CN202815951U - History recorder of engine - Google Patents

History recorder of engine Download PDF

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Publication number
CN202815951U
CN202815951U CN 201220393804 CN201220393804U CN202815951U CN 202815951 U CN202815951 U CN 202815951U CN 201220393804 CN201220393804 CN 201220393804 CN 201220393804 U CN201220393804 U CN 201220393804U CN 202815951 U CN202815951 U CN 202815951U
Authority
CN
China
Prior art keywords
counter
engine
control unit
ecu
electrical control
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN 201220393804
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Chinese (zh)
Inventor
喻承恩
桂晓玉
陈丽
袁伟
李明
成亮
沈领
王进
王扩军
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
AECC South Industry Co Ltd
Original Assignee
China National South Aviation Industry Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by China National South Aviation Industry Co Ltd filed Critical China National South Aviation Industry Co Ltd
Priority to CN 201220393804 priority Critical patent/CN202815951U/en
Application granted granted Critical
Publication of CN202815951U publication Critical patent/CN202815951U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model discloses a history recorder of an engine. The history recorder comprises a first counter for recording the actual frequency of mechanical stress experienced by parts of the engine, a second counter for recording the actual frequency of high-temperature stress experienced by the parts of the engine, a third counter for recording temperature-time indexes of a gas turbine outlet of the engine, and a fourth counter for recording the actual running time of the engine, wherein the first counter, the second counter, the third counter and the fourth counter are connected with an electronic control unit of the engine through an electric connector. The history recorder of the engine has the characteristics of high counting accuracy and high reliability.

Description

A kind of history recorder of engine
Technical field
The utility model relates to the field of accessories of engine, especially, relates to a kind of history recorder of engine.
Background technology
Engine, especially aeromotor need engine total run time, the tired number of cycle of engine and time humidity index are carried out record.
There is no at present special-purpose history recorder above data are carried out record, inconvenience checks that the running of engine is historical, is unfavorable for the judgement of engine maintenance and fault.Although engine total run time, the tired number of cycle of engine and time humidity index can be inquired about inquiry inconvenience in engine electric-controlled unit (ECU); Particularly work as engine and break down, when causing ECU (Electrical Control Unit) (ECU) outage, historical record is easily lost.
The utility model content
The utility model purpose is to provide the history recorder of the high engine of a kind of counting precision height and reliability, checks and record the technical matters of easily losing to solve the inconvenience of engine running record.
For achieving the above object, the utility model provides a kind of history recorder of engine, comprising:
The first counter, the parts that are used for recording engine experience the actual frequency of mechanical stress;
The second counter, the parts that are used for recording engine experience the actual frequency of high temperature stress;
The 3rd counter is for the gas turbine outlet temperature-time index of recording engine;
Four-counter is for the real-world operation time of recording engine;
Described the first counter, described the second counter, described the 3rd counter and described four-counter all link to each other with the ECU (Electrical Control Unit) of engine by electric connector.
As a further improvement on the present invention:
Described the first counter, described the second counter, described the 3rd counter and described four-counter are the counter that shows wheel with mechanical digital.
The count pulse output terminal of the parts of engine experience mechanical stress links to each other in the negative pole of described the first counter and the described ECU (Electrical Control Unit); The count pulse output terminal of the parts of engine experience high temperature stress links to each other in the negative pole of described the second counter and the described ECU (Electrical Control Unit); The pulse output end of the gas turbine outlet temperature-time index of engine links to each other in the negative pole of described the 3rd counter and the described ECU (Electrical Control Unit); The pulse output end of the real-world operation time of engine links to each other in the negative pole of described four-counter and the described ECU (Electrical Control Unit); The anodal of described the first counter, described the second counter, described the 3rd counter and described four-counter all is connected with operating voltage in the described ECU (Electrical Control Unit).
Described the first counter, described the second counter, described the 3rd counter and described four-counter all are installed in the housing, are positioned at described the first counter, described the second counter, described the 3rd counter and described four-counter place on the described housing and are provided with face glass.
Described electric connector is located on the described housing.
Also be provided with the second binding post on the described housing, described the second binding post is connected by the negative pole of commutation diode with described four-counter.
The utlity model has following beneficial effect:
1, the history recorder of engine of the present utility model, adopt No. four counters to cyclic fatigue number (number of times of experience mechanical stress and high temperature stress), total run time and the time humidity index etc. of engine, the real-world operation situation after but recording engine dispatches from the factory, to judge as engine maintenance, fault and the foundation of the durability analysis of engine, be applicable to the engine of various models, be particularly useful for aeromotor.
2, the history recorder of engine of the present utility model, No. four counters are connected the counting precision height with corresponding pulses output in the ECU (Electrical Control Unit) respectively; Employing is counted with the counter of mechanical digital demonstration wheel and is shown, electric signal can be converted into mechanical signal, and count with the digital wheel of mechanical rotation, is difficult for losing so that data show, the registering instrument reliability is higher.
Except purpose described above, feature and advantage, the utility model also has other purpose, feature and advantage.The below is described in further detail the utility model with reference to figure.
Description of drawings
The accompanying drawing that consists of the application's a part is used to provide further understanding of the present utility model, and illustrative examples of the present utility model and explanation thereof are used for explaining the utility model, do not consist of improper restriction of the present utility model.In the accompanying drawings:
Fig. 1 is the electric circuit constitute synoptic diagram of the utility model preferred embodiment;
Fig. 2 is the mounting structure synoptic diagram of the history recorder of the utility model preferred embodiment;
Fig. 3 be Fig. 2 look up structure (lower cover is unkitted state) synoptic diagram;
Fig. 4 is the right TV structure synoptic diagram of Fig. 2.
Marginal data:
1, the first counter; 2, the second counter; 3, the 3rd counter; 4, four-counter; 5, electric connector; 6, housing; 7, the first binding post; 8, the second binding post; 9, the 3rd binding post; 10, commutation diode; 11, mooring bolt; 12, face glass.
Embodiment
Below in conjunction with accompanying drawing embodiment of the present utility model is elaborated, but the multitude of different ways that the utility model can be defined by the claims and cover is implemented.
As shown in Figure 1, the history recorder of engine of the present utility model comprises:
The first counter 1, the parts that are used for recording engine experience the actual frequency of mechanical stress;
The second counter 2, the parts that are used for recording engine experience the actual frequency of high temperature stress;
The 3rd counter 3 is for the gas turbine outlet temperature-time index of recording engine;
Four-counter 4 is for the real-world operation time of recording engine;
The first counter 1, the second counter 2, the 3rd counter 3 and four-counter 4 all link to each other by the ECU (Electrical Control Unit) (ECU, not shown) of electric connector 5 with engine.Adopt No. four counters to cyclic fatigue number (number of times of experience mechanical stress and high temperature stress), total run time and the time humidity index etc. of engine, the real-world operation situation after but recording engine dispatches from the factory, to judge as engine maintenance, fault and the foundation of the durability analysis of engine, be applicable to the engine of various models, be particularly useful for the running history of aeromotor is carried out record.
In the present embodiment, the first counter 1, the second counter 2, the 3rd counter 3 and four-counter 4 are the counter that shows wheel with mechanical digital.No. four counters are connected the counting precision height with corresponding pulses output in the ECU (Electrical Control Unit) respectively; Employing is counted with the counter of mechanical digital demonstration wheel and is shown, electric signal can be converted into mechanical signal, and count with the digital wheel of mechanical rotation, is difficult for losing so that data show, the registering instrument reliability is higher.
In the present embodiment, as shown in Figure 1, the count pulse output terminal of the parts of engine experience mechanical stress links to each other in the negative pole of the first counter 1 and the ECU (Electrical Control Unit); The count pulse output terminal of the parts of engine experience high temperature stress links to each other in the negative pole of the second counter 2 and the ECU (Electrical Control Unit); The pulse output end of the gas turbine outlet temperature-time index of engine links to each other in the negative pole of the 3rd counter 3 and the ECU (Electrical Control Unit); The pulse output end of the real-world operation time of engine links to each other in the negative pole of four-counter 4 and the ECU (Electrical Control Unit); The anodal of the first counter 1, the second counter 2, the 3rd counter 3 and four-counter 4 all is connected with operating voltage in the ECU (Electrical Control Unit).When the ECU (Electrical Control Unit) on the engine is sent a counting pulse signal, by a road in electric connector 5 inputs No. four counters on the history recorder, the digital wheel of this a counter position adds 1, when digital wheel position to 9 the time, then to ten carries of digital wheel, the like, the digital wheel of counter is the afterpulsing signalizing activity continuously, thereby realizes the purpose of counting.
In the present embodiment, such as Fig. 1, Fig. 2, Fig. 3, shown in Figure 4, the first counter 1, the second counter 2, the 3rd counter 3 and four-counter 4 all are installed in the housing 6, and housing 6 installs on rack or the operating table surface by three mooring bolts 11.Be positioned at the first counter 1, the second counter 2, the 3rd counter 3 and four-counter 4 places on the housing 6 and be provided with face glass 12.The anodal first tandem of the first counter 1, the second counter 2, the 3rd counter 3 and four-counter 4 is on the first binding post.Also be provided with the second binding post 8 in the housing 6.The second binding post 8 is connected with the negative pole of commutation diode 10, and the positive pole of commutation diode 10 and the negative pole of four-counter 4 are connected on the 3rd binding post 8.Electric connector 5 links to each other with the ECU (Electrical Control Unit) of engine on the housing 6 by being located at for the negative pole of four counters, the first binding post and the second binding post 8.Commutation diode 10 is for the protection of four-counter 4.During actual the use, the housing integral sealing, electric connector 5 and the first binding post 7, the second binding post 8, the 3rd binding post 9 places all adopt and are threaded and adopt silicon rubber to seal, and are waterproof dustproof, and can play the effect of anti-electromagnetic interference (EMI).
The above is preferred embodiment of the present utility model only, is not limited to the utility model, and for a person skilled in the art, the utility model can have various modifications and variations.All within spirit of the present utility model and principle, any modification of doing, be equal to replacement, improvement etc., all should be included within the protection domain of the present utility model.

Claims (6)

1. the history recorder of an engine is characterized in that, comprising:
The first counter (1), the parts that are used for recording engine experience the actual frequency of mechanical stress;
The second counter (2), the parts that are used for recording engine experience the actual frequency of high temperature stress;
The 3rd counter (3) is for the gas turbine outlet temperature-time index of recording engine;
Four-counter (4) is for the real-world operation time of recording engine;
Described the first counter (1), described the second counter (2), described the 3rd counter (3) and described four-counter (4) all link to each other with the ECU (Electrical Control Unit) of engine by electric connector (5).
2. the history recorder of engine according to claim 1, it is characterized in that described the first counter (1), described the second counter (2), described the 3rd counter (3) and described four-counter (4) are the counter that shows wheel with mechanical digital.
3. the history recorder of engine according to claim 2 is characterized in that,
The count pulse output terminal of the parts of engine experience mechanical stress links to each other in the negative pole of described the first counter (1) and the described ECU (Electrical Control Unit);
The count pulse output terminal of the parts of engine experience high temperature stress links to each other in the negative pole of described the second counter (2) and the described ECU (Electrical Control Unit);
The pulse output end of the gas turbine outlet temperature-time index of engine links to each other in the negative pole of described the 3rd counter (3) and the described ECU (Electrical Control Unit);
The pulse output end of the real-world operation time of engine links to each other in the negative pole of described four-counter (4) and the described ECU (Electrical Control Unit);
The anodal of described the first counter (1), described the second counter (2), described the 3rd counter (3) and described four-counter (4) all is connected with operating voltage in the described ECU (Electrical Control Unit).
4. the history recorder of each described engine in 3 according to claim 1, it is characterized in that, described the first counter (1), described the second counter (2), described the 3rd counter (3) and described four-counter (4) all are installed in the housing (6), are positioned at described the first counter (1), described the second counter (2), described the 3rd counter (3) and described four-counter (4) on the described housing (6) and locate to be provided with face glass (12).
5. the history recorder of engine according to claim 4 is characterized in that, described electric connector (5) is located on the described housing (6).
6. the history recorder of engine according to claim 5, it is characterized in that, also be provided with the second binding post (8) on the described housing (6), described the second binding post (8) is connected with the negative pole of described four-counter (4) by commutation diode (10).
CN 201220393804 2012-08-09 2012-08-09 History recorder of engine Expired - Fee Related CN202815951U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201220393804 CN202815951U (en) 2012-08-09 2012-08-09 History recorder of engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201220393804 CN202815951U (en) 2012-08-09 2012-08-09 History recorder of engine

Publications (1)

Publication Number Publication Date
CN202815951U true CN202815951U (en) 2013-03-20

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201220393804 Expired - Fee Related CN202815951U (en) 2012-08-09 2012-08-09 History recorder of engine

Country Status (1)

Country Link
CN (1) CN202815951U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107103658A (en) * 2017-04-25 2017-08-29 哈尔滨工业大学 Aerial engine air passage method for detecting abnormality based on deep learning and Gaussian Profile

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107103658A (en) * 2017-04-25 2017-08-29 哈尔滨工业大学 Aerial engine air passage method for detecting abnormality based on deep learning and Gaussian Profile
CN107103658B (en) * 2017-04-25 2019-05-14 哈尔滨工业大学 Aerial engine air passage method for detecting abnormality based on deep learning and Gaussian Profile

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C14 Grant of patent or utility model
GR01 Patent grant
CP01 Change in the name or title of a patent holder

Address after: 412002 Dong Jiaduan, Zhuzhou, Hunan

Patentee after: China Hangfa South Industrial Co. Ltd.

Address before: 412002 Dong Jiaduan, Zhuzhou, Hunan

Patentee before: China Southern Airlines Industry (Group) Co., Ltd.

CP01 Change in the name or title of a patent holder
CP01 Change in the name or title of a patent holder

Address after: 412002 Dong Jiaduan, Zhuzhou, Hunan

Patentee after: China Hangfa South Industrial Co. Ltd.

Address before: 412002 Dong Jiaduan, Zhuzhou, Hunan

Patentee before: China Southern Airlines Industry (Group) Co., Ltd.

CP01 Change in the name or title of a patent holder
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20130320

Termination date: 20200809

CF01 Termination of patent right due to non-payment of annual fee