EP0467122A1 - Douille pour broches de ferrures ou charnières - Google Patents

Douille pour broches de ferrures ou charnières Download PDF

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Publication number
EP0467122A1
EP0467122A1 EP91110616A EP91110616A EP0467122A1 EP 0467122 A1 EP0467122 A1 EP 0467122A1 EP 91110616 A EP91110616 A EP 91110616A EP 91110616 A EP91110616 A EP 91110616A EP 0467122 A1 EP0467122 A1 EP 0467122A1
Authority
EP
European Patent Office
Prior art keywords
hinge pin
sleeve
pin bushing
inner sleeve
outer sleeve
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
EP91110616A
Other languages
German (de)
English (en)
Other versions
EP0467122B1 (fr
Inventor
Walter Dr. Hahn
Jürgen Bögel-Pötter
Karl-Hubert Jennessen
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.)
Dr Hanh GmbH and Co KG
Original Assignee
Dr Hanh GmbH and Co KG
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 Dr Hanh GmbH and Co KG filed Critical Dr Hanh GmbH and Co KG
Publication of EP0467122A1 publication Critical patent/EP0467122A1/fr
Application granted granted Critical
Publication of EP0467122B1 publication Critical patent/EP0467122B1/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
    • E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D7/00—Hinges or pivots of special construction
    • E05D7/0009—Adjustable hinges
    • E05D7/0018—Adjustable hinges at the hinge axis
    • E05D7/0045—Adjustable hinges at the hinge axis in a radial direction
    • E05D7/0054—Adjustable hinges at the hinge axis in a radial direction by means of eccentric parts
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D5/00—Construction of single parts, e.g. the parts for attachment
    • E05D5/10—Pins, sockets or sleeves; Removable pins
    • E05D5/14—Construction of sockets or sleeves

Definitions

  • the invention relates to a hinge pin bushing of the type corresponding to the preamble of claim 1.
  • Such a hinge pin bushing is known from DE-PS 3 12 832.
  • the flange ring is designed as a radial flange at the upper end of the inner sleeve.
  • the toothing of the inner sleeve is provided on a separate disk which is rotationally connected to the inner sleeve and can be displaced in relation to the latter in the axial direction until the toothing engages.
  • a rotary tool can engage the disc from below through an opening in the outer sleeve and twist it and thus the inner sleeve for the purpose of adjusting the wing in the frame.
  • the sleeves should be rotated relative to one another with the wing attached, i.e. while this rests with its weight on the flange ring integral with the inner sleeve. It has been shown that with heavy wings and poor lubrication of the flange ring, the adjustment of the inner sleeve requires very high torques, which can lead to a torsional deformation of the inner sleeve. This is because, for structural reasons, the inner sleeve has only a relatively small wall thickness, at least on the eccentric outer side.
  • the invention has for its object to provide a hinge pin bushing of the type corresponding to the preamble of claim 1 so that the adjustment of the hinge pin bushing is possible even with heavy wings without the risk of overstressing the inner sleeve.
  • the inner sleeve Due to the free rotation of the inner sleeve relative to the flange ring, the inner sleeve can be rotated in the outer sleeve without the flange ring, which is under the load of the wing, having to be rotated as well. This not only makes it easier to twist the inner sleeve, but also ensures that it is not overstressed by excessive torque.
  • the embodiment according to claim 2 is important because it allows the cooperating toothings to be attached to the two bushings and to get by with only three parts, namely the flange ring itself and the two bushings. A separate locking part such as the disc in the known embodiment is therefore not required.
  • the flange ring must be fixed in the radial direction to prevent slipping between the cooperating band parts. It is recommended that the flange ring has a cylindrical projection for this purpose, which engages in the inner bore of the outer sleeve. However, since the inner sleeve is also arranged in this inner bore, a distance corresponding to the engagement distance of the toothings between the attachment and the inner sleeve is provided in this embodiment (claim 3).
  • the toothing can be formed in the manner shown in claim 4.
  • the toothing of the outer sleeve acts as a stop when inserting the inner sleeve into the outer sleeve.
  • a locking device which holds the toothings in engagement in the operating state of the hinge pin bushing, that is to say when the adjustment has ended.
  • a necessary feature of the locking device is that it must be detachable, so that after adjustment, readjustment or readjustment can take place after a long time.
  • the locking device must not be designed so that it no longer releases the inner sleeve against the direction of engagement after locking.
  • locking device is the subject of claim 6.
  • the resilient design of the locking device enables independent engagement, but the spring property also serves to enable subsequent disengagement of the engagement and the rotation of the bushings against each other.
  • a possible embodiment of a resilient locking device comprises, according to claim 7, elastically push-away latching tongues which can be designed in detail according to claim 8.
  • the undercut on the inner sleeve can be formed by a circumferential groove in the bottom part of the same (claim 9), an important further development being that the latching tongues seated on the undercut without force leave a radial distance from the base of the groove.
  • the inner sleeve has a thick-walled and a thin-walled side due to the eccentricity. According to the embodiment according to claim 17, it can overlap on its thick-walled side the projection of the flange ring projecting into the bore of the band part up to near the top of the flange ring. As a result, the guide length of the inner sleeve is increased by the corresponding axial distance on at least one side.
  • the band pin bushing 100 consists of an outer bush 3 with a cylindrical outer peripheral surface which sits in the band sleeve bore 4 of the lower band part 2.
  • a projection 5 can be provided on the outer circumference of the outer sleeve 3, which engages in a longitudinal groove (not shown) of the band sleeve bore 4.
  • the outer sleeve 3 has a bevelled all-round projection 6, which rests on a corresponding countersinking of the band sleeve bore 4.
  • the cylindrical outer periphery of the outer sleeve 3 has an axis 7, from which the axis 8 of the bore 9 of the outer sleeve 3 deviates by the amount of the eccentricity.
  • the inner sleeve 11 is seated with its cylindrical outer circumference, the axis of which is 8.
  • the inner bore 12, which receives the hinge pin 10, is in turn eccentric to the outer circumference of the inner sleeve 11 and has an axis, the eccentricity of which corresponds to that of the outer sleeve 3 in the exemplary embodiment.
  • the inner sleeve 11 is also arranged in the setting shown in FIG. 1 so that the axis of the inner bore 12 coincides with the axis 7 of the outer periphery 4 of the outer sleeve 3.
  • the inner sleeve 11 has a bottom part 13 which has a cylindrical outer circumferential surface 14 which is coaxial with the outer circumferential surface of the inner bush 11, that is to say which has the axis 7 and which is guided in a corresponding cylindrical recess 15 at the lower end of the outer bush 3 .
  • a circumferential groove 16 is formed, the base 17 of which is a cylindrical surface with the axis 8.
  • a downwardly open hexagon recess 36 is provided in the bottom part 13 for the attack of a turning tool.
  • a toothing 19 is formed on the outer circumference of the inner sleeve 11, which interacts with a toothing 20 which is formed on a shoulder 21 in the lower region of the outer sleeve 3, on which the outer sleeve 3 from the diameter of its bore 9 changes to the smaller diameter of the cylindrical recess 15 at the lower end. If the inner sleeve 11 is pushed sufficiently far into the outer sleeve 3, the toothings 19, 20 engage in one another, so that the sleeves 11, 3 can no longer rotate against one another.
  • the toothing comprises nine teeth distributed over the circumference, so that the inner sleeve 11 can be locked in a corresponding number of rotational positions.
  • the scale of the figures results from the fact that the hinge pin has a diameter of 12 mm.
  • the eccentricity i.e. the transverse spacing of the axes 7.8 from one another is 0.65 mm in one embodiment, so that a maximum displacement of 1.3 mm in the transverse direction can be achieved.
  • a flange ring 22 is provided which engages over the upper end of the outer sleeve 3 and also engages a radial distance between the band parts 1,2, so that the load of the wing from the upper band part through the flange ring 22 directly into the lower band part 2 is derived without the hinge pin bushing 100 would be affected.
  • the flange ring 22 has an axial tubular cylindrical projection 23 on the inside, which fits with its outer circumference into the bore 9 of the outer sleeve.
  • the projection 23 On the outer circumference, the projection 23 has a rib 24 which snaps into an inner circumferential groove of the bore 9, so that the flange ring 22 is fixed on the outer sleeve 3.
  • the approach 23 ends with its lower edge 26 in a plane perpendicular to the axis.
  • the mutually facing edges 26, 27 have a distance 28 in the axial direction, i.e. in the direction of engagement of the teeth 19, 20, which allows the inner sleeve 11 as shown in FIG. 1 to be pushed up so far that the teeth 19, 20 are free from one another and the inner sleeve 11 can be rotated in the outer sleeve 3.
  • the inner sleeve 11 and the flange ring 22 are separated from one another and are not rotationally connected to one another. This means that the inner sleeve 11 can be rotated easily, although the flange ring 22 is held with considerable friction under the load transmitted by the upper band part 1. The adjustment by rotating the inner sleeve can thus be carried out with the wing attached, without having to rotate the flange ring 22 as well.
  • the inner sleeve 11 has on its thick-walled, i.e. 1 on the left in FIG. 1 has an extension 29 which extends over approximately 180 ° and extends within the extension 23 into the region of its upper end.
  • the approach 23 has a uniform wall thickness and is overlapped by the extension 29 inside. As a result, the bearing length for the hinge pin 10 extends upwards on the left-hand side according to FIG. 1.
  • axially parallel incisions in the exemplary embodiment form three tongues 30 which are evenly distributed over the circumference and which have outwardly directed projections 31 at the lower end which, in the operating state, overlap the lower edge of the band sleeve bore 4 and the band journal sleeve 100 in front of it keep being pulled out of the hinge bore 4 when the wing is detached from the hinge pin 10 upwards.
  • three latching tongues 40 projecting inward in the region of the circumferential groove 16 are also provided at the lower end of the outer sleeve 3, which engage in the manner shown in FIG. 8 against the undercut 32 forming the lower one Set flank 33 of groove 16.
  • the radially inner boundary 34 of the latching tongues 40 maintains a radial distance 35 from the base 17 of the circumferential groove 16.
  • All three parts 3, 11 and 22 of the hinge pin bushing 100 consist of a suitably chosen plastic.
  • the flange ring 22 has high hardness and optimal sliding properties in order to transfer the weight of the wing well.
  • the bushes 3.11 have a limited elasticity.
  • the elasticity of the bushing 3 is sufficient to be able to push the tongues 30 so far inwards when inserted into the band bushing bore 4 that the projections 31 slide along the inner circumference of the band bushing bore 3 and the tongues 30 spring open again when the outer bushing 3 is fully inserted .
  • the elasticity of the inner sleeve 11 is sufficient for the latching tongues 40 to be pushed outwards when inserted through the lower part of the cylindrical outer circumference 14.
  • the latching tongues 40 jump in as shown in FIG. 8 and engage against the flank 33 forming the undercut 32.
  • the elasticity of the outer sleeve 3 can be chosen so that the latching tongues 40 when they occur 8, an axial force to move the inner sleeve 11 according to FIG. 8 upwards, closing the distance 35, sliding inward and thereby releasing an axial path for the inner sleeve which enables the toothings 19, 20 to be released from one another.
  • the locking tongues 40 extend in the exemplary embodiment by approximately 45 ° downwards and inwards.
  • projections 43, 44 are attached, which facilitate the detection of the adjustment position of the sleeves 11, 3.
  • the reference numbers are the same. 9 to 17, the representation is such that the axes 7, 8 lie one behind the other perpendicular to the plane of the drawing.
  • the toothings 19, 20 are not held in engagement by a design of the lower end of the outer sleeve 3 corresponding to the latching tongues 40 in FIGS. 1 to 8, but by a separate part, the so-called spring cup 50.
  • the spring cup 50 consists of a suitable resilient plastic, the interior 36 of which has a hexagonal cross section (see FIGS. 12, 13) for receiving a correspondingly shaped turning tool.
  • the outer shape is also hexagonal, and the spring cup 50 with this cup-shaped part is seated in a hexagonal part 36 'of a continuous recess of the bottom part 13 of the inner sleeve 11, designated as a whole as 37.
  • the spring cup has resilient tongues 60, three of which are distributed over the circumference in the exemplary embodiment and which extend radially outward from the edge of the spring cup.
  • the spring tongues 60 point at an angle of approximately 30 ° to the end of the spring cup 50 which has the latching tongues 39, as is indicated by dash-dotted lines in FIG. 9.
  • Radially displaceable locking slides 65 are provided in the circumferential areas that remain free between the resilient tongues 60 and are guided in a dovetail-shaped undercut recesses 61 on the lower edge of the outer sleeve 3 so as to be displaceable to the outside (see FIGS. 11, 12).
  • the locking slide 65 are held together by a thin detachable ring 62 which, like the locking slide 65 itself, is made of plastic.
  • the locking slides 65 On the inside, the locking slides 65 have an inwardly and upwardly inclined inclined surface 63 which interacts with a conical chamfer 64 at the leading end of the base part 13 of the inner sleeve 11.
  • the locking slide 65 has a bevel 66 which is intended to bear against the countersink 67, which is only indicated in FIGS. 9 and 10, at the lower end of the band sleeve bore 4.
  • the inner sleeve 11 has at its upper edge a push-off peripheral projection 24 ', which sits at the end of an axially widened peripheral groove 25' of the inside of the outer sleeve 3, which also receives the peripheral projection 24 of the shoulder 23 of the flange ring 22. Due to the circumferential projection 24 ', the inner sleeve 11 cannot slide further down.
  • the spring cup 50 is inserted and engages over the connecting ring 62 connecting the locking slide 65 with the spring tongues 60 from the outside.
  • the spring tongues 60 are under tension and extend approximately in a plane radial to the axis, as shown in solid lines in FIG. 9. However, they have the tendency to deform into the position shown in broken lines in FIG. 9.
  • the flange ring 22 leaves an axial distance 45 from the upper end of the outer sleeve 3.
  • the hinge pin bushing 200 is pushed into the band sleeve bore 4 of the band part 2 (see FIGS. 1 and 8). If the wing is then hooked in, its weight presses down the flange ring 22 by closing the spacing space 45 until it rests against the upper end of the outer sleeve 3, the upper circumferential projection 24 'being pushed away and out of the inner circumferential groove 25' onto the cylindrical part of the Bore 9 of the outer sleeve 3 arrives. The hinge pin coming into contact with the bottom of the bore 12 of the inner sleeve 11, which is not shown in FIGS.
  • the locking slides 65 not only have a chamfer 66 on the top of their outer end, but also a chamfer 68 on the bottom so that they do not protrude from the conical chamfer 69 of the lower end of the outer sleeve 3 in the delivery state, as shown in FIG. 9 can be seen.
  • the adjustment can be carried out in the manner described above by rotating the inner bushing 11 within the outer bushing 3 without having to also rotate the flange ring 22.
  • the hinge pin bush 300 is assembled by exerting an axial pressure from below with the turning tool.
  • the latching hooks 39 snap into place and, on the other hand, the locking slides 70 are pressed outwards while sliding over the conical outer circumferential area 52 until their inclined surface 66 comes into contact with the countersink 67 of the band sleeve bore 4.
  • the inner ends of the locking slide 70 stand against a cylindrical outer peripheral region 53 of the spring cup 55 which adjoins the conical outer peripheral region 52 downward, so that there is a definite locking in the radial direction.
  • the spring tongues 60 bear against the end face 42 essentially without force.
  • the spring cup 55 and the inner sleeve 11 are pressed upwards by means of the rotary tool engaging in the recess 36 until the toothings have disengaged.
  • the spring tongues 60 assume the position shown in solid lines in FIG. 9. The rotation can now take place without the flange ring 22 being taken along.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Hinges (AREA)
  • Closing And Opening Devices For Wings, And Checks For Wings (AREA)
  • Pens And Brushes (AREA)
  • Pivots And Pivotal Connections (AREA)
  • Mechanical Coupling Of Light Guides (AREA)
  • Mechanical Pencils And Projecting And Retracting Systems Therefor, And Multi-System Writing Instruments (AREA)
  • Adhesive Tape Dispensing Devices (AREA)
EP91110616A 1990-07-16 1991-06-26 Douille pour broches de ferrures ou charnières Expired - Lifetime EP0467122B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE4022531A DE4022531A1 (de) 1990-07-16 1990-07-16 Bandzapfenbuechse
DE4022531 1990-07-16

Publications (2)

Publication Number Publication Date
EP0467122A1 true EP0467122A1 (fr) 1992-01-22
EP0467122B1 EP0467122B1 (fr) 1994-01-26

Family

ID=6410348

Family Applications (1)

Application Number Title Priority Date Filing Date
EP91110616A Expired - Lifetime EP0467122B1 (fr) 1990-07-16 1991-06-26 Douille pour broches de ferrures ou charnières

Country Status (5)

Country Link
EP (1) EP0467122B1 (fr)
AT (1) ATE100890T1 (fr)
DE (3) DE4022531A1 (fr)
DK (1) DK0467122T3 (fr)
ES (1) ES2049065T3 (fr)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0553600A1 (fr) * 1992-01-31 1993-08-04 GIESSE S.p.A. Charnière réglable pour ferrures de portes et fenêtres
US6412880B1 (en) 2000-03-29 2002-07-02 Honeywell Commercial Vehicle Systems Co. Combined power supply and electronic control circuit for ABS
EP1544392A1 (fr) * 2003-12-19 2005-06-22 OTLAV SpA Charnière, particulièrement pour soutenir des cadres, et méthode pour atteindre au moins un de ses composants
WO2006060018A1 (fr) * 2004-12-02 2006-06-08 Stanley Chung Charniere de porte reglable

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE29503554U1 (de) * 1995-03-02 1995-04-20 Schlechtendahl & Soehne Wilh Band für Türen, Fenster o.dgl.
DE29620361U1 (de) * 1996-11-22 1998-04-02 Hahn Gmbh & Co Kg Dr Band für Türen, Fenster u.dgl.
DE29714911U1 (de) * 1997-08-20 1998-12-24 Niemann Hans Dieter Drehverstelleinrichtung für Türen- oder Fensterbänder

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3418138A1 (de) * 1984-05-16 1985-11-21 Dr. Hahn GmbH & Co KG, 4050 Mönchengladbach Bandzapfenbuechse
DE8609628U1 (de) * 1986-04-09 1986-06-05 Dr. Hahn GmbH & Co KG, 4050 Mönchengladbach Band für Türen, Fenster und dgl.
DE3412832C2 (fr) * 1984-04-05 1987-09-17 Dr. Hahn Gmbh & Co Kg, 4050 Moenchengladbach, De

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2160519A1 (de) * 1971-12-07 1973-06-14 Schlechtendahl & Soehne Wilh Einstellbare zapfenbandanordnung
DE7309196U (de) * 1973-03-09 1973-06-20 Hahn W Mechanische Werkstaetten Bandzapfenbuchse
DE3044674A1 (de) * 1980-11-27 1982-07-01 Haps + Sohn GmbH + Co KG, 5620 Velbert Tuerband

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3412832C2 (fr) * 1984-04-05 1987-09-17 Dr. Hahn Gmbh & Co Kg, 4050 Moenchengladbach, De
DE3418138A1 (de) * 1984-05-16 1985-11-21 Dr. Hahn GmbH & Co KG, 4050 Mönchengladbach Bandzapfenbuechse
DE8609628U1 (de) * 1986-04-09 1986-06-05 Dr. Hahn GmbH & Co KG, 4050 Mönchengladbach Band für Türen, Fenster und dgl.

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0553600A1 (fr) * 1992-01-31 1993-08-04 GIESSE S.p.A. Charnière réglable pour ferrures de portes et fenêtres
US6412880B1 (en) 2000-03-29 2002-07-02 Honeywell Commercial Vehicle Systems Co. Combined power supply and electronic control circuit for ABS
EP1544392A1 (fr) * 2003-12-19 2005-06-22 OTLAV SpA Charnière, particulièrement pour soutenir des cadres, et méthode pour atteindre au moins un de ses composants
WO2006060018A1 (fr) * 2004-12-02 2006-06-08 Stanley Chung Charniere de porte reglable

Also Published As

Publication number Publication date
DE4022531C2 (fr) 1993-07-29
EP0467122B1 (fr) 1994-01-26
DK0467122T3 (da) 1994-03-14
DE59100938D1 (de) 1994-03-10
ATE100890T1 (de) 1994-02-15
DE4022531A1 (de) 1992-01-23
DE9017985U1 (de) 1993-09-16
ES2049065T3 (es) 1994-04-01

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