EP0713947A1 - Dispositif pour la manoeuvre de rotation sur la commande de mise en action d'une fenêtre, d'une porte ou similaire - Google Patents

Dispositif pour la manoeuvre de rotation sur la commande de mise en action d'une fenêtre, d'une porte ou similaire Download PDF

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Publication number
EP0713947A1
EP0713947A1 EP95115114A EP95115114A EP0713947A1 EP 0713947 A1 EP0713947 A1 EP 0713947A1 EP 95115114 A EP95115114 A EP 95115114A EP 95115114 A EP95115114 A EP 95115114A EP 0713947 A1 EP0713947 A1 EP 0713947A1
Authority
EP
European Patent Office
Prior art keywords
rotary
bush
guide
bushing
guide bush
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP95115114A
Other languages
German (de)
English (en)
Other versions
EP0713947B1 (fr
Inventor
Siegfried Müllerbader
Erwin Röder
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Roto Frank AG
Original Assignee
Roto Frank AG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Roto Frank AG filed Critical Roto Frank AG
Publication of EP0713947A1 publication Critical patent/EP0713947A1/fr
Application granted granted Critical
Publication of EP0713947B1 publication Critical patent/EP0713947B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05C—BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS
    • E05C9/00—Arrangements of simultaneously actuated bolts or other securing devices at well-separated positions on the same wing
    • E05C9/02—Arrangements of simultaneously actuated bolts or other securing devices at well-separated positions on the same wing with one sliding bar for fastening when moved in one direction and unfastening when moved in opposite direction; with two sliding bars moved in the same direction when fastening or unfastening
    • E05C9/021—Arrangements of simultaneously actuated bolts or other securing devices at well-separated positions on the same wing with one sliding bar for fastening when moved in one direction and unfastening when moved in opposite direction; with two sliding bars moved in the same direction when fastening or unfastening with rack and pinion mechanism
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B3/00—Fastening knobs or handles to lock or latch parts
    • E05B3/08—Fastening the spindle to the follower

Definitions

  • the invention relates to a rotary actuating device on a manual transmission of a window, a door or the like.
  • an actuating shaft that can be connected by a recess on a casement to a drive element of the manual transmission, which in the installed position passes through a guide bush held in the recess of the casement and on which on the side of the guide bush facing the drive element, a rotary latch element of a rotary latch device effective in the direction of rotation of the actuating shaft is held.
  • the various switching positions of the manual transmission for example the readiness to tilt and / or the readiness to turn, are marked so that the operator can feel them by means of the rotary detent device.
  • the drive element on which the actuation shaft is to be fixed, is arranged in a gear housing inserted into the relevant frame spar from the rebate side of the casement.
  • a bore extending up to the gear housing is first made from the inside of the wing spar.
  • a guide bush bearing against the cylindrical bore wall is inserted into this bore.
  • the actuating shaft with the rotary locking element preassembled thereon is inserted through the guide bushing and connected to the drive element.
  • a manual control handle is attached to the end of the control shaft facing away from the drive element.
  • a guide bushing which has a radial outer collar projecting beyond the bore of the wing spar, by means of which it is supported on the wing spar from the outside in the installed position, then the guide bushing is screwed to the wing frame on its outer collar in a further assembly step. In this way, the guide bush is fixed in the direction of rotation of the actuating shaft of the rotary actuating device.
  • the invention is based on the object of further developing a rotary actuating device in such a way that its assembly is simplified.
  • the assembly consisting of the actuating shaft, rotary catch element, guide bush and, if applicable, manual actuating handle can be inserted with a handle into the bore provided for this purpose on the relevant spar of the casement and fixed in the installed position.
  • the radial projection of the rotary locking element relative to the inner diameter of the guide bushing can be over the entire Extend the outer circumference of the rotary locking element.
  • two tab-like projections acting as stops for the guide bushing can also be provided.
  • At least one radially projecting anti-rotation lock is provided, by means of which the guide bush is supported in the installed position on the inner wall of the recess of the sash frame.
  • the anti-rotation attachment is used to fix the guide bush in the direction of rotation of the actuating shaft.
  • the anti-rotation attachment digs when the guide bush is inserted into the recess provided for this purpose in the inner wall.
  • the guide bush is automatically fixed in the direction of rotation of the actuating shaft.
  • an anti-rotation attachment made of a relatively soft material can be provided, which plastically deforms when the guide bushing is inserted into the recess in the casement and thereby causes a press fit of the guide bush in the interior of the recess in the casement. In any case, due to the described design of the guide bush, additional assembly-related measures for securing the guide bush against rotation are unnecessary.
  • the guide bush has at least one axial stop radially projecting beyond the recess of the sash frame, then in a further expedient embodiment of the invention for securing the guide bush against rotation, at least one anti-rotation pin projecting above the axial stop on the side facing the sash frame is held pre-assembled on the axial stop is.
  • the anti-rotation pin automatically penetrates into the frame spar at the edge of the recess and in this way secures the guide bush against unintentional rotation in the circumferential direction.
  • a preferred embodiment of the rotary actuation device in which the guide bush has at least one axial stop projecting radially beyond the recess of the casement, is characterized in that the guide bush is guided on the actuating shaft so as to be displaceable in the axial direction and is resiliently pressurized in the axial direction on the side facing away from the rotary locking element
  • Such rotary actuators use, for example, a guide bush with a stepped outer circumference.
  • the socket section with the smaller diameter protrudes into the recess or bore on the casement in the installed position; the socket section with the larger diameter protrudes outward beyond the interior of the wing spar in question and forms a ring overlapping with the neck bearing of the manual operating handle mounted on the operating shaft.
  • the transition region which runs essentially perpendicular to the longitudinal axis of the guide bush between the bushing section of smaller diameter and the bushing section of larger diameter comes to rest along the bore intended for receiving the guide bush as an axial stop on the wing spar. If the guide bush is guided on the actuating shaft so as to be displaceable in the axial direction and resiliently pressurized in the axial direction on the side facing away from the rotary latching element, then there is always automatically a tight fit of the contact surface running at an angle to the longitudinal axis of the guide bush, regardless of the depth of the bore Inside of the wing spar in question. Without additional installation measures, an appealing appearance of the visible parts of the rotary control device can be ensured even with varying drilling depths. After the bores are introduced from the inside of the room through the flap of the casement and the drilling depth accordingly depends on the thickness of the casement overturn, changes in the thickness of the flap can be compensated for using rotary actuation devices according to the invention.
  • a helical spring penetrated centrally by the actuating shaft is provided for the resilient pressurization of the guide bush.
  • the coil spring can also be pre-assembled on the actuating shaft before final assembly.
  • a further preferred embodiment of the rotary actuation device in which the rotary locking element is designed as a rotary locking bush with a stepped outer diameter, is characterized in that the outer diameter of the rotary locking bush on the side facing the drive element essentially corresponds to the outer diameter of the guide bushing and on the side facing the guide bushing essentially corresponds to the inner diameter of the guide bushing, the rotary locking bushing on the side facing the guide bushing being guided telescopically therein is.
  • the final assembly of the rotary actuation device requires an exact guidance of the rotary lock bushing and the guide bushing and thus an exact guidance of the whole of the actuating shaft and, if applicable, the manual control handle comprehensive unit in the bore of the wing spar guaranteed. Accordingly, tilting of the rotary locking bushing and the guide bushing inside the bore is avoided and the actuating shaft is displaced with a directed movement in the direction of the drive element.
  • the rotary lock bushing Since the rotary lock bushing does not have to be pushed through the interior of the guide bushing during assembly of the rotary actuating device, the rotary lock bushing can be designed with a relatively large diameter, namely with the diameter of the section of the guide bushing arranged inside the bore. If the latching members of the rotary latching bushing are now arranged on the end face facing the drive element, the distance between diametrically opposite latching members can also be chosen to be relatively large due to the relatively large diameter of the rotary latching bushing. The locking properties of the rotary locking device are hereby positively influenced.
  • a rotary actuation device with a manual actuation handle, which is seated on a handle neck on the end of the actuation shaft facing away from the drive element
  • the interaction of the guide bushing and the guide shoulder stabilizes the structural unit consisting of the actuating shaft, rotary locking bushing, guide bushing and manual operating handle when inserted into the bore of the wing spar in question, in particular in the transverse direction of the actuating shaft. Since the individual parts of the assembly are guided against each other, assembly-preventing canting is excluded from the outset.
  • a particularly effective mutual guidance of the manual control handle and guide bushing is achieved in the case of a further embodiment of the rotary control device according to the invention in that the guide projection is designed as a neck bearing bushing which concentrically surrounds the actuating shaft with the guide bushing and is guided telescopically in the latter.
  • FIG. 1 and 2 show a rotary actuation device for a window sash, which has a handle unit 1 and a drive element in the form of a gear pinion 2 as essential components.
  • the gear pinion 2 is rotatably mounted in the interior of a gear housing 3 and is located with its external toothing in engagement with a rack-like counter-toothing of a drive rod 4.
  • the window sash in the illustrated case a window sash with a wooden frame, can be in known manner in its various positions.
  • a central receptacle 5 provided on the gear pinion 2 has a square cross section.
  • the entire gear housing 3 is inserted from the folded side of a vertical wing spar 6 into this immediately adjacent to a wing flap 7 and connected to the wing spar 6 via a faceplate 29.
  • the gear housing 3 protrudes into a recess made from the inside of the wing spar 6 through the wing flap 7 in the form of a receiving bore 22.
  • the handle unit 1 comprises a manual control handle 8 which is attached to a handle neck 9 on an operating shaft 10 with a square cross-section and is axially secured in the attached position by a press fit.
  • a rotationally fixed connection with the manual actuating handle 8 is established by positive locking between the actuating shaft 10 and a receptacle 11, likewise having a square cross section, in the interior of the handle neck 9.
  • a rotary locking element in the form of a rotary locking bush 12 and a guide bush 13 are arranged concentrically therewith. From the final assembly, the rotary locking bush 12 is supported with its end face facing the free end of the actuating shaft 10 on a locking bolt 15 which can be displaced in the radial direction of the actuating shaft 10.
  • the locking bolt 15 is in the FIGS. 1 and 2 biased position.
  • the locking bushing 12 is acted upon by a locking spring 17. This is supported in the interior of a neck bearing bush 14.
  • a helical spring serving as a compensating spring 18 is arranged between the handle neck 9 and the guide bush 13.
  • the rotary locking bush 12 On its end face facing the gear pinion 2, the rotary locking bush 12 has locking projections 23 projecting in the axial direction. In the final assembly position of the handle unit 1, these interact with corresponding latching receptacles 24 which are provided on the outer wall of the gear housing 3 facing the handle unit 1.
  • Both the rotary locking bush 12 and the guide bush 13 have a stepped outer diameter.
  • the reduced diameter section of the guide bush 13 is constructed in two layers.
  • An outer ring 20 is in fact clamped onto an inner ring 19.
  • the outer ring 20 is used only in connection with window sashes, the sash frame of which is made of wood.
  • window sashes the sash frame of which is made of wood.
  • the hole on the wing spar in question which is intended to accommodate the handle unit, can be proportionate without impairing the spar strength large diameter are drilled. In the case of plastic windows, however, the diameter of the spar bore must be kept as small as possible for reasons of strength.
  • the outer diameter of the rotary locking bushing section with a larger diameter corresponds to the outer diameter of the inner ring 19 on the guide bushing 13.
  • the outer diameter of the reduced-diameter section of the rotary locking bushing 12 and the outer diameter of the neck bearing bushing 14 correspond to the inner diameter of the inner ring 19.
  • the handle unit 1 is inserted as a previously preassembled structural unit into the receiving bore 22 provided for this purpose on the wing spar 6.
  • the locking bolt 15 runs with its beveled front edge onto the facing edge of the receptacle 5 on the gear pinion 2.
  • the locking bolt 15 is moved downward against the action of the locking spring 16 in FIG. 1 until it lies within the contour of the actuating shaft 10.
  • the rotary locking bush 12 comes to rest with its end face facing the interior of the bore on the facing end face of the transmission housing 3.
  • the inner ring 19 slides telescopically over the section of reduced diameter Rotary locking bush 12; the neck bearing bush 14 is also guided telescopically inside the inner ring 19.
  • the locking bolt 15 has passed the receptacle 5 on the gear pinion 2 in the direction of insertion, so it moves under the action of the locking spring 16 in its in the FIGS. 1 and 2 shown starting position, grips the gear pinion 2 radially on its side facing away from the manual operating handle 8 and thus secures the handle unit 1 in the axial direction against being pulled out.
  • the gear pinion 2 is acted upon by the locking bushing 12 on the side facing away from the locking bolt 15 under the action of the locking spring 17.
  • the locking projections 23 provided on the end face of the rotary locking bush 12 facing the gear pinion 2 are in engagement with the locking receptacles 24 on the opposite wall of the gear housing 3 and together with these form the rotary locking device.
  • the guide bush 13 With its section with reduced diameter, lies in the interior of the receiving bore 22 and is supported on the inside of the wing 6 by the radial annular surface 21 acting as an axial stop.
  • the guide bush 13 is acted upon by the compensating spring 18, which brings about a tight contact of the radial annular surface 21 on the wing spar 6.
  • a residual gap between the radial annular surface 21 and the wing spar 6 which affects the appearance of the window construction is thereby avoided.
  • the compensating spring 18 ensures tight contact of the radial annular surface 21 of the guide bush 13 on the outside of the respective wing spar, without the exact guidance of the individual parts of the handle unit 1 being impaired.
  • the rotary actuation device according to FIGS. 3 and 4 differs from the rotary actuation device shown in FIGS. 1 and 2 only in the design of the guide bushing.
  • a handle unit 1a is inserted into a receiving bore 22a of a wing spar 6a provided for this purpose and is positively connected to a gear pinion 2a via an actuating shaft 10a.
  • a guide bush 13a is supported on the wing spar 6a with a radial annular surface 21a, lying on the outside. In this case, metal anti-rotation pins 25 of the guide bush 13a engage in the wing spar 6a.
  • the anti-rotation pins 25 are injected into the guide bushing 13a, which is designed as a plastic injection-molded part, and protrude beyond their radial annular surface 21a with their pointed ends.
  • the anti-rotation pins 25 penetrate with their pointed ends into the wing spar 6a when the annular surface 21a is pressed against the inside of the wing spar 6a.
  • the anti-rotation pins 25 in the final assembly position create a connection between the wing spar 6a and the guide bushing 13a that is rotationally fixed in the direction of rotation of the actuating shaft 10a.
  • FIG. 5 shows a rotary actuator on a plastic window.
  • a handle unit 1b is fixed to a gear pinion 2b by a receiving bore 22b of a wing spar 6b made of plastic.
  • a guide bush 13b is supported on the walls of the receiving bore 22b via an inner ring 19b. Since the receiving bore 22b, as is customary on plastic windows, has been drilled with a relatively small diameter, an outer ring customary in wooden windows is dispensed with on the guide bushing 13b.
  • anti-rotation pins 25b in the final assembly position protrude the guide bush 13b on a radial ring surface 21b with their pointed ends, with which they engage in the wing spar 6b.
  • the anti-rotation pins 25b establish a connection between the guide bush 13b and the wing spar 6b which is rotationally fixed in the direction of rotation of an actuating shaft 10b.
  • the rotary actuation device according to FIGS. 5 and 6 corresponds to the rotary actuation devices described above.
  • FIG. 7 shows a rotary actuating device for wooden windows with a handle unit 1c, on which a manual actuating handle 8c is connected to an actuating shaft 10c via a clamping screw 26.
  • the handle unit 1c is fixed in the manner described above through a receiving bore 22c of a wing spar 6c on a gear pinion 2c.
  • the releasability of the connection between the manual operating handle 8c and the operating shaft 10c made by means of the clamping screw 26 allows the manual operating handle 8c to be moved in the axial direction of the operating shaft 10c.
  • Such a transfer of the manual control handle 8c also makes it possible to adapt the handle unit 1c to changing depths of the receiving bore 22c.
  • the manual control handle 8c in FIG. 7 can be moved to the left after loosening the clamping screw 26, so that the projection of the actuating shaft 10c extends relative to the manual actuating handle 8c and a connection between the gear pinion 2c and the actuating shaft 10c can still be established.
  • FIGS. 8 and 9 show how a guide bushing 13c of the rotary actuating device shown in FIG. 7 is secured against undesired rotation in the direction of rotation of the actuating shaft 10c.
  • a plurality of anti-rotation approaches 27 are attached to an outer ring 20c of the guide bush 13c.
  • the anti-rotation approaches 27 run on the cylindrical Outer surface of the outer ring 20c like strips in the axial direction thereof and have a substantially triangular cross section.
  • the anti-rotation protrusions 27 of the outer ring 20c projecting radially beyond the diameter of the receiving bore 22c dig into the inner wall of the receiving bore 22c.
  • the guide bush 13c is rotatably connected to the wing spar 6c on its outer ring 20c in the direction of rotation of the actuating shaft 10c.
  • grooves 28 are provided on the inner wall of the outer ring 20c facing the inner ring 19c, in which grooves 28 are provided, in which anti-rotation attachments 27 'arranged on the outer wall of the inner ring 19c are supported .
  • the anti-rotation lugs 27 ' correspond in their design and their course to the anti-rotation lugs 27. If the handle unit 1c shown in FIG. 7 on a wooden wing spar 6c is to be mounted on a wing spar made of plastic, on which the receiving bore for the guide bush has a relatively small diameter, the outer ring 20c can be pulled off the inner ring 19c. The guide bush 13c can then be inserted on the inner ring 19c in the receiving bore of the plastic wing spar in question.
  • the anti-rotation lugs 27 ' which protrude radially beyond the receiving bore, are plastically deformed and thereby cause the guide bush to be clamped in the receiving bore. These Clamping connection is also effective in the direction of rotation of the actuating shaft.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Power-Operated Mechanisms For Wings (AREA)
  • Wing Frames And Configurations (AREA)
  • Window Of Vehicle (AREA)
EP95115114A 1994-11-24 1995-09-26 Dispositif pour la manoeuvre de rotation sur la commande de mise en action d'une fenêtre, d'une porte ou similaire Expired - Lifetime EP0713947B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE9418857U DE9418857U1 (de) 1994-11-24 1994-11-24 Drehbetätigungseinrichtung an einem Schaltgetriebe eines Fensters, einer Tür o.dgl.
DE9418857U 1994-11-24

Publications (2)

Publication Number Publication Date
EP0713947A1 true EP0713947A1 (fr) 1996-05-29
EP0713947B1 EP0713947B1 (fr) 1999-01-27

Family

ID=6916565

Family Applications (1)

Application Number Title Priority Date Filing Date
EP95115114A Expired - Lifetime EP0713947B1 (fr) 1994-11-24 1995-09-26 Dispositif pour la manoeuvre de rotation sur la commande de mise en action d'une fenêtre, d'une porte ou similaire

Country Status (3)

Country Link
EP (1) EP0713947B1 (fr)
AT (1) ATE176294T1 (fr)
DE (2) DE9418857U1 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1528198A1 (fr) * 2003-10-28 2005-05-04 Viessmann Kältetechnik AG Poignée d'ouverture et de fermeture pour les portes d'en particulier chambres de préservation, frigorifiques et de refroidisments
EP1659239A1 (fr) * 2004-10-28 2006-05-24 Viessmann Kältetechnik AG Poignée d'ouverture et de fermeture pour des portes, en particulier pour chambres de préservation, frigorifiques et de refroidissements

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE29513664U1 (de) * 1995-08-25 1997-01-16 Bks Gmbh Antriebsverbindung
FR2740496B1 (fr) * 1995-10-26 1998-01-02 Alcan France Poignee demontable pour porte ou fenetre notamment en menuiserie metallique
DE19541214C2 (de) * 1995-11-04 2000-12-14 Roto Frank Ag Drehbetätigungseinrichtung
DE19601119C2 (de) * 1996-01-13 1997-11-20 Roto Frank Ag Drehbetätigungseinrichtung mit Blendhülse
DE202007000497U1 (de) † 2007-01-08 2007-03-15 Siegenia-Aubi Kg Verriegelungsbeschlag und Beschlagteilesatz
DE102014015381A1 (de) * 2014-10-17 2016-05-04 Roto Frank Ag Griffanordnung für ein Fenster oder dergleichen sowie Fenster oder dergleichen mit Griffanordnung
DE102015117330A1 (de) * 2015-10-12 2017-04-13 Maco Technologie Gmbh Koppelstift
DE202019002173U1 (de) 2019-05-20 2019-06-28 Siegenia-Aubi Kg Fenster oder Türbeschlag

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT221981B (de) * 1959-10-29 1962-06-25 Wilhelm Frank Getriebe für Beschläge an Fenstern, Türen od. dgl.
DE4125507A1 (de) * 1990-08-31 1992-03-05 Roto Frank Ag Beschlag fuer ein fenster, eine tuer o. dgl.

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT221981B (de) * 1959-10-29 1962-06-25 Wilhelm Frank Getriebe für Beschläge an Fenstern, Türen od. dgl.
DE4125507A1 (de) * 1990-08-31 1992-03-05 Roto Frank Ag Beschlag fuer ein fenster, eine tuer o. dgl.

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1528198A1 (fr) * 2003-10-28 2005-05-04 Viessmann Kältetechnik AG Poignée d'ouverture et de fermeture pour les portes d'en particulier chambres de préservation, frigorifiques et de refroidisments
EP1659239A1 (fr) * 2004-10-28 2006-05-24 Viessmann Kältetechnik AG Poignée d'ouverture et de fermeture pour des portes, en particulier pour chambres de préservation, frigorifiques et de refroidissements

Also Published As

Publication number Publication date
DE59504972D1 (de) 1999-03-11
DE9418857U1 (de) 1995-01-26
EP0713947B1 (fr) 1999-01-27
ATE176294T1 (de) 1999-02-15

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