Patent Application
20140013825
The present invention relates to an apparatus and method for testing air permeability, and more specifically to an apparatus and method for testing air permeability of a test sample on thickness direction of a resin matrix composite material layer by using air as a test fluid.
Permeability is a parameter characterizing difficulty of a fluid flowing through a porous medium under a pressure. The greater the permeability is, the smaller a resistance of the porous material against flow of the fluid will be. During preparation of a resin matrix composite material by using an autoclave or a vacuum bag process, permeability of a prepreg layer is one of crucial factors affecting discharge of entrained air and volatile components under the action of vacuum, and therefore affects the forming quality of members made of the composite material to a certain degree. A prepreg system comprises a fiber reinforcement and a resin substrate. Hence, the permeability of the prepreg layer is substantially different from that of a fiber layer. The permeability of the prepreg layer not only depends on physical properties and fiber network structure, but also is related to physical properties of the resin substrate. In recent years, permeability of the fiber layer has already became a focus of study in the field of composite material. However, methods for testing the permeability of the prepreg layer of the resin matrix composite material are seldom reported. This is mainly because the test of permeability of the prepreg layer is confronted with certain difficulties, for example, (1) the prepreg system contains the resin substrate; if the liquid is used as a test fluid, a flow front is difficult to be judged and permeability cannot be accurately tested; (2) test of permeability of the prepreg layer by using air imposes higher requirements for the sealing of the testing apparatus; (3) due to a gap between the prepreg layer and a test mold, air flows in the gap so that a large testing deviation is caused; (4) during solidification, the prepreg layer is affected by temperature and pressure, so it is difficult to achieve the test of the permeability during the solidification. As can be seen from the above, designs of the apparatus and method for testing the air permeability of the prepreg layer are of important theoretical significance and high application value, and will confront with a certain technical difficulty, that is, accurate measurement cannot be achieved unless influences from many factors are taken into consideration together.
To overcome the technical problem in the prior art that there is difficulty in using air as fluid to test the permeability of a resin matrix composite material layer to be tested, particularly the permeability in the thickness direction of the prepreg layer, the present invention provides a testing apparatus for testing air permeability in a thickness direction. Preferably, the apparatus is applied to the test of permeability of a prepreg in a resin matrix composite material. The apparatus achieves the test of air permeability of the prepreg layer in the thickness direction by providing a power enabling air to move in the thickness direction of the prepreg layer in a vacuum cavity. Measurement of the air permeability of the prepreg in a solidifying process can be achieved by regulating pressure and temperature.
The present invention provides a testing apparatus for testing air permeability in a thickness direction of a resin matrix composite material layer, comprising: a mold at least comprising a cavity and a cover plate sealed airtight with a cavity wall of the cavity, a loading device for controlling a test pressure, a temperature control device for controlling a test temperature, a vacuum suction device for vacuumize the cavity, and a flow detection element for detecting air flow, wherein the cover plate has a receiving through hole in which an upper permeable sheet and a lower permeable sheet are received, the loading device being adapted to press the upper permeable sheet, a test sample to be tested being laid flatly between the upper permeable sheet and the lower permeable sheet; an air inlet and an air outlet being arranged on the cavity in an up-down direction of the cavity corresponding to the upper permeable sheet and the lower permeable sheet, respectively; wherein the air inlet is communicated with the flow detection element and the air outlet is communicated with the vacuum suction device, and wherein after the vacuum suction device is started to make the pressure at the air inlet higher than the pressure at the air outlet, air flows from the air inlet, through the upper permeable sheet, through the test sample in the thickness direction of the resin matrix composite material layer of the test sample, and then out of the air outlet through the lower permeable sheet.
Specifically, the control temperature device at least comprises a heating rod.
Specifically, the vacuum suction device is a vacuum pump.
Preferably, a vacuum gauge is provided between the vacuum pump and the air outlet.
Preferably, the upper permeable sheet and/or lower permeable sheet are made of a porous material.
Specifically, the loading device comprises a loading flat panel and a loading body, wherein the loading flat panel is located on the upper permeable sheet, and the loading body applies a pressure to the loading flat panel.
Alternatively, the cavity is provided with cavity air guide recesses which are adjacent to the inner wall of the cavity and used as a circulation passage of air after the air passes through the lower permeable sheet and before it enters the air outlet.
Alternatively, cover plate air guide recesses are provided at the edge of the receiving through hole of the cover plate by which the air flows from the air inlet and through the upper permeable sheet.
Alternatively, the test sample to be tested is a prepreg.
Alternatively, the test sample to be tested is laid flatly between the upper permeable sheet and the lower permeable sheet in a uni-directional laying manner, an orthogonal laying manner, or a quasi-isotropic laying manner.
The testing apparatus for testing air permeability of the prepreg layer in the thickness direction according to the present invention has the following advantages: (1) accurate test of the air permeability of the prepreg layer in the thickness direction can be achieved under different pressure and temperature conditions; (2) the apparatus is adapted for a prepreg of various continuous fibers such as glass fiber, carbon fiber and aramid fiber, as well as for a prepreg of various fabrics; (3) the apparatus can achieve measurement of the air permeability of the prepreg which is laid in different laying manners or laid with different numbers of layers; (4) the apparatus exhibits a small measurement error, a high test reliability and a high repeatability; (5) the apparatus is simple, easily operable and time-saving.
The present invention further provides a method for measuring air permeability in a thickness direction of a resin matrix composite material layer, comprising the following steps:
(1) sealing the air inlet of the mold and starting the vacuum suction device communicated with the air outlet of the mold to inspect whether there is air leakage;
(2) applying a test pressure to the upper permeable sheet and the lower permeable sheet received in the receiving through hole of the cover plate of the mold by the loading device, if the inspection result in step (1) is no air leakage, under a condition of with or without the test sample to be tested, and measuring a thickness h of the test sample;
(3) setting a pressure of the vacuum suction device as P to form a differential pressure between the air outlet and the air inlet so as to enable the air to flow, setting the pressure of the test sample as a test pressure corresponding to the thickness h of step (2) via the loading device, setting a temperature of the cavity as a test temperature T via the temperature control device and obtaining a corresponding air viscosity η via a temperature-viscosity formula, and detecting an air flow rate Q via the flow detection element;
(4) calculating the permeability in the thickness direction according to a permeability calculating formula.
Specifically, the temperature-viscosity formula is
wherein T0 and η0 represent a reference temperature and a corresponding viscosity, respectively, and C represents a constant related to air type.
Specifically, the permeability calculating formula is
wherein l and b represent a length and a width of the layer of the test sample, respectively.
Preferably, the step (1) further comprises a step of sealing the loading device and the cover plate and inspecting whether there is air leakage.
Preferably, the step (1) further comprises a step of sealing the cavity and the loading device and inspecting whether there is air leakage.
Specifically, in the step (1), the vacuum suction device sets the pressure of the cavity as −0.1 MPa; if no pressure relief occurs after the vacuum suction device is switched off, there is no air leakage.
Specifically, in the step (2), if a thickness as measured after the loading device applying a pressure to the upper permeable sheet and the lower permeable sheet without the test sample is set as h1 and a thickness as measured after the loading device applying a pressure to the upper permeable sheet and the lower permeable sheet with the test sample is set as h2, the thickness of the test sample is h=h2−h1. Specifically, in the step (3), the vacuum pressure is in a range of −0.02-0MPa.
Exemplary embodiments of the present invention will be described hereunder with reference to the drawings to make the present application apparent. Among the figures,
The present invention will be further described in detail with reference to the figures.
The present invention provides a testing apparatus for testing permeability in a thickness direction of a resin matrix composite material layer. Preferably, the apparatus may be applied to the test of the permeability of the resin matrix composite material prepreg. As schematically shown in
As shown in
In combination with
As shown in
In the present invention, the test sample 14 to be tested refers to a prepreg layer of the resin matrix composite material. Fibers in the prepreg layer may be glass fibers, carbon fibers, aramid fibers or basalt fibers, etc.; a prepreg reinforcement may be a uni-directional fiber or fiber fabric, wherein the fiber fabric may be plain fabric, twill fabric, satin fabric or the like; the resin in the prepreg may be epoxy resin, phenolic resin, cyanate ester resin, bismaleimide resin or the like. The laying manner of the prepreg comprises uni-directional laying, orthogonal laying, quasi-isotropic laying or the like.
The present invention can be used to test air permeability of a prepreg layer of the resin matrix composite material in a thickness direction. Specific operations are as follows:
Preparation of Test Sample
First, the prepreg is cut into pieces with a size of 10×10 cm2, and then the pieces are laid in a laying manner.
Packaging of Test Sample
Referring to
Cavity Leakage Testing
Referring to
Testing of the Thickness of the Prepreg Layer
The loading flat panel 21 is directly laid flatly in the cavity 10. The loading device 2 is used to apply a pressure up to a preset pressure, a dial gauge is adjusted and fixed to allow its contact head to contact the upper surface of the loading flat panel 21, and the dial gauge reads h0.
After pressure relief, the loading flat panel 21 is moved away, the prepreg layer 14 is directly laid in the cavity 10 and the loading flat panel 21 is placed thereon. When the preset pressure is reached, the contact head of the dial gauge is allowed to contact the upper surface of the loading flat panel 21, and the dial gauge reads h1.
Under this pressure, the thickness of the prepreg layer 14 is h=h1−h0 with a measure unit of m.
Testing of Permeability of the Prepreg Layer in the Thickness Direction
The air outlet 103 of the test mold 1 is connected to the vacuum gauge 5 and the vacuum pump 6 via the air duct 8, and the air inlet 102 is connected to the flow meter 4 via the air duct 8.
Subsequently, the loading device 2 is adjusted to control the test pressure applied to the prepreg layer 14. In an embodiment of the present invention, the pressure at a unit area is in a range of 0-0.6 MPa;
Then, the temperature control device 3 is regulated to control a temperature in the test mold. In an embodiment of the present invention, the temperature is in a range of from room temperature to 200° C.;
Then the vacuum pump 6 is started. An air valve is used to regulate a vacuum pressure, and the vacuum gauge 5 is used to accurately measure the pressure valve P. Since air is compressible, the vacuum pressure should be controlled in a range of −0.02-0MPa during test to ensure accuracy of the test results;
Under a pressure gradient, air enters the air inlet 102 through the flow meter 4 and enters the upper permeable sheet 13 through the cover plate air guide recess 112 of the sealing cover plate 11. Since the upper permeable sheet 13 has a higher air permeability, it is ensured that the air can form a flow front on the upper surface of the whole prepreg layer after air enters the upper permeable sheet 13 along the cover plate air guide recess 112, and thereby it is ensured that the air flows out of the prepreg in the thickness direction of the prepreg, and flows towards the air outlet 103 through the lower permeable sheet 12 and the cavity air guide recesses 101. At this time, a volume flow rate Q of air is measured through the flow meter 4, with a measure unit of m3/s.
Finally, the permeability Kin the thickness direction of the prepreg layer 14 may be obtained according to Darcy law.
The permeability in the thickness direction is
wherein K represents the permeability of the prepreg layer 14 in the thickness direction and has a measure unit of m2; P represents a value of the vacuum pressure with a measure unit of Pa; l and b represent a length and a width of the prepreg layer 14 respectively and are both 10 cm in this test; η represents air viscosity with a measure unit of Pa·s.
By adjusting the loading device 2 and the temperature control device 3, the pressure and temperature acting on the prepreg layer 14 are changed to test the permeability of the prepreg layer 14 in the thickness direction under different pressure and temperature conditions.
The air viscosity η increases as the temperature T rises. At the temperature T<2000K, the air viscosity may be calculated from Satran formula
In this formula, T represents a testing temperature condition with a measure unit of K; η represents the air viscosity, i.e. air viscosity here, with a measure unit of Pa·s; T0 and η0 represent a reference temperature (K) and a corresponding viscosity respectively; C is a constant related to air type, and the constant of air C=110.4K. The air viscosities under partial temperatures are listed in Table 1 below.
A volume of air is greatly affected by the temperature. The flow meter 4 measures air flow under a measurement value of T0. When the test mold has a temperature T, the air flow under this temperature condition may be calculated by using a modification formula
In the present embodiment, the carbon fiber/epoxy 914 resin fabric prepreg is used as a test object. The prepreg is cut into pieces with a size of 10×10 cm2, and seven layers of the pieces are laid. The loading device 2 is used to apply a load to the loading flat panel 21 so as to measure the air permeability of the prepreg layer 14 in the thickness direction under different pressure conditions. At a test temperature of 20° C., the air viscosity is 18×10−6 Pa·S. The test results are shown in
In the present embodiment, the T700 carbon fiber/bismaleimide resin uni-directional prepreg is used as a test object. The prepreg is cut into pieces with a size of 10×10 cm2, and 16 layers of the pieces are laid in the uni-directional laying manner. The loading device 2 is used to apply a load to the loading flat panel 21 to measure the air permeability of the prepreg layer 14 in the thickness direction under different pressure conditions. At a test temperature of 20° C., the air viscosity is 18×10−6 Pa·S. The test results are shown in
In the present embodiment, the T700 carbon fiber/bismaleimide resin uni-directional prepreg is used as a test object. The prepreg is cut into pieces with a size of 10×10 cm2, and 16 layers of the pieces are laid in the uni-directional laying manner. The loading device 2 is used to apply a unit pressure of 0.65 MPa to the loading flat panel 21 acting on the upper permeable sheet 13 to measure the air permeability of the prepreg layer 14 in the thickness direction under different temperature conditions. The test results are shown in Table 2 below.
In the above embodiments, the range of the testing pressure varies. For example, in the embodiment 1, the test pressure may reach 1.3 MPa, while the test pressure in the embodiment 2 may reach 0.65 MPa and the pressure applied in the embodiment 3 is also 0.65 MPa. Those skilled in the art may appreciate that the pressure range upon the application of the present invention for testing is not limited to 0-0.6 MPa, and the test may be performed in a broader pressure range according to the loading capability of the loading device. In addition, the test temperature range in the present invention is from room temperature to 200° C. This is because a cooling system is not additionally provided in the present invention and a temperature upper limit of the test instrument is 200° C. However, those skilled in the art may appreciate that so long as the test instrument permits, the present invention may test permeability in a broader temperature range.
The present invention is not, in any form, limited to exemplary embodiments presented in the description and drawings. Many variations are possible within the scope of the present invention as generalized by the appended claims. In addition, any reference signs in the claims shall not be construed as limiting the scope of the present invention.
The reference numbers in the figures denote the following features:
| Number | Date | Country | Kind |
|---|---|---|---|
| 201110030013.X | Jan 2011 | CN | national |
This application claims priority to International Application Serial No. PCT/CN2011/085129, filed Dec. 31, 2011, which claims priority to Chinese Application No. 201110030013.X, filed Jan. 27, 2011. International Application Serial No. PCT/CN2011/085129 is hereby incorporated herein for all purposes by this reference.
| Filing Document | Filing Date | Country | Kind | 371c Date |
|---|---|---|---|---|
| PCT/CN2011/085129 | 12/31/2011 | WO | 00 | 7/29/2013 |
