement relative to the clamping area.
Description
BRIEF DESCRIPTION OF THE FIGURES
(1) In the drawing, which illustrates only exemplary embodiments,
(2)
(3)
(4)
(5)
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(7)
DETAILED DESCRIPTION
(8) A component carrier 1, in particular a mounting frame 1a for structural aircraft components, having four proposed centring arrangements is illustrated in
(9) The mounting frame 1a shown is, in particular, inserted into a processing stationnot illustrated herefor structural aircraft components. The structural aircraft components which can be received by said mounting frame 1a include, in particular, tails and wings of an aircraft and also the constituent parts of said tails and wings.
(10) The proposed centring arrangement comprises a centring pin 2 and a centring receptacle 3 for the centring pin 2, the said centring pin and centring receptacle being illustrated on an enlarged scale in
(11) The centring receptacle 3 is therefore designed to receive the centring pin 2 in its opening. In this case, the centring receptacle 3 is arranged on the workpiece and therefore is associated with the workpiece and in particular with the structural aircraft component. This centring receptacle 3 may be a corresponding receptacle and opening on the workpiece itself, or else, as illustrated in
(12) Since advance, indirect or direct fastening of the centring receptacle 3 to the workpiece in this waythe details of which are not arrived at in this casecan be performed independently of the processing station both in respect of time and in respect of physical area, the time required for this purpose does not play a critical role since the utilization of the processing station is not adversely affected by said fastening operation.
(13) The proposed centring arrangement further comprises a rotary drive 4 for rotating the centring pin 2 about a longitudinal axis 5which is to be understood in a geometrical senseof the centring pin 2, so that the centring pin 2 can be brought into centring engagement with the centring receptacle 3 as a result of the rotation. In this case, the longitudinal axis 5 corresponds here to the main direction of extent of the centring pin 2, as is clear from
(14) In this case, the term engagement is initially to be understood very generally as mechanical contact between the centring pin 2 and the centring receptacle 3. This engagement is centring in as much as it leads to mechanical shifting of the centring receptacle 3, for example as a result of pushing, into a predefined and therefore centred position in at least one dimension relative to the centring pin 2, provided that the centring receptacle 3 is not already centred in this sense. This centred position can relate to the longitudinal axis 5 of the centring pin 2, so that, in the centred state, the profile of the axis of the centring receptacle 3, which axis corresponds to the longitudinal axis 5 of the centring pin 2, corresponds to the profile of the longitudinal axis 5 of the centring pin 2 in the said, at least one dimension in any case. In the event of centring in two dimensions, that is to say in terms of the area, the corresponding axis of the centring receptacle 3 would coincide with the longitudinal axis 5 in the centred position. Established centring engagement in this sense is illustrated, for example, in the
(15) The said centring engagement is produced when the centring pin 2 has been received by the centring receptacle 3 in advance. Before the said rotation, the centring pin 2 in any case has sufficient play in the centring receptacle 3 in order to execute rotation until the centring engagement is established. In connection with
(16) In this case, the centring engagement can perform such that the rotation of the centring pin 2 is not blocked by the centring receptacle 3, but rather the centring pin 2 could still rotate further, wherein centring can then be cancelled again. As shown in
(17) Accordingly, the centring pin 2 can have a closing contour 6 and for the centring receptacle 3 to have a mating contour 7a, b for establishing the centring engagement. A closing contour 6 and two alternative mating contours 7a, b are illustrated by way of example in
(18) In this case, the closing contour 6 represents the cross-sectional outline of the centring pin 2. The mating contour 7a, b is accordingly the cross-sectional outline of the centring receptacle 3.
(19) This embodiment further makes provision for the closing contour 6 to define a maximum outer closing radius 8a and for the mating contour 7 to define a minimum inner contact radius 8b about the longitudinal axis 5, wherein the closing radius 8a does not exceed the contact radius 8b. As illustrated in
(20) The closing radius 8a of the closing contour 6 in this sense identifies that radius in relation to the longitudinal axis 5 within which the closing contour 6 is completely enclosed. In other words, the closing contour 6 does not have any constituent part which is radially further away from the longitudinal axis 5 than the closing radius 8a. The contact radius 8b of the mating contour 7a, b analogously identifies that radius in relation to the same longitudinal axis 5 outside which the mating contour 7a, b is completely formed. In other words, the mating contour 7a, b does not have any constituent part which is radially closer to the longitudinal axis 5 than the contact radius 8b.
(21) Since the closing radius 8a does not exceed the contact radius 8b, it is ensured that in any case no interlocking connection between the closing contour 6 and the mating contour 7a, b can prevent the rotation of the centring pin 2 in the centring receptacle 3 for establishing the centring engagement or else can prevent further rotation of the centring pin 2. Actual collision between the centring pin 2 and the centring receptacle 3 during rotation and even catching are prevented as a result. Instead, this promotes the ability of the centring receptacle 3 to move relative to the centring pin 2 in the event of rotation of the centring pin 2, such that the desired centring is achieved.
(22) In an embodiment, the closing contour 6 can form a polygon 6a, such as a square. A polygon 6a of this kind is suitable for being moved, as a result of rotation about a rotation angle which is defined by the number of edges of the polygon 6a, from a position in which there is no centring engagement within the meaning of the proposal, to a position with centring engagement of this kind. This is facilitated, in particular, by the polygon 6a, as shown in
(23) Building on the above, in some embodiments the mating contour 7a, b can have inwardly projecting contact projections 9, wherein the number of edges of the polygon 6a corresponds at least, and in some embodiments exactly, to the number of contact projections 9. In this connection, inwardly projecting means that the contact projections 9 point radially in the direction of the longitudinal axis 5, and that sections of the mating contour 7a, b which are recessed with respect to the said radial direction and which will be discussed in greater detail below are present between the said contact projections 9. Therefore, in a refinement of this kind, it is expedient for the centring engagement between the centring pin 2 and the centring receptacle 3 to be formed by theradially outwardly pointingedges of the polygon 6a on the one hand and the inwardly projecting contact projections 9 of the mating contour 7a, b on the other hand. This substantive matter is shown, in particular, in
(24) Provision is further made for the centring engagement between the centring pin 2 and the centring receptacle 3 to be established in a centring direction 10a which runs radially in relation to the longitudinal axis 5 and intersects the longitudinal axis 5. When the centring pin 2 is rotated, the centring receptacle 3 is therefore necessarily shifted such that the centring action in this centring direction 10a begins and, after the centring engagement is established, a further relative movementapart from negligible shifts owing to manufacturing tolerancesin this centring direction 10a is prevented by this centring engagement itself. Establishing that the centring direction 10a runs radially in relation to the longitudinal axis 5 and intersects the longitudinal axis 5 could also be formulated such that the centring direction 10a is a radial direction of the longitudinal axis 5.
(25) An embodiment, makes provision for there to be a free space 11which goes beyond the space substantiated in respect of manufacturingbetween the centring pin 2 and the centring receptacle 3 in a direction 12 of play in the case of an interlocking connection, wherein the direction 12 of play runs radially in relation to the longitudinal axis 5 and intersects the longitudinal axis 5. In accordance with the above statements in respect of the centring direction 10a, this is equivalent to the observation that the direction 12 of play is also a radial direction of the longitudinal axis 5. According to an embodiment, a relative movement between the centring pin 2 and the centring receptacle 3 in the centring direction 10a is therefore prevented, but allowed, in principle, in the direction 12 of play. In this case, it may be advantageous for various reasons to define only one centring direction 10a for each centring arrangement of the component carrier 1.
(26) One variant according to this first option, in which the direction 12 of play is perpendicular to the centring direction 10a, is illustrated in
(27) A second option of an embodiment, which is illustrated by way of example in
(28) Any significant translatory relative movement between the centring pin 2 and the centring receptacle 3 in the area defined by the two centring directions 10a, b is prevented as a result of centring engagement between the centring pin 2 and the centring receptacle 3 in this way in two centring directions 10a, b which are perpendicular in relation to one another. This embodiment option is therefore available, for example, when comprehensive centring on the area which is defined by the mounting frame 1a by an individual proposed centring arrangement is desired.
(29) In order to also prevent a relative movement between the centring pin 2 and the centring receptacle 3 from the area which is defined by the two centring directions 10a, b, but primarily in the direction of the longitudinal axis 5, provision is further made for the centring arrangement to have a clamping area 13 which is arranged perpendicular to the longitudinal axis 5, and for the centring arrangement to have a locking apparatus 14 for locking the centring receptacle 3 with respect to a, such as perpendicular, movement relative to the clamping area 13. This clamping area 13 is to be understood as an area within the meaning of a surface, which area is potentially also formed only in the manner of an edge or web, the locking apparatus 14 preventing a movement of the centring receptacle 3 relative to the said clamping area, for example by a force-fitting connection. Therefore, a movement of this kind of the workpiece is therefore also indirectly prevented. In particular, the centring receptacle 3 can be locked with respect to a, such as perpendicular, movement relative to the clamping area 13 in the direction of the longitudinal axis 5. In this way, locking of the workpiece on the component carrier 1 is also achieved in addition to centring of the workpiece on the component carrier 1.
(30) A corresponding further development for this purpose makes provision for the locking apparatus 14 to comprise an engagement contour 15 on the centring pin 2 for engaging behind the centring receptacle 3. An engagement contour 15 of this kind is clearly shown in
(31) Further advantages result whenas illustrated in
(32) The mating contour 7a, b which is already provided for the centring engagement, together with its contact projections 9, which are shown in
(33) The double function can additionally also involve the use of the same rotary movement for the centring engagement and for the process of engaging behind. In this case, provision can be made for the engagement contour 15 to be designed to engage behind the contact projections 9 when the centring pin 2 is brought into centring engagement with the centring receptacle 3 as a result of the rotation. Comparing
(34) A engagement contour 15 of this kindlikewise illustrated in
(35) These components are matched to one another in a particularly suitable manner when the cutouts 17 correspond to the gripping projections 16 to such an extent that the engagement contour 15 can be moved, as a result of the rotation of the centring pin 2 about the longitudinal axis 5, to a position in relation to the mating contour 7 in which the gripping projections 16 can be aligned with the cutouts 17 and the engagement contour 15 can be can be shifted by the mating contour 7a, b. This situation is illustrated in
(36) As has already been described at the outset, the locking which is likewise established by the centring arrangement has to ensure that the workpiece which is received by the component carrier 1, that is to say a structural aircraft component for example, does not fall down from the component carrier 1. This is also intended to apply in the case of an unexpected power loss in the processing station, for example in the event of a power failure or the operation of an emergency off-switch. Against this background, provision can be made for the centring arrangement to have a pretensioning spring 18 which is designed to exert a force, and in particular pretension, onto the centring pin 2 in a direction 18a which points towards the clamping area 13 and which is identified in
(37) In the exemplary embodiments shown here, the pretensioning spring 18 is arranged such that it pushes an intermediate carrier 18b, which is connected to the centring pin 2, away from a rear face of the clamping area 13, as a result of which the centring pin 2 is pretensioned in the said direction 18a. Therefore, a force has to be applied in order to move the centring pin 2 out of the locked situation, so that, in the event of a failure of all motors, locking is ensured solely by the pretensioning spring 18 if the centring pin 2 is in corresponding engagement with the centring receptacle 3.
(38) Against this background, provision can be made, for shifting the centring pin 2 as already described above, for the centring arrangement to have a linear drive 19 for moving the centring pin 2 along the longitudinal axis 5. In this case, the linear drive 19 can be arranged, in particular, at an end of the centring pin 2 which is situated opposite the engagement contour 15and therefore also the closing contour 6. In connection with the activity of the pretensioning spring 18, the linear drive 19 can be designed to move the centring pin 2 in a direction 19b which points away from the clamping area 13. In this case, it is particularly expedient for the linear drive 19 to be fitted on the same intermediate carrier 18b as the said pretensioning spring 18.
(39) Furthermore, the option of a development which utilizes the space in a mounting frame 1a in a particularly economical manner results when the rotary drive 4 has a deflection arm 20 on the centring pin 2, which deflection arm is arranged radially in relation to the longitudinal axis 5. In this way, a motor for effecting rotation in the radial direction can be arranged at a distance from the centring pin 2. This is expedient when there is little installation space in the direction of the longitudinal axis 5 of the centring pin 2. In this development, provision can also be made for the deflection arm 20 to be connected to a lifting rod 22 by means of a rotary joint 21 at a radially outer end. This is shown, in particular, in
(40) A further refinement of the proposed centring arrangement, shown in
(41) If, as illustrated in
(42) As an alternative, the proposed centring arrangement can also have a horizontal alignment on the mounting frame 1a, once again determined on the basis of the longitudinal axis 5 of the centring pin 2. In this case, the guide 26 can be designed in accordance with the illustration of
(43) A further embodiment which can be mentioned is a mounting frame 1a for structural aircraft components, as illustrated in
(44) In this case, a further development of a mounting frame 1a of this kind makes provision for the respective clamping area 13 of the centring arrangements to form part of an outer surface 30 of the frame housing 24. If, as is illustrated in
(45) A further development of the mounting frame 1a makes further provision for the mounting frame 1a to have a linear motor 23 for operating a deflection arm 20, wherein the linear motor 23 is arranged within the frame housing 24 in a lateral direction 29 of the rectangular shape. In a clamping frame 1a of this kind, centring and locking can be performed in a fully automatic manner. A lateral direction 29 of the rectangular shape is to be understood to mean any direction which corresponds to the extent of one of the four rectangle sides of the rectangular shape of the clamping frame 1a.
(46) Since the constituent parts of the proposed centring arrangement and its refinements have now been described, a corresponding proposed method for centring and locking a centring receptacle 3 using a centring pin 2 on a clamping surface 13, in particular on the clamping area 13 of a component carrier 1, will be explained with reference to
(47)
(48) The said proposed method now comprises moving the centring pin 2 through the centring receptacle 3, so that gripping projections 16 of an engagement contour 15 of the centring pin 2 are guided through cutouts 17 in a mating contour 7a, b of the centring receptacle 3. This method step takes place as a transition between the state in
(49) The proposed method comprises rotating the centring pin 2 about a longitudinal axis 5 of the centring pin 2, as a result of which a closing contour 6 of the centring pin 2 is brought into centring engagement with the mating contour 7a, b of the centring receptacle 3 and, at the same time, the gripping projections 16 engage behind the mating contour 7a, b. This method step takes place between the illustration of
(50) Finally, the proposed method comprises pushing the centring receptacle 3 against the clamping area 13 by virtue of a movement of the centring pin 2. This method step corresponds to the transition from the situation of
(51) Further embodiments of the proposed method can be found in the above-described embodiments of the proposed centring arrangement.