A kind of Cast-in-place concrete rib shuttering member
The application for the applying date be that December 16, application number in 2002 are 02156278.4, name is called the dividing an application of application for a patent for invention of " a kind of Cast-in-place concrete rib shuttering member ".
(1) technical field
The present invention relates to a kind of Cast-in-place concrete rib shuttering member.
(2) background technology
At present, in some civilian construction or decorative engineering, need pour into a mould the two-way girt strip of Cast-in-place concrete sometimes, during construction, all be to adopt the template formwork, carry out the concrete cast again and form, this form of construction work, time-consuming, bother very much, therefore, adopted the circular die in four directions to support afterwards, again pour concrete, solved the problems referred to above preferably, speed of application is accelerated greatly.Along with the use of two-way girt strip in engineering, the bottom surface of finding girt strip easily produces the crack, and the material consumption of girt strip is also bigger, therefore, for addressing the above problem, the designer has been designed to the inverted T shape girt strip with girt strip, has solved the problem of easy generation crack, high material consumption preferably, simultaneously, also increased the effect of decorating to a certain extent.For this reason, develop a kind of novel Cast-in-place concrete rib shuttering member, accelerate speed of application for being badly in need of.
(3) summary of the invention
The object of the present invention is to provide a kind of Cast-in-place concrete rib shuttering member, can accelerate speed of application, reduce construction cost, simultaneously, also have intensity height, simple in structure, characteristics such as manufacturing is simple and easy, cost is low.
Solution of the present invention is on the basis of existing technology, comprise annular stomach wall, it is characterized in that being provided with edge of a wing inwall and edge of a wing sidewall at an end of at least one side of annular stomach wall, link into an integrated entity by edge of a wing inwall between annular stomach wall and the edge of a wing sidewall, there is at least one adherent bracing boom annular stomach wall inboard.Like this, because the end at least one side of annular stomach wall is provided with edge of a wing inwall and edge of a wing sidewall, link into an integrated entity by edge of a wing inwall between annular stomach wall and the edge of a wing sidewall, edge of a wing inwall extends to shuttering member inside with respect to annular stomach wall, edge of a wing sidewall extends to the shuttering member outside with respect to edge of a wing inwall, thereby when construction, can form the rib and the edge of a wing template of inverted T shape girt strip, can once form the inverted T shape girt strip after the concrete cast, and formwork is simple, speed of application is fast, the efficient height, construction cost is low, there is at least one adherent bracing boom annular stomach wall inboard, and the intensity and the rigidity of shuttering member are bigger, thereby have reached purpose of the present invention.Simultaneously, shuttering member also has intensity height, simple in structure, easy to manufacture, characteristics such as cost is low, is applicable to two-way ribbed slab floor, and engineerings such as hollow arch without beam, hyollow foundation base plate, hollow wall and hollow bridges are used.
Feature of the present invention is that also at least two adherent bracing booms are parallel.Like this, the intensity of shuttering member and rigidity are bigger.
Feature of the present invention is that also adherent bracing boom is a vertical stiffener.Like this, the intensity of shuttering member and rigidity are bigger.
Feature of the present invention is that also adherent bracing boom is parallel.Like this, the intensity of shuttering member and rigidity are bigger.
Feature of the present invention is that also an end of annular stomach wall is provided with edge of a wing inwall and edge of a wing sidewall all around.Like this, all pourable one-tenth inverted T shape of all girt strips girt strip makes things convenient for selecting for use of design and construction unit, helps accelerating speed of application, reduces construction cost.
The other end that feature of the present invention also is at one end to be provided with the annular stomach wall of edge of a wing inwall and edge of a wing sidewall is provided with edge of a wing inwall.Like this,, can prevent effectively that annular stomach wall from destroying, also make things convenient on annular stomach wall simultaneously to lay panel because edge of a wing inwall is set.
Feature of the present invention also is at one end to be provided with on the edge of a wing inwall of the other end of annular stomach wall of edge of a wing inwall and edge of a wing sidewall and is connected with edge of a wing sidewall.Like this, the Cast-in-place concrete rib of pourable one-tenth I shape can make things convenient for design and construction unit to select for use between the shuttering member.
Feature of the present invention also is to be connected with the edge of a wing outer wall parallel with edge of a wing inwall in the edge of a wing of annular stomach wall side wall ends, and edge of a wing inwall, edge of a wing sidewall and edge of a wing outer wall surround outwardly open flute profile.Like this, can save T type girt strip edge of a wing soffit formwork, accelerate speed of application, reduce construction cost.
Feature of the present invention is that also edge of a wing outer wall stretches out outside the annular stomach wall.Like this, can omit the soffit formwork of T type girt strip fully, reduce construction cost, accelerate speed of application.
Feature of the present invention also is all to be connected with the edge of a wing outer wall parallel with edge of a wing inwall on the upper and lower edge of a wing sidewall of annular stomach wall, and edge of a wing inwall, edge of a wing sidewall and edge of a wing outer wall surround outwardly open flute profile.Like this, the girt strip of pourable one-tenth I shape between the shuttering member, and the upper and lower edge of a wing and shuttering member are combined with each other.
Feature of the present invention is that also at least one side of annular stomach wall is provided with at least one groove.Like this, can form the reinforcing rib of girt strip in the groove, and improve the crowded effect of mutual embedding between shuttering member and the Cast-in-place concrete, improve globality.
Feature of the present invention is that also described groove is parallel or crossing each other.Like this, the mutual embedding between shuttering member and the Cast-in-place concrete is squeezed effect better, and globality is higher, and intensity is bigger.
Feature of the present invention is that also annular stomach wall is provided with the module of protrusion or at least one in the pothole.Like this, effect is squeezed in the mutual embedding that has improved between shuttering member and the Cast-in-place concrete.
Feature of the present invention is that also annular stomach wall is provided with at least one in bracing boom, reinforcing rib or the stiffening rib.Like this, the intensity of shuttering member and rigidity are bigger.
Feature of the present invention is that also the opening part of annular stomach wall opening and edge of a wing sidewall is provided with dismounting or movable hush panel.Like this, support during convenient construction, simultaneously, also can save making up and use.
Feature of the present invention is that also the opening of annular stomach wall and the opening part of edge of a wing sidewall have the permanent sealing plate that is attached thereto.Like this, support during convenient construction, simultaneously, also can save making up and use.
Feature of the present invention is that also edge of a wing inwall and edge of a wing sidewall are linked to be arc or skew lines or broken line or double camber.Like this, make things convenient for design and construction unit to select for use, help accelerating speed of application, reduce construction cost.
Feature of the present invention is that also annular stomach wall is provided with connector.Like this, make things convenient for shuttering member when construction, to interconnect each other, accelerate speed of application.
Feature of the present invention is that also at least two shuttering members connect into the shuttering member of disjunctor by the connector on the annular stomach wall.Like this, construction is more convenient, quick.
Feature of the present invention also be annular stomach wall be global formation or polylith is put together.Like this, make things convenient for design and construction unit to select, help reducing construction cost.
Feature of the present invention also be hush panel be global formation or polylith is put together.Like this, make things convenient for design and construction unit to select, help reducing construction cost.
Feature of the present invention is that also annular stomach wall horizontal section outline is circular, ellipse, polygon or above-mentioned combination.Like this, shuttering member is wide in variety, can make things convenient for design and construction unit to select, and helps reducing construction cost.
Feature of the present invention is that also annular stomach wall horizontal section outline is inner corner trim polygon, arc angle polygon, curve polygon or above-mentioned combination.
Feature of the present invention is that also described groove is the step groove.Like this, during the concrete cast, concrete easily enters in the groove, is beneficial to the quality that guarantees concrete, and simultaneously, concentration phenomenon also can eliminate stress.
Feature of the present invention is that also edge of a wing inwall is a step.Like this, during the concrete cast, concrete easily enters in the groove, is beneficial to the quality that guarantees concrete.
Feature of the present invention also is to be provided with in the cavity that annular stomach wall and hush panel surround at least one in bracing boom, reinforcing rib or the stiffening rib.Like this, the intensity of shuttering member and rigidity are bigger.
Feature of the present invention is that also the Cast-in-place concrete rib is applied to hollow arch without beam with shuttering member.
Feature of the present invention is that also the Cast-in-place concrete rib is applied to hollow building cover with shuttering member.
Feature of the present invention is that also the Cast-in-place concrete rib is applied to hollow roof system with shuttering member.
Feature of the present invention is that also the Cast-in-place concrete rib is applied to the hyollow foundation base plate with shuttering member.
Feature of the present invention is that also the Cast-in-place concrete rib is applied to hollow wall with shuttering member.
Feature of the present invention is that also the Cast-in-place concrete rib is applied to hollow bridges with shuttering member.
(4) description of drawings
Fig. 1 is the structural representation of the embodiment of the invention 1.In the accompanying drawing, 1 is annular stomach wall, and 2 is edge of a wing inwall, and 3 is edge of a wing sidewall, in each accompanying drawing, numbers identically, and its explanation is identical.As shown in Figure 1, be provided with edge of a wing inwall 2 and edge of a wing sidewall 3, link into an integrated entity by edge of a wing inwall 2 between annular stomach wall 1 and the edge of a wing sidewall 3 at an end of two sides of annular stomach wall 1.
Fig. 2 is the structural representation of the embodiment of the invention 2, is provided with edge of a wing inwall 2 and edge of a wing sidewall 3 around the end of its annular stomach wall 1.
Fig. 3 is the structural representation of the embodiment of the invention 3, and its other end that is provided with the annular stomach wall 1 of edge of a wing inwall 2 and edge of a wing sidewall 3 is provided with edge of a wing inwall 2.
Fig. 4 is the structural representation of the embodiment of the invention 4, and it is provided with on the edge of a wing inwall 2 of the other end of annular stomach wall 1 of edge of a wing inwall 2 and edge of a wing sidewall 3 and is connected with edge of a wing sidewall 3.
Fig. 5 is the structural representation of the embodiment of the invention 5, is connected with the edge of a wing outer wall 4 parallel with edge of a wing inwall 2 on the edge of a wing sidewall 3 of its annular stomach wall 1, and edge of a wing inwall 2, edge of a wing sidewall 3 surround outwardly open flute profile with edge of a wing outer wall 4.
Fig. 6 is the structural representation of the embodiment of the invention 6, and its edge of a wing outer wall 4 stretches out outside the annular stomach wall 1.
Fig. 7 is the structural representation of the embodiment of the invention 7, all is connected with the edge of a wing outer wall 4 parallel with edge of a wing inwall 2 on the upper and lower edge of a wing sidewall 3 of its annular stomach wall 1, and edge of a wing inwall 2, edge of a wing sidewall 3 surround outwardly open flute profile with edge of a wing outer wall 4.
Fig. 8 is the structural representation of the embodiment of the invention 8, and two sides of its annular stomach wall 1 are provided with groove 5.
Fig. 9 is the structural representation of the embodiment of the invention 9, and two sides of its annular stomach wall 1 are provided with crossing groove 5.
Figure 10 is the structural representation of the embodiment of the invention 10, and its annular stomach wall 1 is provided with the module 6 of protrusion.
Figure 11 is the structural representation of the embodiment of the invention 11, and its annular stomach wall 1 is provided with pothole 7.
Figure 12 is the structural representation of the embodiment of the invention 12, and its annular stomach wall 1 is provided with reinforcing rib 9.
Figure 13 is the structural representation of the embodiment of the invention 13, and its annular stomach wall 1 is provided with bracing boom 8.
Figure 14 is the structural representation of the embodiment of the invention 14, and its annular stomach wall 1 is provided with stiffening rib 10.
Figure 15 is the structural representation of the embodiment of the invention 15, and the opening 11 of its annular stomach wall 1 is provided with movable and dismountable hush panel 13 respectively with opening 12 places of edge of a wing sidewall 3.
Figure 16 is the structural representation of the embodiment of the invention 16, and the opening 11 of its annular stomach wall 1 is provided with the permanent sealing plate 14 that is attached thereto respectively with opening 12 places of edge of a wing sidewall 3.
Figure 17 is the structural representation of the embodiment of the invention 17, and its edge of a wing inwall 2 is linked to be arc with edge of a wing sidewall 3.
Figure 18 is the structural representation of the embodiment of the invention 18, and its annular stomach wall 1 is provided with drag hook type connector 15.Connector 15 also can be inserted link, jack, cutting ferrule, welded reinforcement, module, tube connector etc.
Figure 19 is the structural representation of the embodiment of the invention 19, and its 4 shuttering members connect into the shuttering member of disjunctor by the tube connector 15 on the annular stomach wall 1.
Figure 20 is the structural representation of the embodiment of the invention 20, and its annular stomach wall 1 is put together for polylith.
Figure 21 is the structural representation of the embodiment of the invention 21, and its hush panel 13,14 is put together for polylith.
Figure 22 is the structural representation of the embodiment of the invention 22, and its groove 5 is the step groove.
Figure 23 is the structural representation of the embodiment of the invention 23, and its edge of a wing inwall 2 is a step.
Figure 24 is the structural representation of the embodiment of the invention 24, is provided with stiffening rib 10 in the cavity that its annular stomach wall 1 and hush panel 14 surround.
Figure 25 is the structural representation of the embodiment of the invention 25, is provided with bracing boom 8 and reinforcing rib 9 in the cavity that its annular stomach wall 1 and hush panel 14 surround.
(5) specific embodiment
The present invention is further illustrated below in conjunction with drawings and Examples.
The present invention as shown in drawings, comprise annular stomach wall 1, it is characterized in that being provided with edge of a wing inwall 2 and edge of a wing sidewall 3 at an end of at least one side of annular stomach wall 1, link into an integrated entity by edge of a wing inwall 2 between annular stomach wall 1 and the edge of a wing sidewall 3, there is at least one adherent bracing boom 8 annular stomach wall 1 inboard.Fig. 1 is the structural representation of the embodiment of the invention 1.In the accompanying drawing, 1 is annular stomach wall, and 2 is edge of a wing inwall, and 3 is edge of a wing sidewall, and 8 is bracing boom, in each accompanying drawing, numbers identically, and its explanation is identical.As shown in Figure 1, end in two sides of annular stomach wall 1 is provided with edge of a wing inwall 2 and edge of a wing sidewall 3, link into an integrated entity by edge of a wing inwall 2 between annular stomach wall 1 and the edge of a wing sidewall 3, to the inner extension of shuttering member, edge of a wing sidewall 3 extends to the shuttering member outside with respect to edge of a wing inwall 2 edge of a wing inwall 2 with respect to annular stomach wall 1.As shown in Figure 8, there is adherent bracing boom 8 its annular stomach wall 1 inboard.
Feature of the present invention is that also at least two adherent bracing booms 8 are parallel.As shown in Figure 8, its two adherent bracing booms 8 are parallel.
Feature of the present invention is that also adherent bracing boom 8 is vertical stiffener.As shown in Figure 8, its adherent bracing boom 8 is a vertical stiffener.
Feature of the present invention is that also adherent bracing boom 8 is parallel.As shown in Figure 8, its adherent bracing boom 8 is parallel.
Feature of the present invention is that also an end of annular stomach wall 1 is provided with edge of a wing inwall 2 and edge of a wing sidewall 3 all around.Fig. 2 is the structural representation of the embodiment of the invention 2, is provided with edge of a wing inwall 2 and edge of a wing sidewall 3 around the end of its annular stomach wall 1.
The other end that feature of the present invention also is at one end to be provided with the annular stomach wall 1 of edge of a wing inwall 2 and edge of a wing sidewall 3 is provided with edge of a wing inwall 2.Fig. 3 is the structural representation of the embodiment of the invention 3, and its other end that is provided with the annular stomach wall 1 of edge of a wing inwall 2 and edge of a wing sidewall 3 is provided with edge of a wing inwall 2.
Feature of the present invention also is at one end to be provided with on the edge of a wing inwall 2 of the other end of annular stomach wall 2 of edge of a wing inwall 2 and edge of a wing sidewall 3 and is connected with edge of a wing sidewall 3.Fig. 4 is the structural representation of the embodiment of the invention 4, and it is provided with on the edge of a wing inwall 2 of the other end of annular stomach wall 1 of edge of a wing inwall 2 and edge of a wing sidewall 3 and is connected with edge of a wing sidewall 3.
Feature of the present invention also is to be connected with in sidewall 3 ends, the edge of a wing of annular stomach wall 1 edge of a wing outer wall 4 parallel with edge of a wing inwall 2, and edge of a wing inwall 2, edge of a wing sidewall 3 surround outwardly open flute profile with edge of a wing outer wall 4.Fig. 5 is the structural representation of the embodiment of the invention 5, and edge of a wing sidewall 3 ends of its annular stomach wall 1 are connected with the edge of a wing outer wall 4 parallel with edge of a wing inwall 2, and edge of a wing inwall 2, edge of a wing sidewall 3 surround outwardly open flute profile with edge of a wing outer wall 4.
Feature of the present invention is that also edge of a wing outer wall 4 stretches out outside the annular stomach wall 1.Fig. 6 is the structural representation of the embodiment of the invention 6, and its edge of a wing outer wall 4 stretches out outside the annular stomach wall 1.
Feature of the present invention also is all to be connected with the edge of a wing outer wall 4 parallel with edge of a wing inwall 2 on the upper and lower edge of a wing sidewall 3 of annular stomach wall 1, edge of a wing inwall 2, edge of a wing sidewall 3 surround outwardly open flute profile with edge of a wing outer wall 4.Fig. 7 is the structural representation of the embodiment of the invention 7, all is connected with the edge of a wing outer wall 4 parallel with edge of a wing inwall 2 on the upper and lower edge of a wing sidewall 3 of its annular stomach wall 1, and edge of a wing inwall 2, edge of a wing sidewall 3 surround outwardly open flute profile with edge of a wing outer wall 4.
Feature of the present invention is that also at least one side of annular stomach wall 1 is provided with at least one groove 5.Fig. 8 is the structural representation of the embodiment of the invention 8, and two sides of its annular stomach wall 1 are provided with groove 5.
Feature of the present invention is that also described groove 5 is parallel or crossing each other.Fig. 9 is the structural representation of the embodiment of the invention 9, and two sides of its annular stomach wall 1 are provided with crossing groove 5.
Feature of the present invention is that also annular stomach wall 1 is provided with the module 6 of protrusion or at least one in the pothole 7.Figure 10 is the structural representation of the embodiment of the invention 10, and its annular stomach wall 1 is provided with the module 6 of protrusion.Figure 11 is the structural representation of the embodiment of the invention 11, and its annular stomach wall 1 is provided with pothole 7.
Feature of the present invention is that also annular stomach wall 1 is provided with at least one in bracing boom 8, reinforcing rib 9 or the stiffening rib 10.Figure 12 is the structural representation of the embodiment of the invention 12, and its annular stomach wall 1 is provided with reinforcing rib 9.Figure 13 is the structural representation of the embodiment of the invention 13, and its annular stomach wall 1 is provided with bracing boom 8.Figure 14 is the structural representation of the embodiment of the invention 14, and its annular stomach wall 1 is provided with stiffening rib 10.
Feature of the present invention is that also opening 12 places of annular stomach wall 1 opening 11 and edge of a wing sidewall 3 are provided with dismounting or movable hush panel 13.Figure 15 is the structural representation of the embodiment of the invention 15, and the opening 11 of its annular stomach wall 1 is provided with movable and dismountable hush panel 13 respectively with opening 12 places of edge of a wing sidewall 3.
Feature of the present invention is that also there is the permanent sealing plate 14 that is attached thereto at the opening 11 of annular stomach wall 1 and opening 12 places of edge of a wing sidewall 3.Figure 16 is the structural representation of the embodiment of the invention 16, and the opening 11 of its annular stomach wall 1 is provided with the permanent sealing plate 14 that is attached thereto respectively with opening 12 places of edge of a wing sidewall 3.
Feature of the present invention is that also edge of a wing inwall 2 and edge of a wing sidewall 3 are linked to be arc or skew lines or broken line or double camber.Figure 17 is the structural representation of the embodiment of the invention 17, and its edge of a wing inwall 2 is linked to be arc with edge of a wing sidewall 3.
Feature of the present invention is that also annular stomach wall 1 is provided with connector 15.Figure 18 is the structural representation of the embodiment of the invention 18, and its annular stomach wall 1 is provided with drag hook type connector 15.Connector 15 also can be inserted link, jack, cutting ferrule, welded reinforcement, module, tube connector etc.
Feature of the present invention is that also at least two shuttering members connect into the shuttering member of disjunctor by the connector 15 on the annular stomach wall 1.Figure 19 is the structural representation of the embodiment of the invention 19, and its 4 shuttering members connect into the shuttering member of disjunctor by the tube connector 15 on the annular stomach wall 1.
Feature of the present invention also be annular stomach wall 1 for global formation or polylith is put together.To shown in Figure 5, annular stomach wall 1 is a global formation as Fig. 1.Figure 20 is the structural representation of the embodiment of the invention 20, and its annular stomach wall 1 is put together for polylith.
Feature of the present invention also be hush panel 13,14 for global formation or polylith is put together.Figure 21 is the structural representation of the embodiment of the invention 21, and its hush panel 13,14 is put together for polylith.
Feature of the present invention is that also annular stomach wall horizontal section outline is circular, ellipse, polygon or above-mentioned combination.As Fig. 1 to Figure 21, its annular stomach wall horizontal section outline is square (quadrangle).
Feature of the present invention is that also annular stomach wall horizontal section outline is inner corner trim polygon, arc angle polygon, curve polygon or above-mentioned combination.
Feature of the present invention is that also described groove 5 is the step groove.Figure 22 is the structural representation of the embodiment of the invention 22, and its groove 5 is the step groove.
Feature of the present invention is that also edge of a wing inwall 2 is step.Figure 23 is the structural representation of the embodiment of the invention 23, and its edge of a wing inwall 2 is a step.
Feature of the present invention also is to be provided with in the cavity that annular stomach wall 1 and hush panel 13,14 surround at least one in bracing boom 8, reinforcing rib 9 or the stiffening rib 10.Figure 24 is the structural representation of the embodiment of the invention 24, is provided with stiffening rib 10 in the cavity that its annular stomach wall 1 and hush panel 14 surround.Figure 25 is the structural representation of the embodiment of the invention 25, is provided with bracing boom 8 and reinforcing rib 9 in the cavity that its annular stomach wall 1 and hush panel 14 surround.
Feature of the present invention is that also the Cast-in-place concrete rib is applied to hollow arch without beam with shuttering member.
Feature of the present invention is that also the Cast-in-place concrete rib is applied to hollow building cover with shuttering member.
Feature of the present invention is that also the Cast-in-place concrete rib is applied to hollow roof system with shuttering member.
Feature of the present invention is that also the Cast-in-place concrete rib is applied to the hyollow foundation base plate with shuttering member.
Feature of the present invention is that also the Cast-in-place concrete rib is applied to hollow wall with shuttering member.
Feature of the present invention is that also the Cast-in-place concrete rib is applied to hollow bridges with shuttering member.
During the invention process, can adopt glass fiber cement mortar or the ferro-cement disposable shuttering member that is made in former.