BE1021225B1 - IMPROVED CONSTRUCTION FOR A WINDOW, A DOOR OR THE LIKE COMPOSITE PROFILE, KIT AND METHOD OF MANUFACTURING IT - Google Patents

Abstract

IMPROVED CONSTRUCTION FOR A WINDOW, DOOR OR THE LIKE ASSEMBLED PROFILE, KIT AND METHOD FOR MANUFACTURE THEREOF In a first aspect, the present invention relates to an improved construction for a window, a door or the like. In a second and third aspect, the present invention relates to a frame and a wing for a window, a door or the like, respectively. In a fourth aspect, the invention relates to a composite profile for a window, a door or the like. In a fifth aspect, the present invention relates to a fixed window. In a sixth aspect, the present invention relates to a kit for a frame and / or wing of a window, a door or the like. In a final aspect, the present invention relates to a method of manufacturing a structure for a window, a door or the like.

Description

IMPROVED CONSTRUCTION FOR A WINDOW, A DOOR OR THE LIKE COMPOSITE PROFILE, KIT AND METHOD OF MANUFACTURING IT

TECHNICAL DOMAIN

The present invention relates to an improved construction for a window, a door or the like, assembled profile, kit and method for fabricating it.

BACKGROUND

As is known, a window or door consists of a fixed frame in which a wing is hinged. The posts and beams of the fixed frame and of the wing are formed from composite profiles. Known composite profiles for wings of windows or doors comprise an inner shell and an outer shell, for example of aluminum, which are mutually attached by means of a thermal break.

The inner shell or outer shell of such profiles generally consists of a sleeve on which are provided on the side wall facing the thermal interruption protrusions or ribs which form a seat for this thermal interruption. The profiles are thus divided into different hollow chambers.

A problem with existing composite profiles is the less rigidity of the thermal breaks, which give rise to a less stable construction. It is also desired to limit the total depth of a window, door or the like.

There is a need for a more stable construction for a window, door or the like together with sufficient thermal insulation and slim design. * *

The present invention has an improved construction as an object as defined by claim 1, which offers a solution for at least one of the aforementioned disadvantages with windows, doors or the like.

SUMMARY OF THE INVENTION

The invention particularly relates to a construction for a window, a door or the like, which comprises a fixed frame and a movable wing, the fixed frame and the movable wing each comprising four composite profiles, each composite profile comprising an outer shell and a comprises inner shell which are connected by means of a thermal interruption, said thermal interruption of the frame extending over preferably 48% to 61%, more preferably 50% to 55%, most preferably about 52.5% of the frame depth and wherein the thermal break of the wing extends over 36% to 52%, more preferably 40% to 50%, most preferably over 43% to 47% of the wing depth as defined by claim 1.

These ratios allow a more optimal combination between the stability of the frame and the wing on the one hand and a more efficient thermal insulation for the window, door or the like on the other hand.

In a second aspect, the present invention relates to a frame for a window, a door, or the like, as defined by claim 19.

In a third aspect, the present invention relates to a wing for a window, a door or the like, as defined by claim 20.

In a fourth aspect, the present invention relates to a composite profile for a frame or a wing for a window, a door or the like, as defined by claim 21.

In a fifth aspect, the present invention relates to a fixed window, as defined by claim 22.

In a sixth aspect, the present invention relates to a kit of profiles and decision for a frame and / or for a wing for a window, a door or the like, as defined by claim 23.

In a final aspect, the present invention relates to a method for manufacturing a construction for a window, a door or the like, the method comprising the steps of: - extruding one or more inner shells, outer shells and thermal interruptions; - possibly extruding the extruded one or more inner shells and outer shells; - rolling in the inner shells, outer shells and thermal breaks into one or more composite profiles for a frame and / or a wing for a window, a door or the like, wherein said thermal break of the frame extends over preferably 48% to 61%, more preferably 50% to 55%, most preferably about 52.5% of the frame depth and that the thermal interruption of the wing extends over 36% to 52%, more preferably 40% to 50%, most preferably about 43% to 47% of the wing depth, as defined by claim 24.

Further preferred forms are elaborated in the sub-claims.

DESCRIPTION OF THE FIGURES

1-5 show a cross-sectional view of a closed window transverse to the longitudinal direction of the profiles of the frame and the wing, according to preferred forms of the invention.

DETAILED DESCRIPTION "A", "de" and "het" in this document refer to both the singular and the plural unless the context clearly presupposes otherwise. For example, "a seat" means one or more than one seat.

The terms "include", "comprising", "consist of", "consisting of", "provided with", "contain", "containing", "include", "including", "contents", "contents" are synonyms and are inclusive or open terms indicating the presence of what follows, and which do not preclude or preclude the presence of other components, features, elements, members, steps, known from or described in the prior art.

The citation of numerical intervals by the end points includes all integers, fractions and / or real numbers between the end points, including these end points.

When "about" or "round" is used in this document for a measurable quantity, a parameter, and the like, variations are meant of +/- 20% or less, preferably +/- 10% or less, more preferably +/- 5% or less, even more preferably +/- 1% or less, and even more preferably +/- 0.1% or less than and of the quoted value, insofar as such variations apply in the described invention. However, it must be understood here that the value of the quantity at which the term "about" or "round" is used is itself specifically disclosed.

Unless defined otherwise, all terms used in the description of the invention, including technical and scientific terms, have the meaning as generally understood by those skilled in the art of the invention.

By the term "outer shell" is meant in the present invention a semi-shell or profile, which is arranged in a composite profile on the outside of said construction. By the term "inner shell" is meant in the present invention a semi-shell or profile which is arranged in a composite profile on the outside of said construction. These inner shells and outer shells preferably concern a half-shell extruded from metal.

By the term "thermal break" is meant in the present invention two or more lanes which are suitable for effecting a thermal insulation between the inner and outer shell of a frame or wing. This thermal break preferably comprises polyamide or noryl.

The term "depth" in the present invention is understood to mean the distance according to which a part of the structure extends in the transverse direction to said structure, in the closed position.

The term "height" in the present invention is understood to mean the distance according to which a component of the structure extends transversely to the corresponding composite profile of said structure and perpendicular to the transverse direction to said structure, in the closed state.

The term "frame depth" in the present invention means the distance along which the frame extends in the depth direction.

The term "wing depth" in the present invention means the distance along which wing extends in the depth direction.

In the present invention, the term "frame height on the outside" means the distance according to the height direction of the side wall on the outside of the frame. The frame height on the inside then corresponds to the side wall on the inside of the frame.

In the present invention, the term "wing height on the outside" means the distance according to the height direction of the side wall on the outside of the wing. The wing height on the inside then corresponds to the side wall on the inside of the wing.

By the term "insulating strip" is meant in the present invention a strip which is suitable to be slid into an insulating strip and which comprises a well-insulating material or foam. Preferably, an insulation strip comprises EPS.

By the term "EPS" is meant expanded polystyrene in the present invention.

The term "inner glass seal" in the present invention is understood to mean a seal, which can preferably be removably attached to the click-glass lath of the wing and which is suitable for clamping and sealing the glazing between click-glass lath and outer shell of the wing.

By the term "outside welding service" is meant in the present invention a seal, which can preferably be removably attached to the outer shell of the wing and which is suitable for clamping and sealing the glazing between click glass lath and outer shell of the wing. wing.

Preferably, an inner glass seal or outer glass seal comprises EPDM (abbreviation of Ethylene-Propylene-diene monomer). By the term "EPDM" is meant in the present invention a synthetic rubber or elastomer obtained by the polymerization of ethylene (= ethylene), propylene (= propylene) and a diene.

In the present invention, the term "open-cell EPDM" becomes EPDM, which is provided with open cells, the material giving a spongy structure and a better insulating effect.

By the term "center seal" is meant in the present invention a seal which is provided on the thermal interruption of the frame and which extends towards the leaf when the leaf is closed.

In the present invention, the term "stop seal depth of the frame" is understood to mean the recess in the depth direction when the wing is closed, of the outer shell of the wing opposite the outer shell of the frame near the stop seal of the frame.

In the present invention, the term "stop seal depth of the wing" means the difference in depth when the wing is closed, between the inner shell of the wing and the inner shell of the frame.

By the term "click glass lath" is meant in the present invention a slat or profile which is suitable for fixing the glazing on the frame or the wing.

By the term "IMORYL" is meant in the present invention the material which is a composition of polyphenylene oxide and polystyrene.

By the term "TPE" is meant in the present invention a thermoplastic elastomer.

In the present invention, the term "rolling in" is understood to mean the folding over of at least one rib of an inner shell or outer shell in the direction of another rib for clamping a longitudinal edge of a lane of a thermal break in the groove formed by the ribs mentioned.

The term "stoving" in the present invention means the temperature curing or hardening of materials. Examples are wet paints and powder paints.

The term "fittings" in the present invention is understood to mean the hinges and locks, which parts are suitable for attaching a wing to a frame, whether or not it is mounted, so that it is movably arranged in the frame and whereby the wing can be closed or locked be in the framework. Typical components are handles, handles, self-drilling screws, slats, locking lugs, hinges, etc.

By the term "batter groove" is meant in the present invention a groove suitable for receiving batter therein. By the term "fitting groove depth" is meant the distance from the recess of the fitting groove according to the height direction of the wing. By the term "fitting groove width" is meant the distance of the width of the fitting groove according to the depth direction of the wing.

By the term "pressing angles" is meant in the present invention an L-shaped element, which is suitable to be placed in two composite profiles for a frame or wing, which lead to a reinforcement and fixing after pressing of the profiles in a corner.

By the term "fixed window" is meant in the present invention a window which does not comprise a movable wing. Preferably, the glazing is provided directly on the frame by means of a click-glass slat, wherein an outer glass seal is removably attached to the outer shell of the frame, an inner glass seal is removably attached to the click-glass slat, and which seals are suitable for securing the glazing clamping and sealing between click glass lath and outer shell of the frame. In an alternative preferred form, a wing is screwed into / on the frame. ♦ *

By the term "Uf value for a window" is meant in the present invention the heat transfer coefficient of the window profile, in accordance with the European standard EN ISO 10077-2. This value is expressed in W / (m2.K).

In a first aspect the invention relates to a construction for a window, a door or the like, which comprises a fixed frame and a movable wing, wherein the fixed frame and the movable wing each comprise four composite profiles, each composite profile comprising an outer shell and a comprises inner shell which are connected by means of a thermal interruption, said thermal interruption of the frame extending over preferably 48% to 61%, more preferably 50% to 55%, most preferably about 52.5% of the frame depth and wherein the thermal break of the wing extends over 36% to 52%, more preferably 40% to 50%, most preferably over 43% to 47% of the wing depth.

These ratios allow a better balance between the stability of the frame and the leaf, a more efficient thermal insulation for the window, door or the like and a sufficiently slim design of the structure.

In a preferred form of the invention, the said thermal interruptions comprise a first and a second lane, between which space is provided, which space is suitable for receiving an insulating strip.

This promotes thermal insulation for the window, door or the like.

In a preferred preferred form of the invention, the ratio between the depth of the second lane of the thermal break of the wing and the depth of the first lane of the thermal break of the wing is between 90% and 99%, preferably between 91 % and 95%, most preferably between 92% and 93%.

In a preferred form of the invention, the said construction is suitable for clamping a glazing between the outer shell of the wing and a click glass lath by means of an inner and an outer sealing, which is removably provided on the inner shell of the wing, the outer sealing being clamped between the outer shell of the wing and the glazing and whereby the inner glass seal is crimped between the glazing and the click glass lath. t

In a preferred preferred form of the invention, the ratio between the height of said click-glass lath and the height of the wing on the inside is between 20% and 35%, preferably between 21% and 30%, most preferably between 24 % and 27%.

This allows a better balance between the stability of the wing and sufficient space for placing the glazing.

In a preferred preferred form of the invention, said outside sealing means comprises a lip which extends towards the frame when the wing is closed, the ratio between the lip height of the outside sealing and the outside wing height at least 75%, preferably at least 78% , most preferably a minimum of 81%.

This promotes thermal insulation for the window, door or the like.

In a preferred form of the invention, the inner shank of the wing is provided with a fitting groove.

In a preferred preferred form of the invention, the ratio between the batter groove depth and the inside egg height is between 10% and 25%, preferably between 12% and 22%, most preferably between 15% and 20%.

In a preferred preferred form of the invention, the ratio between the fitting groove width and the depth of the inner shell of the wing is between 40% and 60%, preferably between 46% and 54%, most preferably between 48% and 52%.

In a preferred form of the invention, the outer shell of the frame is provided with a stop seal, which is suitable for making a sealing contact with the outer shell of the wing when the wing is closed.

This allows better separation of cold / heat from outside to / from the rooms within the profiles.

In a preferred preferred form of the invention, the ratio between the stop seal depth of the frame and the wing depth is between 5% and 10%, preferably between 6% and 9%, most preferably between 6.7% and 8.7%.

This offers a more optimal stop seal.

In a preferred form of the invention, the inner shell of the wing is provided with a stop seal, which is suitable for making a sealing contact with the inner shell of the frame when the wing is closed.

This allows better separation of cold / heat from the inside to and from the rooms within the profiles.

In a preferred preferred form of the invention, the ratio between the stop sealing depth of the wing and the frame depth is between 8% and 20%, preferably between 10% and 17%, most preferably between 10% and 15%.

This offers a more optimal stop seal.

In a preferred preferred form of the invention, said stop seals comprise EPDM.

In a preferred form of the invention, a thermal break of the frame is provided with a center seal which extends towards the wing and which is suitable for making a sealing contact with the thermal break of the wing when the wing is closed.

This offers an extra separation of rooms, which insulate cold / heat. This also promotes wind and water tightness.

In a preferred form of the invention, said thermal breaks include polyamide or noryl.

In a preferred form of the invention, said inner and outer shells comprise metal, preferably aluminum. More preferably, these comprise an EN-AW6060 alloy.

In a preferred form of the invention, bores are provided in the outer shell of the frame and in the outer shell of the wing, wherein the mutual distance of the bores of the outer shells in the depth direction is approximately equal to the stop sealing depth of the frame.

In a second aspect, the present invention relates to a frame for a window, a door, or the like.

In a third aspect, the present invention relates to a wing for a window, a door or the like.

In a fourth aspect, the present invention relates to a composite profile for a frame or a wing for a window, a door or the like.

In a fifth aspect, the present invention relates to a fixed window.

In a sixth aspect, the present invention relates to a kit of profiles and fittings for a frame and / or for a wing for a window, a door or the like.

In a final aspect, the present invention relates to a method for manufacturing a construction for a window, a door or the like, the method comprising the steps of: - extruding one or more inner shells, outer shells and thermal interruptions; - possibly extruding the extruded one or more inner shells and outer shells; - rolling in the inner shells, outer shells and thermal breaks into one or more composite profiles for a frame and / or a wing for a window, a door or the like, wherein said thermal break of the frame extends over preferably 48% to 61%, more preferably 50% to 55%, most preferably about 52.5% of the frame depth and that the thermal interruption of the wing extends over 36% to 52%, more preferably 40% to 50%, most preferably about 43% to 47% of the wing depth.

In a preferred form of the invention, the method further comprises: - processing said composite profiles by means of a milling and / or sawing process.

In a preferred form of the invention, the method further comprises: - the said composite profiles provided with pressing angles, glue and sealing kit; - pressing said profiles corner by corner into a complete frame and / or wing; - mounting fittings on the frame and / or the wing; - applying one or more seals to the wing and the frame; - assembling the wing and frame into a window, a door or the like; - the installation of glazing by means of an external glass seal, an inner glass seal and a click glass lath.

In a preferred form of the invention, the method further comprises: - packaging, transporting and placing said window, door or the like.

In the following, the invention is described a.d.h.v. non-limiting examples illustrating the invention, and which are not intended or may be interpreted to limit the scope of the invention. EXAMPLES:

Figure 1 shows a cross-sectional view of a closed aluminum window transversely of the longitudinal direction of the composite profiles of the frame and the wing, according to a preferred form of the invention.

The figure shows a cross section of a composite profile of a frame (1) and a wing (3) in closed condition. The composite profile of the frame (1) comprises outer shell (30) and inner shell (31) which are connected by the thermal break (2). The composite profile of the wing (3) comprises outer shell (25) and inner shell (26) which are connected by the thermal break (4). The outer and inner shells include the aluminum alloy EN-AW6060.

The ratio between the depth (D2) of said thermal break (2) of the frame (1) and the frame depth (D1) is approximately 52.5%. The ratio between the depth (D4a) of the thermal break (4) of the wing (3) and the wing depth (D3) is approximately 45.6%.

The construction comprises double glazing (16), wherein a gas (18) is provided between the 2 glass plates (17). The steel spacer (19) holds the glass plates (17) apart and is provided on the underside with sealing kit (20), which preferably comprises butyl. This spacer (19) can of course also be made in 'warm edge'.

The structure comprises an inner glass seal (11) and an outer glass seal (12) that clamp the glazing (16) between the outer shell (25) of the wing (3) and the click glass lath (8) in EN-AW6060. This click glazing is removably provided on the inside (34) of the window (clickable) on the inside shell (26) of the wing (3). The inner glass seal (11) is clamped between the click glass lath (8) and the glazing (16). The outer sealing (12) is clamped between the glazing (16) and the outer shell (25) of the wing (3). The outer glass seal (12) and the inner glass seal (11) from EPDM are provided with a spur or lip (22) that extends towards the frame (1) when the leaf (3) is closed.

Furthermore, the outer shell (30) of the frame is provided with an EPDM stop seal (10), which makes a sealing contact with the outer shell (25) of the wing (3). Boreholes (13) are provided in this outer shell (30) and in the outer shell (25) of the wing (3), which provide drainage and venting of the chambers of the frame (1) and the wing (3) on the outside (33) of the structure.

The inner shell (26) of the wing (3) is also provided with an EPDM stop seal (9), which makes a sealing contact with the inner shell (31) of the frame (1). The inner shell (26) of the wing (3) is also provided with a fitting groove (15).

The thermal break (2) of the frame (1) is provided with an acoustic middle seal (6) that extends towards the wing (3). This central seal (6) also makes a sealing contact with the thermal break (4) of the leaf (3). This promotes insulation towards both heat and sound. This includes TPE. The shape of the seal ensures a good drainage of seeping water to the drainage channels (13). In addition, there is the insulating middle seal (7), which is provided at the same thermal break (2). This includes a combination of TPE and open-cell EPDM.

The thermal break (2) of the frame (1) is provided on the other side with a sill seal (14). This ensures a waterproofing and that no contact is made with the hard stone of the sill.

The thermal break of the frame includes a first (2a) and second lane (2b) from Noryl. The thermal break of the wing comprises a first (4a) and second lane (4b) made of polyamide. An empty space is provided between the alleys (2a) and (2b), which space is suitable for receiving an insulating strip (32). An empty space is also provided between the alleys (4a) and (4b), which space is suitable for receiving an insulating strip (23).

This construction offers a Uf value of 1,837 W / (m2K).

Figure 2 shows the same cross-sectional view as in Figure 1, illustrating the dimensions mentioned in the present invention.

Figure 3 shows the same construction of a window as in Figures 1 and 2, wherein the insulating strips (23) and (32) are provided with EPS. This construction offers a Uf value of 1,660 W / (m2K).

Figure 4 shows a cross-sectional view of another closed aluminum window transversely of the longitudinal direction of the composite profiles of the frame and the wing, according to a preferred form of the invention.

The construction differs from that in Figures 1-3 by the triple glazing (16) with 3 glass plates (17) with two spacers (19) in between. The depth (D8) of the click glass lath (8) is smaller in accordance with the wider glazing (16). The construction comprises a thicker outer seal (12).

This construction offers a Uf value of 1,548 W / (m2K).

Figure 5 shows a cross-sectional view of another closed aluminum window transversely of the longitudinal direction of the composite profiles of the frame and the wing, according to a preferred form of the invention.

The construction is similar to Figure 4. However, it comprises an insulation strip (24) made of EPS and in the (cross-sectional) form of a comma, in the rafter of the wing (3). As a result, the inner glass seal (11) does not comprise a spur or lip as in previous figures 1-4. The inner shell (31), outer shell (30) and the thermal break (2) of the frame (1) are higher compared to the embodiment in Figures 1-4. This construction offers a Uf value of 1,390 W / (m2K).

It is believed that the present invention is not limited to the embodiments described above and that some modifications or changes can be added to the described examples without re-evaluating the appended claims. REFERENCE NUMBERS:

Frame (1)

First lane of the thermal break of the frame (2a)

Second lane of the thermal break of the frame (2b)

Wing (3)

First lane of the thermal break of the wing (4a)

Second lane of the thermal break of the wing (4b)

Acoustic middle seal (6)

Insulating center seal (7)

Stop seal of the wing (9)

Click glass lath (8)

Stop seal of the frame (10)

Inner glass seal (11)

Outer glass seal (12)

Hidden dewatering (13)

Door seal (14)

Hardware groove (15)

Glazing (16)

Glass plate (17)

Gas between glass plates (18)

Spacer (19)

Seal kit (20)

Lip of the inner glass seal (21)

Lip of the outside seal (22)

Insulation strip of the thermal break of the wing (23)

Insulation comma (24)

Outer shell of the wing (25)

Inner shell of the wing (26)

Outer scale of the frame (30)

Inner scale of the frame (31)

Insulation strip of the thermal break of the frame (32) Exterior of the window (33)

Inside of the window (34) * *

Claims (27)

CONCLUSIONS A construction for a window, a door or the like, which comprises a fixed frame (1) and a movable leaf (3), wherein the fixed frame (1) and the movable leaf (3) each comprise four composite profiles, each composite profile comprises an outer shell (25.30) and an inner shell (26, 31) which are connected by a thermal break (2,4), characterized in that said thermal break (2) of the frame (1) extends over preferably 48% to 61%, more preferably 50% to 55%, most preferably about 52.5% of the frame depth (D1) and that the thermal break (4) of the wing (3) extends over 36% up to 52%, more preferably 40% to 50%, most preferably over 43% to 47% of the wing depth (D3). A construction according to the preceding claim 1, characterized in that said thermal interruptions (2,4) comprise a first (2a, 4a) and a second lane (2b, 4b), between which space is provided, which space is suitable for to include an insulating strip (32.23). A construction according to the preceding claim 2, characterized in that the ratio between the depth (D4b) of the second lane (4b) of the thermal interruption of the wing (3) and the depth (D4a) of the first lane (4a ) of the thermal break of the wing (3) is between 90% and 99%, preferably between 91% and 95%, most preferably between 92% and 93%. A construction as claimed in any one of the preceding claims 1-3, characterized in that said construction is suitable for clamping a glazing (16) between the outer shell (25) of an inner (11) and an outer sealing (12) the wing (3) and a click glass lath (8), which is removably provided on the inner shell (26) of the wing (3), the outer sealing (12) being clamped between the outer shell (25) of the wing (3) ) and the glazing (16) and wherein the inner glass seal (11) is clamped between the glazing (16) and the click glass lath (8). Construction according to the preceding claim 4, characterized in that the ratio between the height (H8) of said click-glass slat (8) and the height (H3) of the wing (3) is on the inside (34) between 20% and 35%, preferably between 21% and 30%, most preferably between 24% and 27%. A construction as claimed in any one of the preceding claims 4-5, characterized in that said outer sealing (12) comprises a lip (22) which extends towards the frame (1) when the wing (3) is closed, the ratio between the lip height (H22) of the outside seal (12) and the wing height (H25) on the outside (33) is at least 75%, preferably at least 78%, most preferably at least 81%. A construction according to any one of the preceding claims 1-6, characterized in that the inner shell (26) of the wing (3) is provided with a fitting groove (15). A construction according to the preceding claim 7, characterized in that the ratio between the fitting groove depth (H15) and the wing height (H3) on the inside (34) is between 10% and 25%, preferably between 12% and 22% , most preferably between 15% and 20%. Construction according to one of the preceding claims 7 or 8, characterized in that the ratio between the fitting groove width (D15) and the depth (D26) of the inner shell (26) of the wing (3) is between 40% and 60 %, preferably between 46% and 54%, most preferably between 48% and 52%. A construction as claimed in any one of the preceding claims 1-9, characterized in that the outer shell (30) of the frame is provided with a stop seal (10), which is suitable for making a sealing contact with the outer shell (25) of the wing (3) when the wing (3) is closed. A construction according to the preceding claim 10, characterized in that the ratio between the stop sealing depth (D10) of the frame (1) and the wing depth (D3) is between 5% and 10%, preferably between 6% and 9% , most preferably between 6.7% and 8.7%. A construction as claimed in any one of the preceding claims 1-11, characterized in that the inner shell (26) of the wing (3) is provided with a stop seal (9), which is suitable for making a sealing contact with the inner shell (31). ) of the frame (1) when the wing (3) is closed. A construction according to the preceding claim 12, characterized in that the ratio between the stop sealing depth (D9) of the wing (3) and the frame depth (D1) is between 8% and 20%, preferably between 10% and 17% , most preferably between 10% and 15%. A construction as claimed in any one of the preceding claims 10-13, characterized in that said stop seals (9, 10) comprise EPDM. A construction as claimed in any one of the preceding claims 1-14, characterized in that a thermal break (2) of the frame (1) is provided with a central seal (6) which extends towards the wing (3) and which is suitable a sealing contact can be made with the thermal break (4) of the leaf (3) when the leaf (3) is closed. A construction according to any one of the preceding claims 1-15, characterized in that said thermal interruptions (2,4) comprise polyamide or noryl. A construction as claimed in any one of the preceding claims 1-16, characterized in that said inner (26.31) and outer shells (25.30) comprise metal, preferably aluminum. A construction as claimed in any one of the preceding claims 1-17, characterized in that bores (13) are provided in the outer shell (30) of the frame (1) and in the outer shell (25) of the wing (3), wherein the mutual distance (D13) of the bores (13) of the outer shells (30) and (25) in the depth direction is approximately equal to the stop sealing depth (D10) of the frame (1). 19. Frame (1) for a window, door or the like according to any one of the preceding claims 1-18 wherein the frame (1) comprises four composite profiles, each composite profile comprising an outer shell (25) and an inner shell (26) be connected by means of a thermal break (2), characterized in that said thermal break (2) of the frame (1) extends over preferably 48% to 61%, more preferably 50% to 55%, most preferably preferably about 52.5% of the frame depth (D1). A wing (3) for a window, a door or the like according to any one of the preceding claims 1-18 wherein the movable wing (3) comprises four composite profiles, each composite profile comprising an outer shell (30) and an inner shell (31) which are connected by a thermal break (4), characterized in that the thermal break (4) of the wing (3) extends over 36% to 52%, more preferably 40% to 50%, most preferably over 43% to 47% of the wing depth (D3). Composite profile for a frame (1) according to the preceding claim 19 or a wing (3) according to the preceding claim 20 A fixed window provided with a frame (1) according to the preceding claim 19. Kit of profiles and fittings for a frame (1) according to preceding claim 19 and / or for a wing (3) according to preceding claim 20. Method for manufacturing a construction for a window, a door or the like according to one of the preceding claims 1-18, characterized in that the method comprises the following steps: - extruding one or more inner shells (26,31) , outer shells (25.30) and thermal breaks (2.4); - possibly muffling the extruded one or more inner shells (26,31) and outer shells (25,30); - rolling in the inner shells (26,31), outer shells (25,30) and thermal breaks (2,4) into one or more composite profiles for a frame (1) and / or a wing (3) for a window, a door or the like, characterized in that said thermal break (2) of the frame (1) extends over preferably 48% to 61%, more preferably 50% to 55%, most preferably about 52.5% of the frame depth (D1) and that the thermal break (4) of the wing (3) extends over 36% to 52%, more preferably 40% to 50%, most preferably over 43% to 47% of the wing depth ( D3). Method according to the preceding claim 24, characterized in that the method further comprises: - processing said composite profiles by means of a milling and / or sawing process. A method according to any one of the preceding claims 24 or 25, characterized in that the method further comprises: - said composite profiles provided with pressing angles, glue and sealing kit; - pressing said profiles corner by corner into a complete frame (1) and / or a wing (3); - mounting fittings on the frame (1) and / or the wing (3); - applying one or more seals to the wing (1) and the frame (3); - assembling the wing (1) and the frame (3) into a window, a door or the like; - the installation of glazing by means of an external glass seal, an inner glass seal and a click glass lath. A method according to any one of the preceding claims 24-26, characterized in that the method further comprises: packaging, transporting and placing said window, door or the like.