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CN111796006A - A laminated fuel quantity detection sensor for aviation turbine - Google Patents

A laminated fuel quantity detection sensor for aviation turbine Download PDF

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Publication number
CN111796006A
CN111796006A CN202010553665.0A CN202010553665A CN111796006A CN 111796006 A CN111796006 A CN 111796006A CN 202010553665 A CN202010553665 A CN 202010553665A CN 111796006 A CN111796006 A CN 111796006A
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flat plate
detection sensor
pad
quantity detection
flat
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王纪超
王超
张运瑞
褚鑫
郝思伟
张永革
吴会军
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CETC 29 Research Institute
Xinxiang Aviation Industry Group Co Ltd
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Xinxiang Aviation Industry Group Co Ltd
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N27/00Investigating or analysing materials by the use of electric, electrochemical, or magnetic means
    • G01N27/02Investigating or analysing materials by the use of electric, electrochemical, or magnetic means by investigating impedance
    • G01N27/22Investigating or analysing materials by the use of electric, electrochemical, or magnetic means by investigating impedance by investigating capacitance
    • G01N27/221Investigating or analysing materials by the use of electric, electrochemical, or magnetic means by investigating impedance by investigating capacitance by investigating the dielectric properties
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N27/00Investigating or analysing materials by the use of electric, electrochemical, or magnetic means
    • G01N27/02Investigating or analysing materials by the use of electric, electrochemical, or magnetic means by investigating impedance
    • G01N27/22Investigating or analysing materials by the use of electric, electrochemical, or magnetic means by investigating impedance by investigating capacitance

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Abstract

本发明属于传感器技术,具体为一种航空涡轮用叠片式油量检测传感器,它由若干个平板A、平板B、衬垫和导线组成,衬垫安装于平板A与平板B之间,平板A、衬垫与平板B依次叠放,所有平板A、平板B分别由导线连接,与衬垫组成一个电容器,衬垫通过四周边缘与脱脂棉接触。使用时,将本发明放置于棉花中,衬垫接触脱脂棉并吸收脱脂棉内润滑油,直至达到平衡,随着脱脂棉中的润滑油含量变化(增大或减少),衬垫润滑油含量同步变化,衬垫介电常数发生改变,由平板A、平板B与衬垫组成的电容的电容值改变,通过检测电容值的变化,达到脱脂棉中油量检测目的。检测值通过导线传给测量、显示模块。能实现含油量的在线检测。

Figure 202010553665

The invention belongs to sensor technology, in particular to a laminated oil quantity detection sensor for aviation turbines. A. The pads and the plate B are stacked in turn. All the plates A and B are connected by wires respectively, forming a capacitor with the pads, and the pads are in contact with the absorbent cotton through the surrounding edges. When in use, the present invention is placed in cotton, and the pad contacts the absorbent cotton and absorbs the lubricating oil in the absorbent cotton until it reaches equilibrium. As the content of the lubricating oil in the absorbent cotton changes (increases or decreases), the lubricating oil content of the pad changes synchronously, The dielectric constant of the pad changes, and the capacitance value of the capacitor composed of the flat plate A, the flat plate B and the pad changes, and the purpose of detecting the oil content in the absorbent cotton is achieved by detecting the change of the capacitance value. The detected value is transmitted to the measurement and display module through the wire. It can realize on-line detection of oil content.

Figure 202010553665

Description

一种航空涡轮用叠片式油量检测传感器A laminated fuel quantity detection sensor for aviation turbine

技术领域technical field

本发明属于传感器技术,涉及对航空涡轮油室内脱脂棉含油量的在线检测。具体为一种航空涡轮用叠片式油量检测传感器。The invention belongs to sensor technology, and relates to on-line detection of oil content of absorbent cotton in an aviation turbine oil chamber. Specifically, it is a laminated oil quantity detection sensor for aviation turbine.

背景技术Background technique

目前采用油润滑的航空涡轮,润滑油贮存在专用油室内的脱脂棉中,无在线检测润滑油含量的装置,油量消耗及加油周期只能通过记录使用时间得到,但由于实际运行工况复杂,相同的工作时间,润滑油消耗量差别很大,导致加油量难以评估,加油过多会造成润滑油泄漏、污染环境,加油过少会造成轴承因润滑不良而损坏,需要在涡轮内布置润滑油含量传感器,便于在线监测。At present, the oil-lubricated aviation turbine is used, and the lubricating oil is stored in the absorbent cotton in the special oil chamber. There is no device for online detection of the lubricating oil content. The oil consumption and refueling cycle can only be obtained by recording the use time. In the same working hours, the consumption of lubricating oil varies greatly, which makes it difficult to evaluate the amount of oil. Too much oil will cause oil leakage and pollute the environment. Too little oil will cause the bearing to be damaged due to poor lubrication. It is necessary to arrange lubricating oil in the turbine. Content sensor for easy online monitoring.

发明内容SUMMARY OF THE INVENTION

本发明的目的是:提出一种航空涡轮用叠片式油量检测传感器,集成在涡轮中,可实现含油量的在线监测。The purpose of the present invention is to propose a laminated oil quantity detection sensor for aviation turbine, which is integrated in the turbine and can realize on-line monitoring of oil content.

本发明的技术方案是:The technical scheme of the present invention is:

一种航空涡轮用叠片式油量检测传感器,由平板A(1)、平板B(2)、衬垫(3)、导线组成,若干个平板A(1)由同一根导线连接,若干个平板B(2)由另一根导线连接,且平板A(1)、平板B(2)之间不能发生短接;若干个衬垫(3)安装于平板A(1)与平板B(2)之间,平板A(1)、衬垫(3)与平板B(2)依次叠放,平板A(1)、衬垫(3)与衬垫(3)组成一个电容器。A laminated oil quantity detection sensor for an aviation turbine, which is composed of a flat plate A (1), a flat plate B (2), a gasket (3), and a wire. Several flat plates A (1) are connected by the same wire, and several flat plates Plate B (2) is connected by another wire, and there is no short circuit between plates A (1) and B (2); several spacers (3) are installed on plate A (1) and plate B (2) ), the plate A (1), the gasket (3) and the plate B (2) are stacked in sequence, and the plate A (1), the gasket (3) and the gasket (3) form a capacitor.

平板A(1)、平板B(2)材料为不锈钢。The material of the flat plate A (1) and the flat plate B (2) is stainless steel.

平板A(1)、平板B(2)长宽规格依据所测量油室的大小而定。The length and width specifications of plate A (1) and plate B (2) are determined according to the size of the measured oil chamber.

平板A(1)、平板B(2)厚度为2-5mm。The thickness of flat plate A (1) and flat plate B (2) is 2-5mm.

衬垫(3)材料为羊毛毡。The material of the pad (3) is wool felt.

衬垫(3)的厚度应保证和脱脂棉充分接触。The thickness of the liner (3) should ensure sufficient contact with the absorbent cotton.

衬垫(3)的长宽与平板A(1)、平板B(2)的长宽一致。The length and width of the pad (3) are consistent with the length and width of the flat plate A (1) and the flat plate B (2).

若干个平板A(1)、平板B(2)、衬垫(3),保证每一个平板A(1)、平板B(2)之间都设有一个衬垫(3)。Several flat plates A (1), flat plates B (2), and spacers (3) ensure that there is a spacer (3) between each flat plate A (1) and flat plate B (2).

本发明的优点是:将本发明布置于涡轮油室内的脱脂棉中,能实现含油量的在线检测。The advantage of the present invention is that the present invention is arranged in the absorbent cotton in the turbine oil chamber, so that the on-line detection of the oil content can be realized.

附图说明Description of drawings

图1是本发明的结构示意图。Figure 1 is a schematic structural diagram of the present invention.

图2是传感器应用示意图。Figure 2 is a schematic diagram of the sensor application.

具体实施方式Detailed ways

下面对本发明做进一步详细说明。参见图1、2,涡轮用脱脂棉中油量检测传感器,一种航空涡轮用叠片式油量检测传感器,由平板A(1)、平板B(2)、衬垫(3)、导线组成,若干个平板A(1)由同一根导线连接,若干个平板B(2)由另一根导线连接,且平板A(1)、平板B(2)之间不能发生短接;若干个衬垫依次(3)安装于平板A(1)与平板B(2)之间,平板A(1)、衬垫(3)与平板B(2)依次叠放,平板A(1)、衬垫(3)与衬垫(3)组成一个电容器。The present invention will be described in further detail below. Referring to Figures 1 and 2, a sensor for detecting oil level in absorbent cotton for turbines, a laminated oil level detection sensor for aviation turbines, is composed of a flat plate A (1), a flat plate B (2), a gasket (3), and a wire. One flat plate A (1) is connected by the same wire, and several flat plates B (2) are connected by another wire, and there can be no short circuit between flat plates A (1) and B (2); (3) Installed between plate A (1) and plate B (2), plate A (1), pad (3) and plate B (2) are stacked in sequence, plate A (1), pad (3) ) and pad (3) form a capacitor.

平板A(1)、平板B(2)材料为不锈钢。The material of the flat plate A (1) and the flat plate B (2) is stainless steel.

平板A(1)、平板B(2)长宽规格依据所测量油室的大小而定。The length and width specifications of plate A (1) and plate B (2) are determined according to the size of the measured oil chamber.

平板A(1)、平板B(2)厚度为2-5mm。The thickness of flat plate A (1) and flat plate B (2) is 2-5mm.

衬垫(3)材料为羊毛毡。所述羊毛毡一般都是由纯羊毛制作而成,也可以用牛毛或者纤维,利用加工粘合剂制成,主要具有丰富弹性,可作为防震、密封、衬垫和弹性钢丝针布底毡的材料,应用于产业机械防振、含油润滑、耐摩擦等。粘合性能耗,不易松散,可冲切制成各种形状的零件。组织紧密,空隙小,可作为良好的过滤材料,由于羊毛毡的密度紧凑性能较稳定可冲压生产各种毛毡零件。The material of the pad (3) is wool felt. The wool felt is generally made of pure wool, and can also be made of cow hair or fiber by using processing adhesives. Material, used in industrial machinery anti-vibration, oil-containing lubrication, friction resistance, etc. Adhesive energy consumption, not easy to loosen, can be punched into parts of various shapes. The organization is tight and the gap is small, which can be used as a good filter material. Due to the compact density and stable performance of wool felt, various felt parts can be produced by punching.

毛毡保湿性好,可以作为吸附道具,通过毛毡吸附的水量、油路来作为实验判断标准,稳定性好,对于实验测量的数据必不可少。Felt has good moisture retention and can be used as an adsorption prop. The amount of water and oil path absorbed by the felt can be used as the experimental judgment standard. It has good stability and is essential for experimental measurement data.

羊毛毡T132型羊毛毡为普通毛毡,细度不太明显,。密度0.1g-0.6g/cm3,羊毛的粗细度56支(27.1-29um)以下;Wool felt T132 type wool felt is ordinary felt, and the fineness is not obvious. The density is 0.1g-0.6g/cm 3 , and the thickness of wool is below 56 (27.1-29um);

矿物含量小于0.04%;Mineral content is less than 0.04%;

植物含量小于0.05%;Plant content is less than 0.05%;

拉力强度大于110kg(横向和纵向);The tensile strength is greater than 110kg (horizontal and vertical);

T132型羊毛毡也能满足本发明的操作需求。The T132 wool felt can also meet the operational requirements of the present invention.

衬垫(3)的厚度应保证和脱脂棉充分接触。衬垫(3)的厚度一般为1mm。The thickness of the liner (3) should ensure sufficient contact with the absorbent cotton. The thickness of the gasket (3) is generally 1 mm.

若平板A(1)、平板B(2)之间发生短接,将直接影响检测数据的准确性。If there is a short circuit between plate A (1) and plate B (2), it will directly affect the accuracy of the detection data.

衬垫(3)的长宽与平板A(1)、平板B(2)的长宽一致。The length and width of the pad (3) are consistent with the length and width of the flat plate A (1) and the flat plate B (2).

若干个平板A(1)、平板B(2)、衬垫(3),保证每一个平板A(1)、平板B(2)之间都设有一个衬垫(3),Several plates A (1), B (2), and pads (3), to ensure that there is a pad (3) between each plate A (1) and plate B (2),

衬垫(3)通过四周边缘与脱脂棉接触,并吸收脱脂棉内润滑油,直至达到平衡,衬垫(3)润滑油含量同步变化,衬垫(3)介电常数发生改变,由平板A(1)、平板B(2)与衬垫(3)组成的电容的电容值改变,检测电容值的变化,达到脱脂棉中油量检测目的,检测信号通过导线[4]传给测量、显示模块。The gasket (3) is in contact with the absorbent cotton through the surrounding edges, and absorbs the lubricating oil in the absorbent cotton until the balance is reached. The lubricating oil content of the gasket (3) changes synchronously, and the dielectric constant of the gasket (3) changes. ), the capacitance value of the capacitor composed of the flat plate B (2) and the pad (3) changes, and the change of the capacitance value is detected to achieve the purpose of detecting the oil content in the absorbent cotton. The detection signal is transmitted to the measurement and display module through the wire [4].

使用过程Use process

将本发明放置于棉花中,衬垫(3)接触脱脂棉并吸收脱脂棉内润滑油,直至达到平衡,随着脱脂棉中的润滑油含量变化(增大或减少),衬垫(3)润滑油含量同步变化,衬垫(3)介电常数发生改变,由平板A(1)、平板B(2)与衬垫(3)组成的电容的电容值改变,通过检测电容值的变化,达到脱脂棉中油量检测目的。检测信号通过导线[4]传给测量、显示模块。The present invention is placed in cotton, and the liner (3) contacts the absorbent cotton and absorbs the lubricating oil in the absorbent cotton until it reaches equilibrium. Synchronous changes, the dielectric constant of the pad (3) changes, and the capacitance value of the capacitor composed of the plate A (1), the plate B (2) and the pad (3) changes. Quantitative testing purposes. The detection signal is transmitted to the measurement and display module through the wire [4].

Claims (9)

1. The utility model provides an aviation is lamination formula oil mass detection sensor for turbine which characterized in that: the device is composed of flat plates A (1), flat plates B (2), a gasket (3) and wires, wherein the flat plates A (1) are connected by the same wire, the flat plates B (2) are connected by the other wire, and short circuit cannot occur between the flat plates A (1) and the flat plates B (2); a plurality of gaskets (3) are arranged between the flat plate A (1) and the flat plate B (2), the flat plate A (1), the gaskets (3) and the flat plate B (2) are sequentially stacked, and the flat plate A (1), the gaskets (3) and the gaskets (3) form a capacitor.
2. The laminated oil quantity detection sensor for an aviation turbine according to claim 1, wherein: the flat plate A (1) and the flat plate B (2) are made of metal materials.
3. The laminated oil quantity detection sensor for an aviation turbine according to claim 1, wherein: the length and width specifications of the flat plate A (1) and the flat plate B (2) are determined according to the size of the measured oil chamber.
4. The laminated oil quantity detection sensor for an aviation turbine according to claim 1, wherein: the thickness of the flat plate A (1) and the flat plate B (2) is 2-5 mm.
5. The laminated oil quantity detection sensor for an aviation turbine according to claim 1, wherein: the material of the pad (3) is wool felt.
6. The laminated oil quantity detection sensor for an aviation turbine according to claim 1, wherein: the thickness of the pad (3) is such that it is in sufficient contact with the cotton wool.
7. The laminated oil quantity detection sensor for an aviation turbine according to claim 1, wherein: the length and width of the pad (3) are consistent with those of the flat plate A (1) and the flat plate B (2).
8. The laminated oil quantity detection sensor for an aviation turbine according to claim 1, wherein: the flat plates A (1), the flat plates B (2) and the gaskets (3) ensure that one gasket (3) is arranged between each flat plate A (1) and each flat plate B (2).
9. The laminated oil quantity detection sensor for an aviation turbine according to claim 1, wherein: the pad (3) is contacted with the absorbent cotton through the peripheral edge and absorbs the lubricating oil in the absorbent cotton until balance is achieved, the lubricating oil content of the pad (3) is changed synchronously, the dielectric constant of the pad (3) is changed, the capacitance value of a capacitor formed by the flat plate A (1), the flat plate B (2) and the pad (3) is changed, the change of the capacitance value is detected, the purpose of detecting the oil content in the absorbent cotton is achieved, and a detection signal is transmitted to the measuring and displaying module through a lead.
CN202010553665.0A 2020-06-17 2020-06-17 A laminated fuel quantity detection sensor for aviation turbine Pending CN111796006A (en)

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Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4080593A (en) * 1975-10-09 1978-03-21 Linde Aktiengesellschaft Apparatus for the detection of liquid components in gases for dry-running compressors
CN1892189A (en) * 2005-07-04 2007-01-10 日本特殊陶业株式会社 Liquid condition sensing apparatus
CN101435788A (en) * 2008-12-17 2009-05-20 中国人民解放军国防科学技术大学 On-line oil liquid monitoring sensor based on permittivity measurement and system thereof
CN101738240A (en) * 2008-11-27 2010-06-16 苟阳明 Capacitance sensing type fuel meter
CN107854220A (en) * 2017-11-03 2018-03-30 小贵族科技有限公司 Electronic humidity sensing absorption article and humidity degree detection method thereof
CN208686450U (en) * 2018-06-08 2019-04-02 新乡航空工业(集团)有限公司 A kind of integrated cooling device
CN109996676A (en) * 2016-11-30 2019-07-09 Ppg工业俄亥俄公司 The aerospace transparent body with moisture transducer

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4080593A (en) * 1975-10-09 1978-03-21 Linde Aktiengesellschaft Apparatus for the detection of liquid components in gases for dry-running compressors
CN1892189A (en) * 2005-07-04 2007-01-10 日本特殊陶业株式会社 Liquid condition sensing apparatus
CN101738240A (en) * 2008-11-27 2010-06-16 苟阳明 Capacitance sensing type fuel meter
CN101435788A (en) * 2008-12-17 2009-05-20 中国人民解放军国防科学技术大学 On-line oil liquid monitoring sensor based on permittivity measurement and system thereof
CN109996676A (en) * 2016-11-30 2019-07-09 Ppg工业俄亥俄公司 The aerospace transparent body with moisture transducer
CN107854220A (en) * 2017-11-03 2018-03-30 小贵族科技有限公司 Electronic humidity sensing absorption article and humidity degree detection method thereof
CN208686450U (en) * 2018-06-08 2019-04-02 新乡航空工业(集团)有限公司 A kind of integrated cooling device

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Application publication date: 20201020