EP1994246A1 - Penture permettant de fixer de manière articulée par charnière un battant mobile sur un châssis immobile - Google Patents

Penture permettant de fixer de manière articulée par charnière un battant mobile sur un châssis immobile

Info

Publication number
EP1994246A1
EP1994246A1 EP07722879A EP07722879A EP1994246A1 EP 1994246 A1 EP1994246 A1 EP 1994246A1 EP 07722879 A EP07722879 A EP 07722879A EP 07722879 A EP07722879 A EP 07722879A EP 1994246 A1 EP1994246 A1 EP 1994246A1
Authority
EP
European Patent Office
Prior art keywords
band
wing
hinge
frame
support
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.)
Withdrawn
Application number
EP07722879A
Other languages
German (de)
English (en)
Inventor
Jürgen Bögel-Pötter
Tibor Herglotz
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 EP1994246A1 publication Critical patent/EP1994246A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D11/00—Additional features or accessories of hinges
    • 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
    • E05D7/0027—Adjustable hinges at the hinge axis in an axial direction
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2600/00—Mounting or coupling arrangements for elements provided for in this subclass
    • E05Y2600/60—Mounting or coupling members; Accessories therefor
    • E05Y2600/634—Spacers
    • E05Y2600/636—Washers

Definitions

  • the invention relates to a band for hinged mounting a movable wing on a fixed frame, with a fastened to the wing leaf hinge part and with a frame fastened to the frame hinge part.
  • the holding forces of the wing are introduced from the leaf hinge part in the frame hinge part.
  • the vertically acting at a vertically extending hinge axis force components are in this case transmitted from the wing hinge part on the frame hinge part by the wing hinge part directly or indirectly, for example by intervening adjustment, which serve to adjust the wing in the frame in the vertical direction, supported on the frame hinge part.
  • a wing For hinge-hinged attachment of a wing to a frame, for example a door, there are always several - at least two - spaced in the direction of the hinge axis se arranged bands use.
  • the frame and wing hinge parts are preassembled before attaching the wing to, for example, by teaching predetermined positions on the frame or wing. After this pre-assembly, the hanging of the wing takes place, for example by inserting and fixing the hinge pin defining hinge pin. Subsequently, the hinges are generally given more attention only when readjustment of the sash in the frame is required. The readjustment is then carried out by displacing the attachment points of the band parts on the frame or the wing or - if provided - by operating integrated in the bands adjustment.
  • the invention is therefore the object of developing a generic tape such that when used in a band comprising a plurality of bands adjustment of the bands in terms of equalization of the distribution of holding forces on the bands of the band assembly is possible.
  • this band means are provided according to the invention, with which the force acting between the band parts in the direction of the hinge axis, detectable and / or influenced.
  • detectable is meant that the fitter can - for example visually - detect after mounting the wing, which forces act, for example, in particular in a vertical direction on the individual bands. If, for example, in the case of the use of two bands, it turns out that almost the entire Weight of the wing is absorbed by the upper band, in other words: that only the wing hinge part of the upper band is supported on the frame hinge part, whereas the wing hinge part of the lower band "in the air", so the fitter by moving the frame and / or of the wing hinge part or by actuation of optionally existing adjustment devices, that, while maintaining the adjustment position of the wing in the frame, part of the, for example, vertically acting forces are also introduced into the lower band.
  • the force which acts between the hinge parts in the direction of the hinge axis can be influenced.
  • this can, since they are automatically effected by means of spring elements, between the frame and the Wing hinge part act.
  • the spring elements are then arranged in the band, that the support of the leaf hinge part takes place on the frame band part via these spring elements. If the bands provided for attaching the wing to the frame are each prepositioned to such an extent that the spring elements of all bands are subjected to force after the wing is suspended, a distribution of the forces takes place depending on the respective spring tension on the individual bands, without this being the case further action is needed.
  • the hydraulic or pneumatic volumes of these support elements can then be connected to one another in a communicating manner so that the same pressure is automatically set on each of the support elements and thus all the bands are loaded approximately uniformly.
  • pneumatically acting support elements each with a closed volume as spring elements, wherein the distribution of forces in the individual bands can be detected for example by coupled to the individual support elements pressure indicator devices.
  • the means comprise a piezoelectric support element.
  • a piezoelectric support element This can be used on the one hand for detecting the force by tapping and evaluating the piezoelectric voltage or for influencing the force acting between the hinge parts in the direction of the hinge axis, by applying to the piezoelectric support an external electrical voltage, which is connected to the desired contraction or expansion of the support element leads in the direction of the hinge axis.
  • an external electrical voltage which is connected to the desired contraction or expansion of the support element leads in the direction of the hinge axis.
  • the piezoelectric support elements for adjustment or as adjustment aid.
  • the means with which the force acting between the band parts in the direction of the hinge axis, can be detected pressure-sensitive support means, in which the pressure acting on them is visually perceptible.
  • These support elements may consist in particular of plastic materials whose color changes depending on the pressure.
  • Figure 1 a fragmentary - a two-band band assembly for connecting a wing profile to a frame profile in a perspective view;
  • FIG. 2 shows a plan view of a first embodiment of a band according to the invention in a partially sectioned illustration of the frame band part;
  • Fig. 3 shows a second embodiment in a Fig. 2 corresponding view
  • Fig. 4 shows a third embodiment of a tape according to the invention - partially cut - in a view corresponding to approximately Fig. 1;
  • Fig. 5 shows the band shown in Fig. 4 above in an enlarged view
  • FIG. 6 is a perspective view of a first variant of an optionally separately usable and removable adjusting aid on a band arrangement comprising two bands;
  • FIG. 7 shows the adjusting aid in FIG. 6 with partially cut frame hinge part
  • FIG. 8 shows a second embodiment of an adjusting aid in a view corresponding to FIG. 6;
  • FIG. 9 shows the same adjustment aid as in FIG. 8 in a view corresponding to FIG. 7;
  • FIG. 10 shows a third embodiment of the adjusting aid in a view corresponding to FIG. 9; 11 shows a further variant of a band according to the invention in a plan view with optically acting pressure detecting means;
  • FIG. 12 shows the embodiment according to FIG. 11 in a representation showing the frame hinge part
  • Fig. 13 shows a further embodiment of the tape according to the invention in a Fig. 12 corresponding representation with wear body and
  • Fig. 14 shows the detail XIV in Fig. 13 in an enlarged view.
  • the band assembly shown in Fig. 1 comprises two bands 1, 2, the hinged joint attachment of a wing to a frame, wherein of the wing only the wing profile 3, of the frame, only the frame profile 4 is shown.
  • the bands 1, 2 each comprise a wing hinge part 5 and a frame hinge part 6.
  • the hinge parts 5, 6 for mounting on the front surfaces 7, 8 of the wing profile 3 and the frame profile 4 are formed.
  • the invention is by no means limited to such configured bands, but it can be further developed according to the invention in any other way mountable bands, for example those whose band parts are mounted in the gap between the wing and the frame.
  • the exemplary embodiment of a band according to the invention shown in FIG. 2 may be band 1 shown above in FIG. 1 as well as band 2 shown below. Also, more bands can be provided, in particular for heavy wings, which can then be configured in a corresponding manner. In the following, by way of example, reference will always be made to the upper band of a band arrangement.
  • the band 1 comprises a hinge pin 9 in the frame hinge part 6 surrounding hinge pin bushing 10, which has a top of the frame hinge part 6 outstanding, a support surface for the wing hinge part 5 forming circumferential collar 11.
  • the hinge pin bushing 10 is mounted in a recess 12 of the frame hinge part 6. In its lower part, the recess 12 has an internal thread 13, in which a designated as a whole by 14 support bearing, which has a complementary external thread 15, is screwed.
  • the support bearing 14 has an approximately cup-shaped base body 16, in which a support body 17 is mounted approximately in a piston-like manner and is supported on the bottom of the base body 16 via a plate spring assembly 18 formed as a spring element.
  • a plate spring assembly 18 formed as a spring element.
  • On the upper side 19 of the support body 17 rests the lower end face of the hinge pin bushing 10th
  • the base body 16 of the support bearing 14 is screwed so far into the recess 12 that the disc spring assembly is biased under the action of the support body 17 with hinged wing, so that at least a portion of the forces acting in the direction of the hinge axis S forces of the hinge pin bushing 10 via the support bearing 14 is introduced into the frame hinge part 6.
  • FIG. 1 Another embodiment of a tape according to the invention is shown in FIG.
  • Corresponding components in their function are denoted by the same reference numerals as in FIG. 2, but increased by 100.
  • the band 101 in turn comprises a wing band part 105 and a frame band part 106.
  • a support bracket 114 for the band bolt bushing 110 is again provided in the recess 112 in the frame band part 106, which however is formed in one piece and only consists of a base body 116.
  • the hinge pin bush 110 On the upper side 119 of the base body 116, the hinge pin bush 110 is supported directly.
  • the circumferential collar 111 of the band bushing 110 is designed as a spring element 120, which elastically deforms under the action of the force acting on the leaf hinge part 105 in the direction of the hinge axis S.
  • the function of the embodiment shown in Fig. 3 therefore corresponds substantially to that of FIG. 2.
  • the spring element acts on the at least a part of the hinge axis in the direction of the hinge axis S of the leaf hinge part in the frame hinge part, but not between the hinge pin bushing 110 and the Support bearing 114 is provided, but between the wing hinge part 105 and the hinge pin bushing 110 formed by the circumferential collar 111.
  • a sliding disk 121 is provided between the latter and the leaf hinge part. It consists of a Gieitreibungskostoryen reducing material, such as Teflon.
  • FIGS. 4 and 5 Another embodiment of a tape according to the invention is shown with reference to FIGS. 4 and 5. Corresponding components in their function are denoted by the same reference numerals as in Figs. 1 and 2, but increased by 200. In order to avoid repetition, again only the differences from the exemplary embodiment according to FIG. 2 are discussed.
  • a recess 222 is provided in the lower region of the wing band part 205 around the band pin 209, in which a flexible support element 223 having an interior volume is arranged ,
  • the internal volume of the support element which serves to receive a hydraulic or pneumatic medium under pressure, is connected via a communicating line 224 to the volume of the corresponding support element in the belt 202, so that the same pressure always prevails in the inner volumes of the support elements.
  • a friction-reducing element 224 is again provided between the circumferential collar 211 and the support element 223, which is non-rotatable in the frame hinge part 204 and thus is also arranged rotationally fixed to the support element 223.
  • FIGS. 6 and 7. Another embodiment of the invention is shown in FIGS. 6 and 7. Again, corresponding components with the same reference numerals as in Fig. 2, but increased by 300, referred to.
  • the means with which the force acting between the hinge parts in the direction of the hinge axis, can be detected not formed as part of the band, but as an additional, optionally attachable component, which is hereinafter referred to as adjustment aid.
  • adjustment aid is - as shown in Fig. 6 - during the adjustment process in all bands 301, 302 used to determine the forces that transmit in both bands of the respective wing hinge part 305 in the respective frame hinge part 306 in the direction of the hinge axis S. become.
  • the adjustment aids designated by 325 in FIGS. 6 and 7 comprise a support extension 326, via which the leaf hinge part 305 is supported on the circumferential collar 311 of the hinge pin bushing 310.
  • the supporting extension 326 comprises piezoelectric elements which are electrically connected to an electrical connection 327 provided on the adjusting aid 325 and generate therefrom an electrical voltage whose height depends on the pressure force exerted in the direction of the hinge axis S on the supporting extension 326.
  • the distribution of the forces acting in the direction of the hinge axis S on the individual, provided for connecting the wing to the frame bands can be done by comparing the piezoelectric voltages.
  • optionally connectable auxiliary devices are used.
  • FIGS. 8 and 9 it is also possible, as shown in FIGS. 8 and 9, to integrate voltage measuring devices with suitable displays directly in the adjusting aids, as is the case, for example, with the adjusting aids 425 shown in FIGS. 8 and 9 and otherwise the adjusting aids 325 correspond.
  • the adjusting aids 325, 425 are intended to be removed again after adjustment in the sense of the desired distribution of the introduction of force to the various belts.
  • alignment aids 325, 425 designated components fixed to the belts 301, 302; 401, 402 so that they are permanently installed and the distribution of forces on the individual bands is constantly verifiable.
  • this comprises a plug instead of the electrical connection 327 or the display 427 Indicator 527 coupled to support extension 526 which changes color as a function of the pressure acting on support extension 526.
  • FIGS. 11 and 12 A further exemplary embodiment of a band according to the invention, in which the indicator, which makes the magnitude of the introduced force visually perceptible, is integrated in the band, is shown in FIGS. 11 and 12. Again, corresponding components are given the same reference numerals as in FIG. however, increased by 600, referred to.
  • a pressure-sensitive support element 628 in the form of a ring pushed onto the circumferential collar 611 is provided on the circumferential collar 611 of the hinge pin bushing 610 at the upper end region of the peripheral collar 611.
  • the pressure-sensitive support member abuts against the leaf hinge part 605 and thus detects the force which is introduced in the direction of the hinge axis S of the wing hinge part 605 in the circumferential collar 611. It is made of a material which changes its color as a function of the introduced compressive force, so that the introduced compressive force - and with several correspondingly configured bands the pressure force distribution - is visually recognizable.
  • FIGS. 13 and 14 A further embodiment of a band according to the invention is finally shown in FIGS. 13 and 14. Again, corresponding components are designated by the same reference numerals, but now increased by 700.
  • a wear body 729 in the form of a wear plate is provided between the wing band part 705 and the peripheral collar 711 of the band bolt bushing 710 (see in particular FIG. 14).
  • This wear body consists of a material which exceeds a predetermined load value when the blade is actuated, but has abrasion-resistant properties below this load value.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Clamps And Clips (AREA)
  • Pivots And Pivotal Connections (AREA)

Abstract

L'invention concerne une penture permettant de fixer de manière articulée par charnière un battant mobile sur un châssis immobile, laquelle penture présente une partie penture de battant (5, 105, 205, 305, 405, 505, 605, 705) pouvant être fixée sur le battant et une partie penture de châssis (6, 106, 206, 306, 406, 506, 606, 706) pouvant être fixée sur le châssis. Selon ladite invention, cette penture est pourvue de moyens permettant de détecter et/ou d'influer sur la force s'exerçant entre les parties de penture (5, 105, 205, 305, 405, 505, 605, 705; 6, 106, 206, 306, 406, 506, 606, 706) en direction de l'axe de charnière (S).
EP07722879A 2006-03-11 2007-02-21 Penture permettant de fixer de manière articulée par charnière un battant mobile sur un châssis immobile Withdrawn EP1994246A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE202006004145U DE202006004145U1 (de) 2006-03-11 2006-03-11 Band zur scharniergelenkigen Verbindung eines beweglichen Flügels an einem feststehenden Rahmen
PCT/EP2007/001502 WO2007104410A1 (fr) 2006-03-11 2007-02-21 Penture permettant de fixer de manière articulée par charnière un battant mobile sur un châssis immobile

Publications (1)

Publication Number Publication Date
EP1994246A1 true EP1994246A1 (fr) 2008-11-26

Family

ID=38179624

Family Applications (1)

Application Number Title Priority Date Filing Date
EP07722879A Withdrawn EP1994246A1 (fr) 2006-03-11 2007-02-21 Penture permettant de fixer de manière articulée par charnière un battant mobile sur un châssis immobile

Country Status (3)

Country Link
EP (1) EP1994246A1 (fr)
DE (1) DE202006004145U1 (fr)
WO (1) WO2007104410A1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2942538B1 (fr) * 2009-02-26 2012-06-08 Airbus France Dispositif de mesure de moment de charniere
GB2490663A (en) * 2011-05-05 2012-11-14 Intastop Ltd A door mount having a sensor determining the force exerted on the mount

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE363439A (fr) *
DE593899C (de) * 1932-08-10 1934-06-16 Robert Kriechel Scharnier fuer Tueren, Fenster u. dgl.
FR1370410A (fr) * 1963-09-30 1964-08-21 Appareil de levage à coin coulissant commandé hydrauliquement
US3501732A (en) * 1964-05-04 1970-03-17 Endevco Corp Semiconductive piezoresistive transducer having a grooved support with electrical contacts
DE7302348U (de) * 1973-01-23 1973-05-10 Karl Peter Kunststoffe Tuerband
FR2479884B1 (fr) * 1980-04-02 1989-11-17 Laurent Solange Perfectionnements apportes aux paumelles reglables en hauteur
DE3323341A1 (de) * 1983-06-29 1985-01-10 Otto 5227 Windeck Hechler Tuer- oder fensterangel
DE29607915U1 (de) * 1996-05-02 1996-07-25 Lutzenberger, Helmut, Güimar, Teneriffa Türen-Fenster-Anhebe- und Einschlaggerät für Ausgleichsscheiben oder Sprengringe mit integrierter Nach- oder Einstellschraube in Türen-Fensterbeschläge oder Gelenke u.dgl.
AT4096U1 (de) * 1999-11-11 2001-01-25 Flaga Fluessiggas Vertriebsges Wägesystem für lastfahrzeuge
DE20002473U1 (de) * 2000-02-11 2000-07-20 Schüring GmbH & Co. Fenster-Technologie KG, 53842 Troisdorf Einstellbares Gelenkband mit zentrierender Zapfenlagerung

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2007104410A1 *

Also Published As

Publication number Publication date
DE202006004145U1 (de) 2007-08-02
WO2007104410A1 (fr) 2007-09-20

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