CN117508561A

CN117508561A - Wing integral type shaping structure and forming die thereof

Info

Publication number: CN117508561A
Application number: CN202311651370.7A
Authority: CN
Inventors: 唐全升; 孙德权; 张建坤; 夏吉升; 欧阳焰; 方月华
Original assignee: Jiangxi Jiuyou Aviation Equipment Co ltd; Harbin Yuanchi Aviation Equipment Co ltd
Current assignee: Jiangxi Jiuyou Aviation Equipment Co ltd; Harbin Yuanchi Aviation Equipment Co ltd
Priority date: 2023-12-04
Filing date: 2023-12-04
Publication date: 2024-02-06
Anticipated expiration: 2043-12-04
Also published as: CN117508561B

Abstract

The application discloses wing integral type shaping structure and forming die thereof, the wing includes the wing portion and sets up the strengthening rib at the wing portion internal surface, the material embryo is general including the first material embryo body that is used for shaping the wing portion and the second material embryo body that is used for shaping the strengthening rib, be provided with material embryo main part and the first contact body of setting on material embryo main part on the first material embryo body, be provided with the second contact body on the second material embryo body and set up the material embryo muscle body on the inboard surface of the second contact body, material embryo muscle body is used for shaping the strengthening rib, first contact body and second contact body looks block in corresponding position department in order to form the material embryo is general; the outer side surface of the second contact body is matched with the outer side surface of the blank body to form the outer surface of the wing part; the first contact body has a gradually increasing extension length in a direction along the outer side surface toward the inner side surface, and the second contact body has a gradually decreasing extension length in a direction along the outer side surface toward the inner side surface, the extension length being matched with the extension length at a corresponding position.

Description

Wing integral type shaping structure and forming die thereof

Technical Field

The application relates to the technical field of aviation materials, in particular to an integrated wing forming structure and a forming die thereof.

Background

Wings are the main components providing lift to aircraft and in addition to the aerodynamic profile they have an increasing demand for their own weight reduction. In order to reduce the weight of the wing as much as possible while ensuring sufficient strength, it is an ideal technical line to use composite materials for the production of multi-cavity structural members.

Thermoplastic resin matrix composites (abbreviated as thermoplastic composites in this application) have better heat resistance, excellent damage tolerance, good impact resistance, short molding cycle, high production efficiency, and repeated molding, and have received more and more attention in the aerospace field in recent years.

The reinforcing ribs are usually glued on the wing structure, however, the reinforcing ribs are poor in tensile compression resistance, impact resistance and interlaminar shearing resistance, and the mechanical strength of the whole member is reduced, so that the performance of the wing is affected to a certain extent. In addition, the straightness and the position of the reinforcing ribs also have a certain influence on the performance of the wing.

Disclosure of Invention

In view of the above-mentioned drawbacks or shortcomings in the prior art, it is desirable to provide an integrated wing molding structure and a molding mold thereof, which can improve the manufacturing quality of the reinforcing ribs and the molding effect of the wing.

In a first aspect, the present application provides an integrated airfoil forming structure, where the airfoil includes an airfoil portion and a stiffener disposed on an inner surface of the airfoil portion, the airfoil is integrally formed by a blank, the blank generally includes a first blank for forming the airfoil portion and a second blank for forming the stiffener,

the first blank body comprises a blank body and a first contact body arranged on the blank body, a second contact body and a blank rib body arranged on the inner side surface of the second contact body are arranged on the second blank body, the blank rib body is used for forming the reinforcing rib, and the first contact body and the second contact body are clamped at corresponding positions to form a blank overall body;

the outer side surface of the second contact body is matched with the outer side surface of the blank main body to form the outer surface of the wing part;

the first contact body has a gradually increasing extension length in a direction along the outer side surface toward the inner side surface, and the second contact body has a gradually decreasing extension length in a direction along the outer side surface toward the inner side surface, the extension length being matched with the extension length at a corresponding position.

Optionally, the wing part comprises a first wing side part and a second wing side part, a bending part is arranged between the first wing side part and the second wing side part, and the reinforcing rib is arranged at the bending part and extends along the direction from the first wing side part to the second wing side part; the inner surfaces of the wing parts are provided with a plurality of reinforcing ribs;

the first blank body comprises a plurality of blank bodies, the blank bodies are respectively positioned at two sides of the second contact body, and the first contact body is positioned at one end, close to the first contact body, of the blank body.

Optionally, the second blank body has a central plane, the second blank body includes blank split bodies located at two sides of the central plane, the blank split bodies are symmetrically disposed about the central plane, and each of the blank split bodies includes a first blank split body for forming the blank rib body and a second blank split body for forming the second contact portion; the two material embryo components of a whole that can function independently pass through pre-compaction fixed connection, the second material embryo body still includes the range upon range of setting two the material embryo extension components of a whole that can function independently on the side of being away from the inboard surface of second material embryo components of a whole that can function independently.

Optionally, the inner side surface of the second contact and the inner side surface of the first contact mate to form an inner surface of the wing;

The second contact portion includes a plurality of layers of a second prepreg ply in a direction from the outside surface to the inside surface; the second prepreg layup includes an integer layer of the second prepreg.

Optionally, the first contacts located on two sides of the second contact are symmetrically disposed about the central plane, the first contact portion includes a plurality of first prepreg stacks, the first prepreg stacks include an integer number of first prepregs, and the first prepreg stacks have the same thickness as the second prepreg stacks of the corresponding number of layers and are in end contact with each other in the direction from the outer surface to the inner surface.

In a second aspect, the present application provides a forming die for forming a wing integral forming structure as described in any one of the above, the forming die comprising:

the first die comprises a first molding area and a second molding area, wherein the first molding area is used for laying multiple layers of first prepregs along with the shape to form a material blank main body, the second molding area is used for extending the first prepregs from the first molding area to the second molding area to form a first contact body, a plurality of first bosses are arranged on the second molding area in a stacked mode, and the first bosses are used for limiting the extending length of the first prepregs;

The second mould comprises a first paving area and a second paving area, wherein the first paving area is used for paving a plurality of layers of second prepregs along with the shape to form the material blank rib, the second paving area is used for enabling the second prepregs to extend from the first paving area to the second paving area to form a second contact body, a plurality of second bosses are arranged on the second paving area in a stacked mode, and the second bosses are used for limiting the extension length of the second prepregs.

Optionally, the first die comprises a first base, a plurality of first female dies and a plurality of second female dies, wherein the first female dies and the plurality of second female dies are arranged on the first base, the second female dies are detachably connected with the first base, and each second female die is positioned between two adjacent first female dies;

the first forming area is arranged on the first female die, the second forming area is arranged on the second female die, two second forming areas are symmetrically arranged on the second female die and are used for being matched with the adjacent first forming areas so as to form the first contact body at one end of the corresponding blank main body.

Optionally, the second molding region includes two molding extension regions, each of the molding extension regions is connected with the adjacent first molding region, the molding extension regions are matched with the shape of the outer surface of the wing, the first bosses are arranged between the two molding extension regions, and the lengths of the first bosses in the direction away from the molding extension regions are gradually decreased; the thickness of each first boss is an integral multiple of the thickness of the first prepreg, the first prepreg extends from the first forming area to the end part corresponding to the first boss and is flush with the surface of the corresponding first boss after the multi-layer conformal paving, and the next laminated first prepreg extends from the first forming area and covers the surface of the corresponding first boss.

Optionally, the first die further includes a third female die detachably connected to the first bottom plate, the third female die includes a third molding area, the third molding area is matched with the shape of the outer surface of the wing portion, and the third female die is used for replacing the second female die after the first contact body and the second contact body are clamped at corresponding positions to form a blank overall.

Optionally, the second mold comprises a second base, and a first half mold and a second half mold which are arranged on the second base, at least one of the first half mold and the second half mold is detachably connected with the second base, and the first half mold and the second half mold are respectively used for forming a blank body, separating and prepressing to form the second blank body;

the first half mould and the second half mould comprise the first paving area and the second paving area, the first paving area and the second paving area are vertically arranged, and the shape of the first paving area is matched with the shape of the reinforcing rib;

the second bosses are arranged at one end of the second paving region far away from the first paving region, and the lengths of the second bosses in the direction far away from the second paving region are gradually decreased; the thickness of each second boss is an integral multiple of the thickness of the second prepreg, the second prepreg extends from the second molding area to the end part corresponding to the second boss, is flush with the surface of the corresponding second boss after multi-layer conformal laying, and the next laminated second prepreg extends from the first laying area to and covers the surface of the second boss.

The technical scheme provided by the embodiment of the application can comprise the following beneficial effects:

according to the wing integrated forming structure, the first material blank body for forming the wing part and the second material blank body for forming the reinforcing ribs are arranged, contact fixation is carried out in a clamping mode, the outer surface of the second material blank body is flush with the outer surface of the wing, and the connection strength of the wing part and the reinforcing ribs is improved; and the joint of the first contact body and the second contact body of the clamping area, which are gradually changed in length, improves the connection strength of the clamping area, prevents layering, wrinkling and the like, and improves the molding effect.

Drawings

Other features, objects and advantages of the present application will become more apparent upon reading of the detailed description of non-limiting embodiments, made with reference to the following drawings, in which:

FIG. 1 is a schematic structural view of a wing provided in an embodiment of the present application;

FIG. 2 is a schematic structural diagram of a first blank according to an embodiment of the present disclosure;

FIG. 3 is a schematic structural diagram of a second blank according to an embodiment of the present disclosure;

fig. 4 is a schematic structural diagram of a first mold according to an embodiment of the present disclosure;

fig. 5 is a schematic view illustrating formation of a first contact according to an embodiment of the present application;

Fig. 6 is a schematic structural diagram of a first contact according to an embodiment of the present application;

FIG. 7 is a schematic diagram illustrating the mating of a first contact and a second contact according to an embodiment of the present application;

fig. 8 is a schematic view illustrating formation of a second contact according to an embodiment of the present application;

fig. 9 is a schematic structural diagram of a second contact according to an embodiment of the present application;

FIG. 10 is a schematic view of a vacuum flexible membrane according to an embodiment of the present application;

fig. 11 is a schematic cross-sectional view of a vacuum flexible film according to an embodiment of the present application.

Detailed Description

The present application is described in further detail below with reference to the drawings and examples. It is to be understood that the specific embodiments described herein are merely illustrative of the invention and are not limiting of the invention. It should be noted that, for convenience of description, only the portions related to the invention are shown in the drawings.

It should be noted that, in the case of no conflict, the embodiments and features in the embodiments may be combined with each other. The present application will be described in detail below with reference to the accompanying drawings in conjunction with embodiments.

Referring to fig. 1 in detail, the present application provides a wing 100, where the wing 100 includes a wing portion 110 and at least one stiffener 120 disposed on an inner surface 102 of the wing portion 110.

The wing 110 includes a first wing side 111 and a second wing side 112, a bending portion 113 is disposed between the first wing side 111 and the second wing side 112, and the stiffener 120 is disposed at the bending portion 113 and extends along a direction from the first wing side 111 to the second wing side 112; the inner surface 102 of the wing 110 is provided with a plurality of ribs 120.

The wing 110 includes an outer surface 101 and an inner surface 102 that are disposed opposite to each other, and the number of the ribs 120 may be one, two or more, and when the number of the ribs 120 is plural, the ribs 120 are disposed side by side on the inner surface 102 of the wing 110.

One end of the reinforcing rib 120 is disposed on the first wing part 110, the other end of the reinforcing rib 120 is disposed on the second wing part 110, and the reinforcing rib 120 extends from the first wing part 110 to the second wing part 110. In this embodiment, the length of the stiffener 120 is not limited, and one end of the stiffener 120 may be flush with the edge of the first wing 110, or one end of the stiffener 120 may be spaced from the first wing 110 by a certain distance, which is not limited in this application.

In this embodiment, as shown in fig. 2-3, the wing 100 is integrally formed by a blank, and the blank generally includes a first blank 210 for forming the wing portion 110 and a second blank 220 for forming the stiffener 120.

The first blank 210 includes a blank main body 212 and a first contact body 211 disposed on the blank main body 212, the second blank 220 is provided with a second contact body 221 and a blank rib body 222 disposed on an inner side surface of the second contact body 221, the blank rib body 222 is used for forming the reinforcing rib 120, and the first contact body 211 and the second contact body 221 are engaged at corresponding positions to form a blank assembly.

In this embodiment, the first blank 210 and the second blank 220 are formed by laying, pre-pressing, and the like. In this embodiment of the present application, the prepreg includes a substrate and a polymer material impregnated on the substrate, where the substrate may be a glass fiber cloth or a carbon fiber cloth, and the polymer material may be various plastic resins, and the embodiment of the present application is not specifically limited thereto. The first prepreg, the second prepreg, the third prepreg 530, and the like in the embodiments of the present application may be the same prepreg or different prepregs, which are not limited in this application.

In this embodiment, the outer surface of the second contact 221 and the outer surface of the blank body 212 are matched to form the outer surface 101 of the wing 110. In other words, in this embodiment, the wing portion 110 is formed by the first blank 210 and a portion of the second blank 220, and the position where the second contact 221 and the first contact 211 are engaged or overlapped is disposed on the area of the wing portion 110, so as to improve the bonding effect of the blank rib 222 and the blank body 212, and improve the mechanical strength of the formed reinforcing rib 120.

The number of the second blank bodies 220 corresponds to the number of the reinforcing ribs 120, and accordingly, the number of the blank bodies 212 may be plural. Specifically, the first blank 210 includes a plurality of blank bodies 212, the blank bodies 212 are respectively located at two sides of the second contact 221, and the first contact 211 is located at one end of the blank body 212 near the first contact 211.

Wherein the first contact body 211 has a gradually increasing extension length in a direction from the outer side surface to the inner side surface, and the second contact body 221 has a gradually decreasing extension length in a direction from the outer side surface to the inner side surface, the extension length being matched with the extension length at a corresponding position.

The extension length of the first contact body 211 is defined as the length between one end of the first contact body 211 close to the blank body 212 and the other end far away from the blank body 212, wherein the end of the first contact body 211 close to the blank body 212 can be regarded as flush, i.e. the measurement starting points of the extension lengths are consistent. The extension length of the second contact is defined herein as the length between the center of the second contact 221 and the end of the second contact 221 near the first contact 211.

It can be appreciated that, in the embodiment of the present application, the first contact body 211 and the second contact body 221 are engaged with each other, that is, in a direction from the outer surface 101 to the inner surface 102, the edge of the first contact body 211 contacts with the edge of the second contact body 221, that is, the gradual increasing trend of the extension length is consistent with the gradual decreasing trend of the extension length.

In the embodiment of the application, the contact positions of the first contact body 211 and the second contact body 221 are gradually changed, so that the combination effect during molding is improved; the forming effect of the first blank 210 and the second blank 220 at the contact surface is improved, and the uniformity and consistency of the thickness of the contact position are improved.

In this application, the structure of forming the reinforcing rib 120 is set to include two parts, namely, the second contact body 221 and the blank rib 222, that is, the outer side surface corresponding to the second contact body 221 and the outer side surface of the blank body 212 are matched to form the outer surface 101 of the wing portion 110, so that the positioning accuracy of the reinforcing rib 120 can be ensured, the straightness is improved, and the tensile compression, impact resistance and interlaminar shearing resistance of the reinforcing rib 120 are realized.

In this embodiment, the second blank 220 has a central plane, the second blank 220 includes blank segments located at two sides of the central plane, the blank segments are symmetrically disposed about the central plane, and each of the blank segments includes a first blank segment 231 for forming the blank rib 222 and a second blank segment 232 for forming the second contact portion; the two blank components are fixedly connected by pre-pressing, and the second blank 220 further includes a blank extending component 233 stacked on one side of the two second blank components 232 away from the inner side surface.

In this embodiment, the prepreg is laid by the first and second split blanks 231 and 232 on two sides of the center plane, and then the two split blank extending parts 233 are formed to connect the two parts together, and the split blank extending parts 233 are used to form on one side of the outer surface 101 of the wing 110, so as to improve the manufacturing quality and the connection strength of the wing 100.

It can be appreciated that in the embodiment of the present application, two ends of the blank extension split 233 respectively form a second contact body 221 with the first blank split 231 and another second contact body 221 with the second blank split 232, so as to be matched with the first contact bodies 211 on the first blank 210 respectively located at two sides of the second blank 220.

The outer side surface of the second contact body 221 and the outer side surface of the blank body 212 mate to form the outer surface 101 of the wing 110. An inner side surface of the second contact 221 and an inner side surface of the first contact 211 mate to form the inner surface 102 of the wing 110.

In this embodiment, the overall distribution trend of the extension length of the first contact body 211 along the direction from the outer side surface to the inner side surface is a stepwise increase, and the overall distribution trend of the extension length of the second contact body 221 along the direction from the outer side surface to the inner side surface is a stepwise decrease.

In this embodiment, the second contact portion includes a plurality of layers of a second prepreg ply 202 along the outside surface to inside surface direction; the second prepreg ply includes an integer layer of second prepreg.

The first contacts 211 located on both sides of the second contact 221 are symmetrically disposed about the center plane, and the first contact portion includes a plurality of first prepreg laminates 201 including an integer number of first prepregs, and the first prepreg laminates 201 are in contact with the ends of the second prepreg laminates having the same thickness as the corresponding number of layers in the direction from the outer surface toward the inner surface.

In this embodiment of the present application, one layer of the first prepreg stack 201 is an integer layer of the first prepreg with consistent extension length, and one layer of the second prepreg stack 202 is an integer layer of the second prepreg with consistent extension length, so that the forming is convenient to lay along with the shape, and the forming quality is improved. In the present application, the joint where the lengths of the first contact body 211 and the second contact body 221 in the engagement region are gradually changed improves the connection strength of the engagement region, prevents delamination, wrinkles, and the like, and improves the molding effect.

By providing the first contact body 211 on the first blank 210 forming the wing portion 110, and providing the second contact body 221 on the second blank 220 forming the reinforcing rib 120, the first contact body 211 and the second contact body 221 are engaged to form a blank assembly; the contact positions of the first contact body 211 and the second contact body 221 are gradually changed, so that the combination effect during molding is improved; by disposing a part of the structure forming the wing portion 110 on the second blank 220, the joining effect of the blank rib 222 and the blank body 212 is further improved, and the mechanical strength of the formed reinforcing rib 120 is improved.

The application provides an integrated forming die for a wing 100, wherein the forming die comprises a first die 300, a second die 400 and a third die which are matched with each other.

First die 300

As shown in fig. 4 to 5, the first mold 300 includes a first molding zone 301 and a second molding zone 302, the first molding zone 301 is used for laying multiple layers of first prepregs along with the first molding zone 301 to form the material blank main body 212, the second molding zone 302 is used for extending the first prepregs from the first molding zone 301 to the second molding zone 302 to form the first contact body 211, a plurality of first bosses 340 are stacked on the second molding zone 302, and the first bosses 340 are used for limiting the extending length of the first prepregs.

When specifically arranged, the first mold 300 includes a first base 310, and a plurality of first concave dies 320 and a plurality of second concave dies 330 disposed on the first base 310, where the second concave dies 330 are detachably connected to the first base 310, and each of the second concave dies 330 is located between two adjacent first concave dies 320. The first molding zone 301 is disposed on the first die 320, and the second molding zone 302 is disposed on the second die 330.

In this embodiment, the number of the second female dies 330 corresponds to the number of the first contact portions. The first concave dies 320 correspond to the number of blank bodies 212.

The second molding region 302 includes two molding extension regions 303, each molding extension region 303 is connected with the adjacent first molding region 301, the molding extension regions 303 are matched with the shape of the outer surface 101 of the wing 100, the first bosses 340 are disposed between the two molding extension regions 303, and the lengths of the first bosses 340 in the direction away from the molding extension regions 303 are gradually decreased; the thickness of each first boss 340 is an integer multiple of the thickness of the first prepreg, the first prepreg extends from the first molding region 301 to the end of the corresponding first boss 340, and is flush with the surface of the corresponding first boss 340 after multiple layers are laid in a conformal manner, and the next laminated first prepreg extends from the first molding region 301 and covers the surface of the corresponding first boss 340.

In this embodiment, the number of the first bosses 340 is matched with the number of layers of the first prepreg stack 201 to be molded, and the lengths of the plurality of first bosses 340 gradually decrease in the stacking direction along the die surface away from the first molding region 301; in this embodiment, the length of the first boss 340 is along the extending length direction of the first contact body 211. In this embodiment, the end portion of the first boss 340 near the side of the first molding region 301 is used to define the extension length of the first prepreg on the first molding region 301 and the second molding region 302, and the first prepreg with the corresponding number of layers extends to the end portion of the first boss 340 with the corresponding thickness, so as to implement the limitation of the extension length of the first prepreg stack 201.

Two second molding areas 302 are symmetrically disposed on the second die 330, and the second molding areas 302 are configured to match with the adjacent first molding areas 301 to form the first contact body 211 at one end of the corresponding blank body 212.

In this embodiment, the second die 330 may limit the extension length of the blank body 212 on both sides simultaneously, so both sides of the first boss 340 may limit the first prepreg laid on the first die 320 on both sides simultaneously, so as to form the first contact body 211 on the blank body 212 on both sides.

It should be noted that, in the embodiment of the present application, the second die 330 is only used to form the first contact body 211 with a predetermined length on the second molding area 302, and after the first prepreg is laid layer by layer and pre-pressed on the second molding area 302, the second die 330 is removed from the first base 310, so that the installation of the second blank 220 and the integral molding of the whole blank are not affected.

As shown in fig. 7, the first mold 300 further includes a third female mold 350 detachably connected to the first base plate, the third female mold 350 includes a third molding area 304, the third molding area 304 is matched with the shape of the outer surface 101 of the wing portion 110, and the third female mold 350 is used for replacing the second female mold 330 after the first contact body 211 and the second contact body 221 are engaged at corresponding positions to form a blank assembly.

In this embodiment, the mounting positions of the first concave die 320 and the third concave die 350 are consistent, and after the second blank 220 and the first blank 210 are assembled in a clamping manner, the third concave die 350 is installed to form the outer surface 101 of the blank corresponding to the position of the reinforcing rib 120. The first female die 320 and the second female die 330 are combined to form an integral molding on the wing 100.

Second die 400

As shown in fig. 8 to 9, the second mold 400 includes a first laying area 401 and a second laying area 402, the first laying area 401 is used for laying multiple layers of second prepregs along with the shape to form the material blank rib 222, the second laying area 402 is used for extending the second prepregs from the first laying area 401 to the second laying area 402 to form the second contact body 221, a plurality of second bosses 440 are stacked on the second laying area 402, and the second bosses 440 are used for limiting the extending length of the second prepregs.

The second mold 400 includes a second base 410, a first mold half 420 and a second mold half 430 disposed on the second base 410, at least one of the first mold half 420 and the second mold half 430 is detachably connected to the second base 410, and the first mold half 420 and the second mold half 430 are respectively used for forming a blank body and prepressing to form the second blank body 220.

The first half mold 420 and the second half mold 430 each include the first laying area 401 and the second laying area 402, the first laying area 401 and the second laying area 402 are vertically disposed, and the shape of the first laying area 401 is matched with the shape of the reinforcing rib 120.

Wherein the second bosses 440 are disposed at an end of the second paving region 402 away from the first paving region 401, and the lengths of the plurality of second bosses 440 in a direction away from the second paving region 402 are gradually decreased; the thickness of each second boss 440 is an integer multiple of the thickness of the second prepreg, the second prepreg extends from the second molding region 302 to the end of the corresponding second boss 440, and is flush with the surface of the corresponding second boss 440 after the multi-layer conformal laying, and the next laminated second prepreg extends from the first laying region 401 to and covers the surface of the second boss 440.

In this embodiment, the first mold half 420 is used to form the first blank component 231 alone, and the second mold half 430 is used to form the second blank component 232 alone. After the first half mold 420 and the second half mold 430 are closed, the first blank component 231 and the second blank component 232 may be pre-pressed and fixed, and the second blank 220 may be formed.

In this embodiment, the number of the second bosses 440 is matched with the number of layers of the second prepreg stack 202 to be molded, and the lengths of the plurality of second bosses 440 gradually decrease in the stacking direction along the die surface away from the second laying area 402. In this embodiment, the length of the second boss 440 is along the extending length direction of the second contact 221. In this embodiment, the end portion of the second boss 440 near the side of the second laying area 402 is used to define the extension length of the second prepreg laid onto the second laying area 402 by the first laying area 401, and the second prepreg with the corresponding layer number extends to the end portion of the second boss 440 with the corresponding thickness, so as to implement the limitation on the extension length of the second prepreg stack 202.

In one embodiment of the present application, the second blank 220 comprises a blank extension that may be limited at one or more bosses adjacent to the second laydown area 402 to form the second contact 221.

Third die

As shown in fig. 10-11, the shape of the third mold is matched with the shape of the wing 100, the third mold is used for laying an air guide net 510, at least two unvulcanized rubber layers 520 and a third prepreg 530 arranged between two adjacent unvulcanized rubber layers 520 along with the shape, and a plurality of ultrasonic vibration pieces 540 are arranged on the unvulcanized rubber layers 520 to form a vacuum soft film 500 with the same shape as the wing 100 in a vulcanization mode, the vacuum soft film 500 comprises a first soft film part matched with the shape of the wing 110 and a second soft film part matched with the shape of the reinforcing rib 120, the air guide net 510 covers the first soft film part and the second soft film part along with the shape, the plurality of ultrasonic vibration pieces 540 are at least distributed on the second soft film part, and the plurality of ultrasonic vibration pieces are used for vibration vulcanization in the vulcanization forming process.

In this embodiment of the present application, the third mold includes a male mold and a female mold, the male mold and the female mold form a cavity after being clamped, and the vacuum soft film 500 is formed in the cavity. In the embodiment of the application, the male die and the female die are adopted, so that the air guide net 510 and the ultrasonic vibration piece 540 can be conveniently paved. In the embodiment of the application, the ultrasonic vibration piece 540 is connected to the vibration generator through the connecting wire, so that the vacuum soft membrane 500 can be conveniently vibrated, the vibration vacuumizing is realized, and the vacuumizing capability is improved.

The air guide net 510 in the embodiment of the present application may be a heat-resistant net such as asbestos, glass wool, rock wool, slag wool, and the like. The ultrasonic vibration plate 540 may be a ceramic vibrator.

In this embodiment, the air guide net 510 is disposed on a surface of the vacuum soft film 500 that is in contact with the blank. The vibration generator is disposed in the inner layer of the vacuum bladder 500, and the number of the unvulcanized rubber layers 520 and the third prepregs 530 in the vacuum bladder 500 is in this embodiment in such a manner that one third prepreg 530 is disposed between every two unvulcanized rubber layers 520, by which the rigidity and the air impermeability of the vacuum bladder 500 can be improved.

In this embodiment, the vacuum soft film 500 is used to cover all surfaces of the material blank on the first mold 300 in the integral molding process of the wing 100, and the vacuum pumping operation in the vacuum hot press molding process can be performed through the vacuum soft film 500. Therefore, the molding quality (including the shape accuracy and the air impermeability) of the vacuum film 500 directly affects the vacuuming effect. In this application, the vacuum bladder 500 is identical to the shape of the wing 100, and therefore, a high profile accuracy is required when the shape of the rib 120 or other curved surface is to be used. In the embodiment of the present application, the unvulcanized rubber and the third prepreg 530 are adopted for molding, and in the present application, the ultrasonic vibration piece 540 is sandwiched between rubber materials, so that the ultrasonic vibration piece 540 can vibrate in the vulcanization molding process of the vacuum soft film 500, thereby improving the flowing effect of the rubber materials and meeting the appearance requirement; the vacuum soft film 500 formed by the composite material can be reduced by ultrasonic vibration, so that the problems of high porosity, glue enrichment and the like are solved, and the appearance accuracy and the air impermeability are improved.

In the embodiment of the application, the ultrasonic vibration piece 540 can also be applied to a vacuumizing process before the vacuum hot-pressing integrated forming process, and the vacuumizing effect is improved in a vibration mode.

In this embodiment, the number of layers of the unvulcanized rubber layer 520 and the third prepreg 530 is not limited, and may be set according to needs in different embodiments, and in this embodiment, the rigidity of the vacuum soft film 500 may be improved, and the vacuumizing effect and the overall supporting effect on the material blank may be improved through the third prepreg 530.

An embodiment of the present application provides an integral forming method of a wing 100, where the method includes:

s100, forming a first blank 210 through a first die 300.

The first mold 300 includes a first molding zone 301 and a second molding zone 302, a plurality of layers of a first prepreg are laid on the first molding zone 301 in a conformal manner and the first prepreg is extended from the first molding zone 301 to the second molding zone 302 to form a preform body 212 on the first molding zone 301 and a first contact body 211 on the second molding zone 302, and an extension length of the first contact body 211 in a direction along an outer side surface toward an inner side surface is gradually increased.

In particular, as shown in fig. 5-6, the method for forming the first blank 210 by the first die 300 includes:

s110, paving the first prepregs layer by a preset layer number, and extending each layer of the first prepregs from the first molding zone 301 to the end part of the first boss 340 corresponding to the paving layer until the first prepregs are flush with the surface of the corresponding first boss 340;

S120, continuing laying a first prepreg of a next layer, the first prepreg of the next layer extending from the first molding zone 301 and covering the surface of the corresponding first boss 340;

s130, until all the first prepregs for forming the first blank 210 are laid up to form the first blank 210.

It will be appreciated that in the present embodiment, the sides of the same first boss 340 are used to limit the lay-up length of the first prepreg of the same thickness, and the surface of the first boss 340 may also be used for conformal lay-up of the next first prepreg layup 201. To form a stack of stacked layers of different lengths of the first prepreg layup 201.

S200, forming a second blank 220 through a second die 400.

The second mold 400 includes a first lay-up area 401 and a second lay-up area 402, a plurality of layers of a second prepreg are laid down on the first lay-up area 401 in a conformal manner and the second prepreg is extended from the first lay-up area 401 to the second lay-up area 402 to form a green body 222 on the first lay-up area 401 and a second contact body 221 on the second lay-up area 402, and an extension length of the second contact body 221 in a direction along an outer side surface toward an inner side surface is gradually decreased.

Specifically, as shown in fig. 8-9, the method for forming the second blank 220 by the second mold 400 includes:

s210, paving a preset number of layers of the second prepreg layer by layer on the first paving region 401 on the first half mold 420, and extending each layer of the second prepreg layer from the second paving region 402 to the end part, corresponding to the second boss 440, of the paving layer on the second paving region 402 until the end part is level with the surface of the corresponding second boss 440; continuing to lay down a next lay-up of a second prepreg extending from the second lay-down area 402 and covering the surface of the corresponding second boss 440; until all of the second prepreg layup for shaping the prepreg ribs 222 is completed to form a prepreg split over the first mold half 420.

S220, forming a blank split on the second half mold 430; the manner of forming the blank split on the second mold half 430 may refer to S210, and will not be described herein.

S230, fixing the second half mold 430 and the first half mold 420 on the second base 410 so that the split material blank on the first half mold 420 is in split contact with the split material blank on the second half mold 430;

S240, providing a filling block 234, wherein the filling block 234 is disposed in a triangular area enclosed between the blank split on the first half mold 420 and the blank split on the second half mold 430, and an upper surface of the filling block 234 is flush with an upper surface of the blank split.

The filling block 234 in the embodiment of the present application is preformed, and the material of the filling block 234 is the same as that of the second prepreg. The filling block 234 is approximately triangular in shape and has three surfaces, wherein two equal-length surfaces are respectively contacted with blanks on two sides in a split manner, so as to improve the molding quality of the second blank 220.

And S250, continuously paving a plurality of layers of second prepregs layer by layer along with the shape on the upper surfaces of the two split material blanks, wherein two ends of each second prepreg extend to the end parts of the second bosses 440 corresponding to the paving layers respectively until the second prepregs are flush with the surfaces of the corresponding second bosses 440 so as to form the split material blank extension 233.

S260, pre-pressing each layer of the second prepreg to form the second blank 220, and peeling the second blank 220 from the second mold 400.

In the embodiment of the application, the pre-pressing process is a mode of vacuumizing pre-pressing or rolling after the prepreg is laid, so that the contact effect between adjacent prepregs is improved, and interlayer bubbles are prevented. To further enhance the integrated shaping of the wing 100.

S300, forming a blank overall.

As shown in fig. 7, the first contact body 211 on the first blank 210 and the second contact body 221 on the second blank 220 are snapped together at corresponding positions on the first mold 300 to form the blank assembly, wherein the outer side surface of the second contact body 221 and the outer side surface of the blank body 212 are matched to form the outer surface 101 of the wing 110, and the extension length of the first contact body 211 is matched to the extension length of the second contact body 221 at corresponding positions.

In an embodiment of the present application, the method for forming a blank overall includes:

s310, after the second female die 330 is removed from the first bottom plate, the first contact body 211 and the second contact body 221 are engaged at corresponding positions;

s320, installing the third female die 350 on the first bottom plate, and attaching and pre-pressing the material blank overall with the third forming area 304 to form the material blank overall.

S400, forming a vacuum soft film 500 through a third die: the shape of the third mold is matched with the shape of the wing 100, an air guide net 510, at least two layers of unvulcanized rubber layers 520 and a third prepreg 530 arranged between two adjacent unvulcanized rubber layers 520 are laid on the third mold along with the shape, a plurality of ultrasonic vibration sheets 540 are arranged on the unvulcanized rubber layers 520, the vacuum soft film 500 with the shape identical to the shape of the wing 100 is formed by vibration vulcanization, and the plurality of ultrasonic vibration sheets 540 are at least distributed at positions corresponding to the reinforcing ribs 120.

In the embodiment of the present application, the vibration vulcanization molding refers to that the ultrasonic vibration piece 540 vibrates during the vulcanization molding process.

The method of forming the vacuum bladder 500 includes:

s410, laying the air guide net 510, the first unvulcanized rubber layer 520, the third prepreg 530 layer and the second unvulcanized rubber layer 520 on the male die in a lamination manner, wherein connecting wires are arranged on the ultrasonic vibration sheet 540, and the ultrasonic vibration sheet 540 is arranged between the third prepreg 530 and the second unvulcanized rubber layer 520 or between the third prepreg 530 and the first unvulcanized rubber layer 520;

and S420, the male die and the female die are matched, and the vacuum soft film 500 is formed through a vibration vulcanization process.

Optionally, the vulcanization process conditions: the method adopts a sectional heating and pressure maintaining mode, the heating rate is less than or equal to 1.5 ℃/min, the vulcanizing temperature is 175 ℃ to 210 ℃, the time is 350min to 420min, the pressure is 0.665MPa to 0.735MPa, and the whole process is kept under full vacuum.

S500, carrying out vibration vacuumizing: the vacuum flexible film 500 is covered on the blank in a conformal manner, and is connected with an ultrasonic vibration plate 540, and vacuum is formed between the vacuum flexible film 500 and the first mold 300 through a vibration vacuumizing process, so that the wing 100 is molded through a vacuum hot-pressing process.

Illustratively, evacuating through the vacuum bag, the evacuating pressure being-90 Kpa to-100 Kpa; a positive pressure of +80Kpa to +100Kpa is applied through the outside of the vacuum tank. Heating up to 125+/-10 ℃ at a heating rate of 0.5-3 ℃/min and preserving heat for 60-75 min in a vacuum tank in the curing process, continuously heating up to 175+/-5 ℃ and preserving heat for 240-255 min, continuously heating up to 200+/-5 ℃ and preserving heat for 60-75 min, continuously heating up to 230+/-5 ℃ and preserving heat for 240-255 min, then cooling down at a cooling rate lower than 1.5 ℃/min, and releasing pressure when the temperature is reduced to below 80 ℃ to finish curing. It should be noted that the process parameters are adjusted as needed in different embodiments.

The vibration vacuuming process in the embodiment of the present application refers to vibration by the ultrasonic vibration sheet 540 during vacuuming.

It is to be understood that the terms "length," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like indicate or are based on the orientation or positional relationship shown in the drawings, merely to facilitate describing the invention and simplify the description, and do not indicate or imply that the devices or elements referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus should not be construed as limiting the invention.

Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defining "a first" or "a second" may explicitly or implicitly include one or more such feature. In the description of the present invention, the meaning of "a plurality" is two or more, unless explicitly defined otherwise.

Unless defined otherwise, technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention pertains. The terminology used herein is for the purpose of describing particular implementations only and is not intended to be limiting of the invention. Terms such as "disposed" or the like as used herein may refer to either one element being directly attached to another element or one element being attached to another element through an intermediate member. Features described herein in one embodiment may be applied to another embodiment alone or in combination with other features unless the features are not applicable or otherwise indicated in the other embodiment.

The present invention has been described in terms of the above embodiments, but it should be understood that the above embodiments are for purposes of illustration and description only and are not intended to limit the invention to the embodiments described. Those skilled in the art will appreciate that many variations and modifications are possible in light of the teachings of the invention, which variations and modifications are within the scope of the invention as claimed.

Claims

1. The integrated wing forming structure is characterized in that the wing comprises a wing part and reinforcing ribs arranged on the inner surface of the wing part, the wing is integrally formed by a material blank, the material blank generally comprises a first material blank body for forming the wing part and a second material blank body for forming the reinforcing ribs, wherein,

2. The wing-integrated forming structure according to claim 1, wherein the wing part includes a first wing side part and a second wing side part, a bending part is provided between the first wing side part and the second wing side part, and the stiffener is provided at the bending part and extends in a direction from the first wing side part to the second wing side part; the inner surfaces of the wing parts are provided with a plurality of reinforcing ribs;

3. The wing-integrated forming structure according to claim 1, wherein the second blank body has a center plane, the second blank body includes blank split bodies located at both sides of the center plane, the blank split bodies are symmetrically disposed with respect to the center plane, and each of the blank split bodies includes a first blank split body for forming the blank rib body and a second blank split body for forming the second contact portion; the two material embryo components of a whole that can function independently pass through pre-compaction fixed connection, the second material embryo body still includes the range upon range of setting two the material embryo extension components of a whole that can function independently on the side of being away from the inboard surface of second material embryo components of a whole that can function independently.

4. The wing integral molding structure of claim 3, wherein an inside surface of the second contact and an inside surface of the first contact mate to form an inside surface of the wing;

5. The integrated airfoil structure of claim 4, wherein the first contact on both sides of the second contact is symmetrically disposed about the center plane, the first contact portion comprises a plurality of first prepreg plies, the first prepreg plies comprising an integral number of first prepregs, the first prepreg plies having a same thickness as a corresponding number of second prepreg plies and being in end-to-end contact with the inner surface from the outer surface.

6. A mold for molding an airfoil according to any one of claims 1 to 5, the mold comprising:

7. The airfoil forming die of claim 6, wherein the first die comprises a first base, and a plurality of first female dies and a plurality of second female dies disposed on the first base, the second female dies being detachably connected to the first base, each of the second female dies being located between two adjacent first female dies;

8. The airfoil mold of claim 7, wherein said second molding zone includes two molding extensions, each of said molding extensions being contiguous with its adjacent first molding zone and said molding extension being shape-matched to an outer surface of said airfoil, said first plurality of bosses being disposed between two of said molding extensions, said first plurality of bosses tapering in length in a direction away from said molding extensions; the thickness of each first boss is an integral multiple of the thickness of the first prepreg, the first prepreg extends from the first forming area to the end part corresponding to the first boss and is flush with the surface of the corresponding first boss after the multi-layer conformal paving, and the next laminated first prepreg extends from the first forming area and covers the surface of the corresponding first boss.

9. The airfoil forming die of claim 7, wherein the first die further comprises a third die detachably connected to the first base plate, the third die comprising a third forming region, the third forming region being matched in shape with an outer surface of the airfoil, the third die being configured to replace the second die after the first contact body and the second contact body are engaged at corresponding positions to form a blank overall.

10. The airfoil forming mold of claim 6, wherein the second mold comprises a second base, and a first mold half and a second mold half disposed on the second base, at least one of the first mold half and the second mold half being detachably connected to the second base, the first mold half and the second mold half being respectively used for forming a blank split and pre-pressing the second blank;