CN105500728B - 一种制造蓄压油箱大型膜片的方法及蓄压油箱大型膜片 - Google Patents

一种制造蓄压油箱大型膜片的方法及蓄压油箱大型膜片 Download PDF

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CN105500728B
CN105500728B CN201510828397.8A CN201510828397A CN105500728B CN 105500728 B CN105500728 B CN 105500728B CN 201510828397 A CN201510828397 A CN 201510828397A CN 105500728 B CN105500728 B CN 105500728B
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绳索修
田旭
阎中伟
陈亚争
李丽贤
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Shenyang Aircraft Design and Research Institute Aviation Industry of China AVIC
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/30Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/54Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
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    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
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    • D06M11/00Treating fibres, threads, yarns, fabrics or fibrous goods made from such materials, with inorganic substances or complexes thereof; Such treatment combined with mechanical treatment, e.g. mercerising
    • D06M11/51Treating fibres, threads, yarns, fabrics or fibrous goods made from such materials, with inorganic substances or complexes thereof; Such treatment combined with mechanical treatment, e.g. mercerising with sulfur, selenium, tellurium, polonium or compounds thereof
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Abstract

本发明公开了一种制造蓄压油箱大型膜片的方法。所述制造蓄压油箱大型膜片的方法包括如下步骤:步骤1:制作待制作大型膜片的模胎;步骤2:向模胎涂抹脱模剂;步骤3:向模胎铺设织物,从而使织物的一侧为待处理侧;步骤4:对织物的待处理侧进行表面处理;步骤5:向织物的待处理侧涂抹底胶;步骤6:向织物的待处理侧涂抹主体胶液;步骤7:在织物的待处理侧上涂抹滑石粉,并翻转,从而使另一侧固定在模态上,并重复所述步骤1至所述步骤6;步骤8:向经过步骤7处理后的织物粘接橡胶密封垫片,并固化,从而形成制造成型的大型膜片。本发明的制造蓄压油箱大型膜片的方法中,膜片主体受力骨架材料为织物,织物强度比橡胶材料高。

Description

一种制造蓄压油箱大型膜片的方法及蓄压油箱大型膜片
技术领域
本发明涉及非金属零件技术领域,具体涉及一种制造蓄压油箱大型膜片的方法及蓄压油箱大型膜片。
背景技术
蓄压油箱是飞机燃油系统重要功能附件,可以保证飞机在进入零负过载时向发动机供油。膜片是蓄压油箱的重要敏感元件,通过膜片的运动才能把蓄压油箱内的燃油挤压出来流入燃油管路,实现向发动机供油。
现有技术中,膜片通常采用纯橡胶膜片,纯橡胶膜片具有强度低,受压后易变形的缺点。
因此,希望有一种技术方案来克服或至少减轻现有技术的至少一个上述问题。
发明内容
本发明的目的在于提供一种制造蓄压油箱大型膜片的方法来克服或至少减轻现有技术中的至少一个上述问题。
为实现上述目的,本发明提供了一种制造蓄压油箱大型膜片的方法,所述制造蓄压油箱大型膜片的方法包括如下步骤:步骤1:制作待制作大型膜片的模胎;步骤2:向模胎涂抹脱模剂;步骤3:向模胎铺设织物,从而使织物的一侧为待处理侧;步骤4:对织物的待处理侧进行表面处理;步骤5:向经过所述步骤4处理后的织物的待处理侧涂抹底胶;步骤6:向经过步骤5处理后的织物的待处理侧涂抹主体胶液;步骤7:在经过所述步骤6处理后的织物的待处理侧上涂抹滑石粉,并翻转,从而使另一侧固定在模态上,并重复所述步骤1至所述步骤6;步骤8:向经过步骤7处理后的织物粘接橡胶密封垫片,并固化,从而形成制造成型的大型膜片。
优选地,所述步骤1中的模胎为木质材料制成。
优选地,所述步骤2具体为:涂抹脱模剂,并在温度18~30℃,相对湿度不大于75%下干燥30min~50min。
优选地,所述步骤3中的织物为锦丝绸,所述铺设方法具体为:用均匀的拉力将锦丝绸绷在胎膜上,使纬线相对模胎纵轴成35°~45°分布,从下底部沿模胎纵向用钉子固定已铺好的织物,间距为10mm~30mm,保证织物以绷紧状态固定在胎膜上。
优选地,所述步骤3进一步包括:拉紧锦丝绸的圆弧段,使之无皱褶和折痕。
优选地,所述步骤4中的表面处理具体为:将拉紧到模胎上的锦丝绸用乙酸乙酯除油2次,在18℃~30℃干燥10min~30min。
优选地,所述步骤5具体为:涂刷底胶2遍,每遍胶液用量150~160g,即240~255g/m2,在温度18℃~30℃干燥10min~30min。
优选地,所述步骤6具体为:涂刷主体胶液8层~10层,每遍胶液用量130~140g,即210~225g/m2,每层干燥15min~30min,单面涂胶的锦丝绸在模胎保持24h。
优选地,所述步骤8具体为:沿膜片外边缘粘接橡胶密封垫片,并在23℃±2℃环境下硫化168小时。
本发明还提供了一种蓄压油箱大型膜片,所述蓄压油箱大型膜片采用如上所述的制造蓄压油箱大型膜片的方法制造而成。
本发明的制造蓄压油箱大型膜片的方法中,膜片主体受力骨架材料为织物,织物强度比橡胶材料高,因此该膜片能够承受更大的系统压力。且本方法可以使织物光滑的内嵌在膜片中,从而保证了膜片的制造质量,保证了膜片的功能。
附图说明
图1是根据本发明第一实施例的制造蓄压油箱大型膜片的方法的流程示意图。
具体实施方式
为使本发明实施的目的、技术方案和优点更加清楚,下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行更加详细的描述。在附图中,自始至终相同或类似的标号表示相同或类似的元件或具有相同或类似功能的元件。所描述的实施例是本发明一部分实施例,而不是全部的实施例。下面通过参考附图描述的实施例是示例性的,旨在用于解释本发明,而不能理解为对本发明的限制。基于本发明中的实施例,本领域普通技术人员在没有作出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。下面结合附图对本发明的实施例进行详细说明。
在本发明的描述中,需要理解的是,术语“中心”、“纵向”、“横向”、“前”、“后”、“左”、“右”、“竖直”、“水平”、“顶”、“底”“内”、“外”等指示的方位或位置关系为基于附图所示的方位或位置关系,仅是为了便于描述本发明和简化描述,而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作,因此不能理解为对本发明保护范围的限制。
图1是根据本发明第一实施例的制造蓄压油箱大型膜片的方法的流程示意图。
如图1所示的制造蓄压油箱大型膜片的方法包括如下步骤:步骤1:制作待制作大型膜片的模胎;步骤2:向模胎涂抹脱模剂;步骤3:向模胎铺设织物,从而使织物的一侧为待处理侧;步骤4:对织物的待处理侧进行表面处理;步骤5:向经过所述步骤4处理后的织物的待处理侧涂抹底胶;步骤6:向经过步骤5处理后的织物的待处理侧涂抹主体胶液;步骤7:在经过所述步骤6处理后的织物的待处理侧上涂抹滑石粉,并翻转,从而使另一侧固定在模态上,并重复步骤1至步骤6;步骤8:向经过步骤7处理后的织物粘接橡胶密封垫片,并固化,从而形成制造成型的大型膜片。
在本实施例中,所述步骤1中的模胎为木质材料制成。
在本实施例中,所述步骤2具体为:涂抹脱模剂,并在温度18~30℃,相对湿度不大于75%下干燥30min~50min。
在本实施例中,所述步骤3中的织物为锦丝绸,所述铺设方法具体为:用均匀的拉力将锦丝绸绷在胎膜上,使纬线相对模胎纵轴成35°~45°分布,从下底部沿模胎纵向用钉子固定已铺好的织物,间距为10mm~30mm。保证织物以绷紧状态固定在胎膜上。
在本实施例中,所述步骤3进一步包括:拉紧锦丝绸的圆弧段,使之无皱褶和折痕。
在本实施例中,所述步骤4中的表面处理具体为:将拉紧到模胎上的锦丝绸用乙酸乙酯除油2次,在18℃~30℃干燥10min~30min。
在本实施例中,所述步骤5具体为:涂刷底胶2遍,每遍胶液用量150~160g,即240~255g/m2,在温度18℃~30℃干燥10min~30min。
在本实施例中,所述步骤6具体为:涂刷主体胶液8层~10层,每遍胶液用量130~140g,即210~225g/m2,每层干燥15min~30min,单面涂胶的锦丝绸在模胎保持24h。
在本实施例中,所述步骤8具体为:沿膜片外边缘粘接橡胶密封垫片,并在23℃±2℃环境下硫化168小时。
作为一个实施例中,胶液的配制为:
a)底胶的配制:用烧杯称取适量底胶丁腈胶液,加入间二酚甲醛树脂、硫磺及醋酸乙脂,搅拌均匀。加入量按(1)、(2)、(3)计算:
X=0.2145C·D………………………………………………(1)
Y=0.01341C·D………………………………………………(2)
Z=(X·E+Y)(1-C)/C-X(1-E)………………………………(3)
式中:
X——间苯二酚甲醛树脂加入量,kg;
Y——硫磺加入量,kg;
Z——醋酸乙酯加入量,kg:
C——底胶丁腈胶液的不挥发物含量,%;
D——底胶丁腈胶液的实际配合量,kg;
E——间苯二酚甲醛树脂的不挥发物含量,%。
b)主体胶液的配制:用烧杯称取适量的主体胶液丁腈胶液,加入硫磺,并用醋酸乙酯稀释,搅拌均匀。加入量按(4)、(5)计算:
Y=0.01425C·D………………………………………………(4)
Z=Y(1-C)/C…………………………………………………(5)
式中:
Y——硫磺加入量,kg;
Z——醋酸乙酯加入量,kg;
C——主体胶液丁腈胶液的不挥发物含量,%;
D——主体胶液丁腈胶液的实际配合量,kg。
本发明还提供了一种蓄压油箱大型膜片,所述蓄压油箱大型膜片采用如上所述的制造蓄压油箱大型膜片的方法制造而成。
最后需要指出的是:以上实施例仅用以说明本发明的技术方案,而非对其限制。尽管参照前述实施例对本发明进行了详细的说明,本领域的普通技术人员应当理解:其依然可以对前述各实施例所记载的技术方案进行修改,或者对其中部分技术特征进行等同替换;而这些修改或者替换,并不使相应技术方案的本质脱离本发明各实施例技术方案的精神和范围。

Claims (3)

1.一种制造蓄压油箱大型膜片的方法,其特征在于,所述制造蓄压油箱大型膜片的方法包括如下步骤:
步骤1:制作待制作大型膜片的模胎;
步骤2:向模胎涂抹脱模剂;
步骤3:向模胎铺设织物,从而使织物的一侧为待处理侧;
步骤4:对织物的待处理侧进行表面处理;
步骤5:向经过所述步骤4处理后的织物的待处理侧涂抹底胶;
步骤6:向经过步骤5处理后的织物的待处理侧涂抹主体胶液;
步骤7:在经过所述步骤6处理后的织物的待处理侧上涂抹滑石粉,并翻转,从而使另一侧固定在模胎上,并重复所述步骤1至所述步骤6;
步骤8:向经过步骤7处理后的织物粘接橡胶密封垫片,并固化,从而形成制造成型的大型膜片;
所述步骤1中的模胎为木质材料制成;
所述步骤2具体为:涂抹脱模剂,并在温度18~30℃,相对湿度不大于75%下干燥30min~50min;
所述步骤3中的织物为锦丝绸,所述铺设方法具体为:用均匀的拉力将锦丝绸绷在模胎上,使纬线相对模胎纵轴成35°~45°分布,从下底部沿模胎纵向用钉子固定已铺好的织物,间距为10mm~30mm,保证织物以绷紧状态固定在模胎上;
所述步骤3进一步包括:拉紧锦丝绸的圆弧段,使之无皱褶和折痕;
所述步骤4中的表面处理具体为:将拉紧到模胎上的锦丝绸用乙酸乙酯除油2次,在18℃~30℃干燥10min~30min;
所述步骤5具体为:涂刷底胶2遍,每遍胶液用量150~160g,即240~255g/m2,在温度18℃~30℃干燥10min~30min;
所述步骤6具体为:涂刷主体胶液8层~10层,每遍胶液用量130~140g,即210~225g/m2,每层干燥15min~30min,单面涂胶的锦丝绸在模胎保持24h;
其中,所述底胶的配制:用烧杯称取适量底胶丁腈胶液,加入间二酚甲醛树脂、硫磺及醋酸乙脂,搅拌均匀,加入量按(1)、(2)、(3)计算:
X=0.2145C·D………………………………………………(1)
Y=0.01341C·D………………………………………………(2)
Z=(X·E+Y)(1-C)/C-X(1-E)………………………………(3)
式中:
X——间苯二酚甲醛树脂加入量,kg;
Y——硫磺加入量,kg;
Z——醋酸乙酯加入量,kg:
C——底胶丁腈胶液的不挥发物含量,%;
D——底胶丁腈胶液的实际配合量,kg;
E——间苯二酚甲醛树脂的不挥发物含量,%;
所述主体胶液的配制:用烧杯称取适量的主体胶液丁腈胶液,加入硫磺,并用醋酸乙酯稀释,搅拌均匀,加入量按(4)、(5)计算:
Y=0.01425C·D………………………………………………(4)
Z=Y(1-C)/C…………………………………………………(5)
式中:
Y——硫磺加入量,kg;
Z——醋酸乙酯加入量,kg;
C——主体胶液丁腈胶液的不挥发物含量,%;
D——主体胶液丁腈胶液的实际配合量,kg。
2.如权利要求1所述的制造蓄压油箱大型膜片的方法,其特征在于,所述步骤8具体为:沿膜片外边缘粘接橡胶密封垫片,并在23℃±2℃环境下硫化168小时。
3.一种蓄压油箱大型膜片,其特征在于,所述蓄压油箱大型膜片采用如权利要求1至2中任意一项所述的制造蓄压油箱大型膜片的方法制造而成。
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