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WO1994011592A1 - Guidage de commande forcee du mouvement du battant d'une lucarne - Google Patents

Guidage de commande forcee du mouvement du battant d'une lucarne Download PDF

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Publication number
WO1994011592A1
WO1994011592A1 PCT/DE1993/001057 DE9301057W WO9411592A1 WO 1994011592 A1 WO1994011592 A1 WO 1994011592A1 DE 9301057 W DE9301057 W DE 9301057W WO 9411592 A1 WO9411592 A1 WO 9411592A1
Authority
WO
WIPO (PCT)
Prior art keywords
wing
sash
frame
guide
plane
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.)
Ceased
Application number
PCT/DE1993/001057
Other languages
German (de)
English (en)
Inventor
Ernst Lahmann
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.)
Hautau GmbH
Original Assignee
Hautau GmbH
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
Priority claimed from DE9215108U external-priority patent/DE9215108U1/de
Application filed by Hautau GmbH filed Critical Hautau GmbH
Priority to EP93924501A priority Critical patent/EP0670941A1/fr
Publication of WO1994011592A1 publication Critical patent/WO1994011592A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04D—ROOF COVERINGS; SKY-LIGHTS; GUTTERS; ROOF-WORKING TOOLS
    • E04D13/00—Special arrangements or devices in connection with roof coverings; Protection against birds; Roof drainage ; Sky-lights
    • E04D13/03—Sky-lights; Domes; Ventilating sky-lights
    • E04D13/035—Sky-lights; Domes; Ventilating sky-lights characterised by having movable parts
    • E04D13/0358—Sky-lights; Domes; Ventilating sky-lights characterised by having movable parts the parts moving, in their own plane, e.g. rolling or sliding, or moving in parallel planes with or without an additional movement, e.g. both pivoting and rolling or sliding
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D15/00—Suspension arrangements for wings
    • E05D15/16—Suspension arrangements for wings for wings sliding vertically more or less in their own plane
    • E05D15/20—Suspension arrangements for wings for wings sliding vertically more or less in their own plane movable out of one plane into a second parallel plane
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D15/00—Suspension arrangements for wings
    • E05D15/06—Suspension arrangements for wings for wings sliding horizontally more or less in their own plane
    • E05D15/10—Suspension arrangements for wings for wings sliding horizontally more or less in their own plane movable out of one plane into a second parallel plane
    • E05D15/1042—Suspension arrangements for wings for wings sliding horizontally more or less in their own plane movable out of one plane into a second parallel plane with transversely moving carriage
    • E05D2015/1055—Suspension arrangements for wings for wings sliding horizontally more or less in their own plane movable out of one plane into a second parallel plane with transversely moving carriage with slanted or curved track sections or cams
    • 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
    • E05Y2900/00—Application of doors, windows, wings or fittings thereof
    • E05Y2900/10—Application of doors, windows, wings or fittings thereof for buildings or parts thereof
    • E05Y2900/13—Type of wing
    • E05Y2900/148—Windows
    • E05Y2900/152—Roof windows
    • E05Y2900/154—Skylights

Definitions

  • the invention relates to a guide for the compulsory control of the movement of a roof window sash with the features of the preamble of claim 1.
  • the invention provides a guide for the forced control of the movement of a roof window wing of this type with the configuration according to the teaching of claim 1.
  • This arrangement is particularly suitable for a displacement movement of the Wing from the closed position in the direction obliquely downwards, so that the ventilation opening can be exposed in the upper area of the frame, if a folding wing is arranged above this wing in the sloping roof, so in cooperation and with synchronous opening of the two wings a very special large ventilation opening can be exposed by moving one wing down while the other wing is folded up.
  • the reliable movement, guidance and support can take place.
  • the sash is adjusted between two levels, one level is its closed position, the other level is the level in which it can be moved in the direction of the sloping roof by the guide rails.
  • the entry and exit of the wing into and out of the closing plane is achieved by the essentially horizontally running short branch sections, which run essentially horizontally regardless of the inclination of the wing plane, so that the opening and closing of the wing requires little or no vertical force components . This benefits a user who only has to exert small forces to issue a possibly heavy wing.
  • a compensation force is exerted on the wing via compensation force elements arranged on both sides of the wing (claim 10), which achieve that it regardless of its position of displacement in the main direction of movement is adjustable with essentially the same force and this force is very low because the compensating force elements essentially compensate for the sash weight which is effective in the direction of the sloping roof.
  • the compensation force is for the short adjustment process from the closed position to the raised position or vice versa ineffective.
  • the lifting and closing process which is already smooth due to the horizontal branch sections, is thereby further facilitated, but the sash is kept smoothly in its main adjustment movement in the open state, because the compensating force comes into its own here.
  • the lots can be realized by a slot piece (claim 13); it can also be accomplished by a short, straight (not twisted) end portion of a known torsion bar of a compensation force element which otherwise applies a substantially constant force regardless of its elongation between its attachment ends.
  • a particularly slim shape of the wing and the fitting that guides it is achieved when only two levels are provided, in and between which the rollers of the wing move (claim 6). If an even more precise guidance and support of the wing - be it a hand-operated or a motor-operated wing - is to be achieved, then the pairs of rollers on the wing can not only be spaced apart in the wing plane, but also be spaced perpendicular to the wing plane.
  • the particularly secure support of the wing during its movements in the guide rails is achieved by the vertical and longitudinal displacement of the pairs of rollers on the wing (claim 1).
  • the closed positions of these pairs of rollers in the guide rails can be assigned special inserts (claim 2; claim 7) which carry the branch or switch sections for the rollers which run obliquely to the longitudinal direction of the guide rails. This results in two or three superimposed levels in the guide rails, in which running or support surfaces for the rollers of the wing are arranged.
  • the guide rails can be angular profile rails which have the various raceways or running surfaces and insert pieces used in a specific arrangement.
  • the second leg of the guide rails serves primarily for fastening them to the frame, but also, if appropriate, for receiving and supporting and mounting the motor drives, which can extend along the guide rails.
  • a third pair of rollers can be arranged in the wing plane or offset perpendicular to it so that it runs into the guide rails from their lowermost end section, just before the wing is transferred to the closed position.
  • a horizontal branch section corresponding to the horizontal branch sections mentioned is provided, so that all three pairs of rollers provided run parallel and simultaneously into the substantially horizontal branch sections when the wing is moved into the closed position and when the wing is lifted into the lifting position A. leave this.
  • the invention pays particular attention to the use of the elongated constant force elements which are arranged between the frame and sash so that they pivot by a small angle during the sliding movement of the roof window sash.
  • the use of these (known) constant force elements for the roof windows to be installed obliquely makes the cable pull mechanisms previously required for the wings installed in the roof slope unnecessary (claim 15).
  • Figure 1 is a skylight in a vertical plan view of the sloping roof surface
  • Figure 2 on a larger scale, a vertical section A-B through the parts of the guide 2, 3 running parallel to the direction of displacement of the sash and the sash 1 and the frame 4, with the sash closed;
  • Figure 4 is a side view of the guide rail of the guide of Figure 1 with the wing in the closed position;
  • Figure 5 in the same representation as Figure 4, the guide rail with the wing open and pushed down;
  • FIG. 6 shows an alternative form of the guide 2, 3 from FIG. 1 with a running rail 5 which guides the rollers 12, 13, 14 of the wing 1 in one plane for adjustment movements and holds them in the closed position in a second plane;
  • FIG. 6a shows the part indicated in figure 6 with an XX sectional view in a direction vertical to the frame plane direction, for explaining the two levels between which the blade 1 is movable, in particular the closing plane E j _ and the plane of movement E 2;
  • Figures 7a, 7b and 7c three schematic representations of the wing movement when attaching the wing 1 and the window frame 4 in an inclined roof direction of about 30 °, the guide rails 5 being omitted for the sake of clarity, but can be equipped as shown in Figure 6 or Figure 5 show;
  • Figure 8 is an enlarged cross section of the slot piece 50, which is arranged in Figures 7a, 7b and 7c at the upper end of the compensation force element (39) there, in an exemplary position according to Figure 7c.
  • FIGS. 2 and 3 are cross sections along the section lines A-B of FIG. 1.
  • 1 denotes the casement and 4 the frame.
  • one leg 6 of an angular guide rail 5 is attached, on the other leg 7 guide and
  • Support surfaces 8,9,10 are formed, on which rollers 12,13 can be supported, which are fastened with a mounting plate 11 on the casement side.
  • a motor drive 15 which extends over the length of the side of the wing and is fixedly connected to the wing frame 1 with its movable member via a driver 16.
  • the entire arrangement is covered by a hood-shaped cover 17, which is firmly connected to the casement 1 and can sealingly cooperate at 18 with a corresponding seal 19 on the frame or on the guide rail 5, as can be seen from FIGS. 2 and 3.
  • rollers on the wing are arranged in pairs on both sides in axial alignment, the wing being two pairs of rollers as
  • the pairs of rollers 12 and 13 are, as can be seen from FIGS. 4 and 5, with respect to the plane of the casement both in the direction of displacement and in the direction perpendicular to each other. There is a different one in the guide rail for each pair of rollers
  • insert pieces 30 are inserted in the guide rails at selected points, which guide switch sections 31 for the Provide guideways. As can be seen from FIGS. 4 and 5, the two insert pieces 30 are arranged in the same sense and with the same dimensions in the direction of displacement and perpendicular to one another, as is the case with the pairs of rollers 12 and 13.
  • the two insert pieces 30 are arranged in the same sense and with the same dimensions in the direction of displacement and perpendicular to one another, as is the case with the pairs of rollers 12 and 13.
  • Switch sections 31 connect the different height levels of the running or support surfaces 8, 9, 10 for the running rollers.
  • Figure 5 shows the arrangement with dash-dotted wing 1 in the open position.
  • the offset in the direction of displacement of the pairs of rollers 12, 13 is designated 32. It ensures that the sash weight is securely picked up and set down when it moves on the guide rails 5, 6, 7.
  • the distance in the direction of displacement of the pairs of rollers corresponds to approximately half the possible maximum displacement movement of the sash between the closed position and the maximum open position.
  • the size of the opening to be exposed in the sliding direction is designated 33.
  • the switch sections 31 in the inserts 30 ensure a parallel lifting and pressing of the wing at the beginning of the opening movement or at the end of the closing movement, the angle of the guide rail switch 31 in the insert 30 being adapted to the roof slope so that the movement of the wing into the lifting position (Start of opening) and from the lifting position when transferring to the closed position can be achieved without a substantial vertical force component.
  • the sash is thus reliably and securely held and guided and allows easy opening over a large area.
  • FIG. 6 schematically shows the guidance of a roof window sash 1 when it is kept in a particularly narrow design. Only one guide surface 9 is provided, which runs parallel to the sloping roof and has two upper inlet sections 10a and 10b and a lower inlet section 10c, which lead into the second plane - the closing plane - of the window sash 1.
  • the elongated straight section of the guide is continuous.
  • the short inlet and outlet sections 10a, 10b and 10c in the inserts 30a, 30b, 30c of the entire guide rail 5 are essentially horizontal.
  • a role of the roller pairs 12, 13, which are guided in the guide rail shown in FIG. 6, is shown in each case.
  • rollers 12a, 13a are shown in two wing positions, on the one hand in the closed position, in which they have run in at the rear end in the two upper inlet sections 10a, 10b which are close to one another. This is the wing closed position.
  • the second wing position shown is the maximum open position at which the two spaced rollers 12a, 13a come to rest in their end position at the lower end of the guide.
  • the deep-lying roller 12a has run against a stop 5a, which is arranged in the course of the guide 5 to determine the maximum opening travel of the wing.
  • a further inlet switch 10c is provided below the stop 5a, which corresponds to the section 30b.
  • the roller 14a which is a roller of the axially aligned roller pair 14 is only held in the wing closed position, while the roller pair 14 is in the open position of the wing without guidance, that is to say exposed.
  • an expanding guide receiving section 9a can be provided at the lower end of the guide rail 5.
  • the entire guide rail 5 can be embodied integrally or in one piece with its elongated one guide section 9 and its three short substantially horizontally running inlet sections 10a, 10b and 10c. Then a guide rail 5 is only suitable for a sloping roof. Modularly, a large number of sloping ceilings can be equipped with the guide rail according to FIG. 6 if the two upper sections 30a and 30b and possibly also the optional third section 30c are interchangeable. They then form short switch sections 30a, 30b, 30c, which have already been explained in the context of FIGS. 4 and 5 as switch sections 30 were. These switch sections can be designed such that they have different inclinations of the inlet and outlet sections 10a, 10b, 10c depending on the roof slope, as is shown schematically with the switch sections 30b 'and 30b "for the switch 30b. The different angles that the
  • Inlet sections 10b 'and 10b "in this case opposite the direction of the elongated tread 9 can then be matched to the respective roof slope in which the window is to be installed.
  • switch sections 30, 30a, 30b and 30c of which the
  • Switch sections 30b and 30c can even be identical, almost all angles of roofs can be compensated so that the short inlet and outlet sections 10a, 10b and 10c each run essentially horizontally, in order to raise almost no vertical force component when lifting and running in the wing to have to.
  • the switch section that best guarantees a horizontal alignment of the short inlet section can be used for this roof. In this way it can be ensured that the vertical force component when the wing is raised can be reduced to zero with only a limited number of rail pieces or switch pieces or with slight inclinations of the short ones
  • the vertical force can thus be kept independent of the sloping roof.
  • compensation force elements 39 are pivotally hinged laterally on the wing 1 with their longitudinal axis 39a. They allow compensation of the leaf weight acting in the adjustment direction so that the leaf is balanced in every open position, that is to say it does not move in the closing direction or further in the opening direction. Only small adjustment forces then have to be applied by hand in order to move the leaf in the closing direction or further in the opening direction.
  • compensation force elements consist, for example, of two mutually extending springs that mutually neutralize their tensile force (inner and outer springs 41), which can be precisely matched to the effective weight of the sash (depending on the sloping roof and the window size).
  • compensation force elements are commercially available under the name "Torso", each specifying a specific weight class.
  • Cover frame 4 The slack is achieved in that a roof-mounted bolt (arranged on the cover frame 4 or the running rail 5) is displaced in a longitudinal slot 51. While the bolt is in the closed position of the wing 1 at the lower end of the longitudinal slot 51, it lies in the
  • Lifting division A (at the beginning of the opening position of the wing in the direction of the arrow S) at the upper end of the longitudinal slot 51. This begins the effect of the constant force of the element 39 on the wing 1. It is then constantly effective with the elongated spring 41 until the wing has reached the lower stop 5a. This is shown in Figure 7c. If the wing is moved back from the adjustment position shown in FIG. 7c in the direction of its closed position in the direction of the arrow S shown, then it arrives in the adjustment position which is sketched in FIG 39 picks up. The wing can be brought into and out of its closed position without great effort, which is shown in FIG. 7a. This adjustment of the wing is short and, if it is combined with the horizontal switch sections according to FIG. 6, it can also be carried out by persons who are able to exert only little force.
  • connection of the slot piece 50 with the balancing constant force of the element 39 and the horizontal inlet sections 10a, 10b, 10c can thus provide the total ease of movement of an otherwise difficult to operate roof wing in the direction of the sloping roof.
  • the slot piece 50 is shown in cross section in FIG. 8. It consists of a rectangular metal plate (tab), which has an elongated slot 51 approximately in the middle, the Width is adapted to the bolt diameter 52. The lower end of the tab is attached to the outer spring 41 of the constant force element 39 via a rivet attachment 43. If a split pin 53 prevents the slotted piece 50 from sliding off the bolt 52 during operation, the interchangeability of the spring element 39 can nevertheless be made possible.
  • a constant force element 39 for example the torso "spring” mentioned above
  • Damaged constant force elements can also be easily replaced.
  • the slotted piece In addition to the longitudinal displacement on the bolt, the slotted piece also permits a pivoting movement of the axis 39a of the compensation force elements 39, which ensures continuous alignment of all parts of the element 39, regardless of the lifting / displacement movement of the wing 1.
  • the slot piece 50 Without the slot piece 50, a loose effect can also be achieved with a special design of the twisted (not shown) inner rod of the constant force element.
  • the technical design of the known elongated constant force element will be briefly discussed. It consists of a precision hollow tube 40 with a first spring 41 (outer spring) recessed therein.
  • the hollow tube 40 is rotatably articulated on a fastening tab 42 on the wing 1.
  • Outer spring 41 is either attached to the slot piece 50 (with the constant force element unchanged) or directly linked to the bolt 52 with the changed constant force element described below, via an upper attachment tab 43.
  • the outer spring 41 runs a wound inner spring, which is twisted or relaxed by a twisted rod with a variable thread pitch so that an inner spring force counteracts the external spring force. Becomes the elongated twisted rod with variable thread pitch
  • FIG. 6a shows the section indicated by XX in FIG. 6 in a vertical plane relative to the sash plane of sash 1.
  • the section illustrates the frame spar 4 and the sash 1 which can be displaced in an adjustment plane E 2 and which has its closed position in the plane E ⁇ Has.
  • the wing 1 is guided by pairs of rollers 12, 13 (possibly also 14) on a supporting surface or plane 9, which forms the track for the roller 12 a shown in section in the adjustment plane E 2 .
  • the roller 12a shown in section has entered the inlet section 10b and lies against the rear semicircular end thereof.
  • FIG. 6a is otherwise designed like the section according to FIG. 3 (but without a motor).
  • the constant force element 39 is articulated at its two ends 42, 43. With its lower end 42 it is
  • the other end 43 is articulated via the slot piece 50 already described on the running rail or the frame.
  • the constant force element 39 is thus located above the support bracket 16 outside the running rail 5, but still above and in the area of the frame spar 4.
  • the constant force elements in the double-articulated form are provided on both sides of the wing on both oblique frame spars 1.
  • An approximately L-shaped bent metal shield 19a can protect the running rail 5, U-bracket 16 and the easily pivotable constant force element 39 against wind and weather influences, for which elastic rubber lips 19 additionally take care of the free edge of the
  • Shield 19a cooperate sealingly in the closed position E 1 of the wing.
  • the use of the easily pivotable constant force elements 39 arranged on the outside enables the cable pull mechanisms previously used to be eliminated in the case of inclined roof windows, enables modularization by adapting the specific constant force to the respective sash weight and enables simple mounting and adjustment of the roof windows without threading of ropes and weights with

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  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Power-Operated Mechanisms For Wings (AREA)

Abstract

Un guide de commande forcée du battant (1) d'une lucarne permet d'ajuster librement le battant (1) de la lucarne. A cet effet, le battant (1) se déplace sur deux plans, le plan de fermeture (10) et le plan d'ajustement principal (9). Des paires de rouleaux (12, 13, 14) qui roulent sur des surfaces de roulement ou de soutien (8, 9, 10; 10a, 10b, 10c) peuvent se situer dans deux ou trois plans superposés. Dans son plan d'ajustement principal (9), le battant (1) se déplace dans un seul plan. Lesdites paires de rouleaux peuvent se déplacer dans plusieurs plans (8, 9, 10). Pour fermer le battant elles pénètrent dans de courts embranchements sensiblement horizontaux, quelle que soit l'inclinaison de la section de guidage principale allongée (9). En outre, une force constante (39) temporairement découplée peut être exercée sur le battant pendant sa course d'ajustement (S) par une pièce de guidage à fente (50).
PCT/DE1993/001057 1992-11-06 1993-11-05 Guidage de commande forcee du mouvement du battant d'une lucarne Ceased WO1994011592A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP93924501A EP0670941A1 (fr) 1992-11-06 1993-11-05 Guidage de commande forcee du mouvement du battant d'une lucarne

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
DEG9215108.6U 1992-11-06
DE9215108U DE9215108U1 (de) 1992-11-06 1992-11-06 Führung zur zwangsweisen Steuerung der Bewegung eines Dachfensterflügels
EP93115289 1993-09-22
EP93115289.6 1993-09-22

Publications (1)

Publication Number Publication Date
WO1994011592A1 true WO1994011592A1 (fr) 1994-05-26

Family

ID=25960121

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/DE1993/001057 Ceased WO1994011592A1 (fr) 1992-11-06 1993-11-05 Guidage de commande forcee du mouvement du battant d'une lucarne

Country Status (1)

Country Link
WO (1) WO1994011592A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE202005003434U1 (de) * 2005-03-03 2005-12-08 H. H. Heim Und Haus Holding Gmbh Fenster

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0290645A1 (fr) * 1987-05-12 1988-11-17 Morkel-Liemberg, Maria Couverture pour des ouvertures de toit
GB2220968A (en) * 1988-06-24 1990-01-24 Percy Lane Limited Sliding window
US4924930A (en) * 1986-11-21 1990-05-15 Craig Drennan Window assembly
WO1991019070A1 (fr) * 1990-05-29 1991-12-12 Stephen William Emanuel Installations architecturales telles que des fenetres et des portes

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4924930A (en) * 1986-11-21 1990-05-15 Craig Drennan Window assembly
EP0290645A1 (fr) * 1987-05-12 1988-11-17 Morkel-Liemberg, Maria Couverture pour des ouvertures de toit
GB2220968A (en) * 1988-06-24 1990-01-24 Percy Lane Limited Sliding window
WO1991019070A1 (fr) * 1990-05-29 1991-12-12 Stephen William Emanuel Installations architecturales telles que des fenetres et des portes

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE202005003434U1 (de) * 2005-03-03 2005-12-08 H. H. Heim Und Haus Holding Gmbh Fenster

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