CN105300698B - A kind of fanjet ground experiment starting failure method for removing - Google Patents

A kind of fanjet ground experiment starting failure method for removing Download PDF

Info

Publication number
CN105300698B
CN105300698B CN201510811673.XA CN201510811673A CN105300698B CN 105300698 B CN105300698 B CN 105300698B CN 201510811673 A CN201510811673 A CN 201510811673A CN 105300698 B CN105300698 B CN 105300698B
Authority
CN
China
Prior art keywords
fanjet
starter
failture evacuation
ground experiment
box
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.)
Active
Application number
CN201510811673.XA
Other languages
Chinese (zh)
Other versions
CN105300698A (en
Inventor
姜凤
杨天南
刘岩飞
范世新
张凯
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 Shenyang Liming Aero Engine Co Ltd
Original Assignee
Shenyang Liming Aero Engine Group 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 Shenyang Liming Aero Engine Group Co Ltd filed Critical Shenyang Liming Aero Engine Group Co Ltd
Priority to CN201510811673.XA priority Critical patent/CN105300698B/en
Publication of CN105300698A publication Critical patent/CN105300698A/en
Application granted granted Critical
Publication of CN105300698B publication Critical patent/CN105300698B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Testing Of Engines (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)

Abstract

The present invention relates to a kind of fanjet ground experiment starting failure method for removing, this method passes through the situation to fanjet ground experiment starting different faults, first, carry out the setting failture evacuation of fanjet operating table surface switching plate, then, the starter starting failure that fanjet is equipped with is excluded, the starter power supply line failture evacuation equipped to fuse in fanjet contactless box and fanjet, carry out fanjet trigger circuit failure and starting ignition failture evacuation, fanjet fuel oil is carried out to uprush valve and interlock circuit failture evacuation, finally, carry out fanjet starter box peripheral circuit failture evacuation, until fanjet ground experiment starts normally, realize that fanjet ground experiment starting failure excludes.The inventive method excludes to fanjet ground experiment starting failure in a short time, saves the cost of time and failture evacuation.

Description

A kind of fanjet ground experiment starting failure method for removing
Technical field
The invention belongs to aero-engine fault diagnosis technique field, and in particular to a kind of fanjet ground experiment rises Dynamic troubleshooting methodology.
Background technology
Often there are various failures in fanjet ground experiment, and particularly starting failure is more frequent, fanjet Starting process it is relative complex, be related to starter, trigger circuit, start fuel feeding, start the factors such as ancillary equipment, every time therefore Barrier be required for taking a long time analyzed and processed, verification experimental verification, cause the fanjet troubleshooting time longer, verification experimental verification Cost is higher.
The content of the invention
In view of the shortcomings of the prior art, the present invention proposes a kind of fanjet ground experiment starting failure method for removing.
A kind of fanjet ground experiment starting failure method for removing, comprises the following steps:
Step 1:When ground experiment starting failure occurs for fanjet, fanjet operating table surface switching plate is judged Whether have and failure is set, if so, carrying out operating table surface switching plate sets failture evacuation, perform step 12, otherwise, perform step 2;
Step 2:Judge whether the equipped starter of fanjet starts, if so, performing step 3, otherwise, perform step 4;
Step 3:Judge whether the fanjet equipped starter working time disconnection phenomenon occurs in 5s~7s, if It is to perform step 5, otherwise, performs step 6;
Step 4:Judge whether fuse is working properly in fanjet contactless box, if so, carrying out fanjet Equipped starter power supply line failture evacuation, step 12 is performed, otherwise, change in fanjet contactless box and fuse Device, perform step 12;
Step 5:Judge the equipped starter of fanjet whether to work after 10s to occur disconnecting phenomenon, if so, performing step Rapid 7, otherwise, perform step 8;
Step 6:Fanjet trigger circuit failure and starting ignition failture evacuation are carried out, performs step 12;
Step 7:Carry out fanjet fuel oil to uprush valve and interlock circuit failture evacuation, perform step 12;
Step 8:Fanjet starter box is connect with+27V electricity, starter box plug X1 No. 33 contact pins are monitored with universal meter, Judge whether the 27V electricity of the contact pin occurs disconnecting phenomenon in 5s~7s, if so, then performing step 9, otherwise, carry out lubricating oil pressure Power bleeding, the air in lubricating oil pressure pipeline is excluded, perform step 12;
Step 9:Fanjet starter box is connect with+27V electricity, starter box plug X1 No. 14 contact pins are monitored with universal meter, Judge whether the 27V electricity of the contact pin occurs disconnecting phenomenon in 5s~7s, if so, then performing step 10, otherwise, open fuel oil and increase Press pump, perform step 12;
Step 10:Inserted with+27V electricity short circuit fanjet starter box plugs X1 No. 33 contact pins and No. 14 of plug X1 Pin, simulation lubricating oil pressure supply and fuel pressure supply, judge starter box within the 50s cycles whether normal work, if so, then holding Row step 11, otherwise, fanjet starter box is changed, perform step 12;
Step 11:Carry out fanjet starter box peripheral circuit failture evacuation;
Step 12:Fanjet ground experiment starts normally, realizes that fanjet ground experiment starting failure excludes.
The equipped starter power supply line failture evacuation of the fanjet includes:To fanjet starter The failture evacuation of power supply lines open circuit, and the event to fanjet starter power supply line insurance termination damage Barrier excludes.
Beneficial effects of the present invention:
The present invention proposes a kind of fanjet ground experiment starting failure method for removing, and the inventive method can make technology Personnel find the reason for fanjet ground experiment starting failure in a short time, and are excluded, and the row of being less prone to Unnecessary operation during therefore, save time and troubleshooting cost.
Brief description of the drawings
Fig. 1 is the flow chart of fanjet ground experiment starting failure method for removing in the specific embodiment of the invention.
Embodiment
The specific embodiment of the invention is described in detail below in conjunction with the accompanying drawings.
In present embodiment, fanjet starting process is double remaining controls, and one is time control, and one is rotating speed Control, rotating speed control is first choice, and when speed conditions deficiency, time control plays a role.
A kind of fanjet ground experiment starting failure method for removing, as shown in figure 1, comprising the following steps:
Step 1:When ground experiment starting failure occurs for fanjet, fanjet operating table surface switching plate is judged Whether have and failure is set, if so, carrying out operating table surface switching plate sets failture evacuation, perform step 12, otherwise, perform step 2。
Step 2:Judge whether the equipped starter of fanjet starts, if so, performing step 3, otherwise, perform step 4。
Step 3:Judge whether the fanjet equipped starter working time disconnection phenomenon occurs in 5s~7s, if It is to perform step 5, otherwise, performs step 6.
Step 4:Judge whether fuse is working properly in fanjet contactless box, if so, carrying out fanjet Equipped starter power supply line failture evacuation, step 12 is performed, otherwise, change in fanjet contactless box and fuse Device, perform step 12.
In present embodiment, the equipped starter power supply line failture evacuation of fanjet includes:Turbofan is sent out The failture evacuation of engine start electromechanical source supply line open circuit, and to fanjet starter power supply line guard terminal The failture evacuation of head damage.
Step 5:Judge the equipped starter of fanjet whether to work after 10s to occur disconnecting phenomenon, if so, performing step Rapid 7, otherwise, perform step 8.
Step 6:Fanjet trigger circuit failure and starting ignition failture evacuation are carried out, performs step 12.
In present embodiment, the resistance value of fanjet trigger circuit is detected with meter specially, if its resistance is infinite Big or more than 10 ohm, then fanjet trigger circuit failure, if its resistance is within 1 ohm, fanjet starts Circuit is normal, is measurement operational issue, it is necessary to re-operate if its resistance is between 1 ohm to 10 ohm.
In present embodiment, fanjet starting ignition failure:Fanjet starting ignition point is directly connected into behaviour Make the manual ignition switch on platform, if there is fanjet starting ignition failure, change igniter and judge trouble point again.
Step 7:Carry out fanjet fuel oil to uprush valve and interlock circuit failture evacuation, perform step 12.
In present embodiment, there is starter fuel feeding in fanjet starting process and fuel oil is uprushed fuel feeding, can use The resistance that meter specially detects magnetic valve in the output end of starter box judges, resistance between 20~60 ohm be it is normal, it is no Then, it is failure, then carries out fanjet fuel oil and uprush the replacing of part where valve.
Step 8:Fanjet starter box is connect with+27V electricity, starter box plug X1 No. 33 contact pins are monitored with universal meter, Judge whether the 27V electricity of the contact pin occurs disconnecting phenomenon in 5s~7s, if so, then performing step 9, otherwise, carry out lubricating oil pressure Power bleeding, the air in lubricating oil pressure pipeline is excluded, perform step 12.
Step 9:Fanjet starter box is connect with+27V electricity, starter box plug X1 No. 14 contact pins are monitored with universal meter, Judge whether the 27V electricity of the contact pin occurs disconnecting phenomenon in 5s~7s, if so, then performing step 10, otherwise, open fuel oil and increase Press pump, perform step 12.
Step 10:Inserted with+27V electricity short circuit fanjet starter box plugs X1 No. 33 contact pins and No. 14 of plug X1 Pin, simulation lubricating oil pressure supply and fuel pressure supply, judge starter box within the 50s cycles whether normal work, if so, then holding Row step 11, otherwise, fanjet starter box is changed, perform step 12.
Step 11:Carry out fanjet starter box peripheral circuit failture evacuation.
In present embodiment, remove outside failure and special point listed above, fanjet starter box also has many peripheries Circuit, includes the power supply of starter box, starter box receive other equipment to signal instruction, whether the signal line that starter box is sent Insulate normal failure, is investigated one by one.
Step 12:Fanjet ground experiment starts normally, realizes that fanjet ground experiment starting failure excludes.

Claims (2)

1. a kind of fanjet ground experiment starting failure method for removing, it is characterised in that comprise the following steps:
Step 1:When ground experiment starting failure occurs for fanjet, whether fanjet operating table surface switching plate is judged With failure is set, if so, carrying out operating table surface switching plate sets failture evacuation, step 12 is performed, otherwise, performs step 2;
Step 2:Judge whether the equipped starter of fanjet starts, if so, performing step 3, otherwise, perform step 4;
Step 3:Judge whether the fanjet equipped starter working time disconnection phenomenon occurs in 5s~7s, if so, Step 5 is performed, otherwise, performs step 6;
Step 4:Judge whether fuse is working properly in fanjet contactless box, be equipped with if so, carrying out fanjet Starter power supply line failture evacuation, perform step 12, otherwise, change fanjet contactless box in fuse, Perform step 12;
Step 5:Judge the equipped starter of fanjet whether to work after 10s to occur disconnecting phenomenon, if so, step 7 is performed, Otherwise, step 8 is performed;
Step 6:Fanjet trigger circuit failure and starting ignition failture evacuation are carried out, performs step 12;
Step 7:Carry out fanjet fuel oil to uprush valve and interlock circuit failture evacuation, perform step 12;
Step 8:Fanjet starter box is connect with+27V electricity, starter box plug X1 No. 33 contact pins are monitored with universal meter, is judged Whether the 27V electricity of the contact pin occurs disconnecting phenomenon in 5s~7s, if so, then performing step 9, otherwise, carries out lubricating oil pressure pipe Road is deflated, and excludes the air in lubricating oil pressure pipeline, performs step 12;
Step 9:Fanjet starter box is connect with+27V electricity, starter box plug X1 No. 14 contact pins are monitored with universal meter, is judged Whether the 27V electricity of the contact pin occurs disconnecting phenomenon in 5s~7s, if so, then performing step 10, otherwise, opens fuel pressurization Pump, perform step 12;
Step 10:With+27V electricity short circuit fanjet starter box plugs X1 No. 33 contact pins and plug X1 No. 14 contact pins, mould Intend lubricating oil pressure supply and fuel pressure supply, judge starter box within the 50s cycles whether normal work, if so, then performing step Rapid 11, otherwise, fanjet starter box is changed, perform step 12;
Step 11:Carry out fanjet starter box peripheral circuit failture evacuation;
Step 12:Fanjet ground experiment starts normally, realizes that fanjet ground experiment starting failure excludes.
2. fanjet ground experiment starting failure method for removing according to claim 1, it is characterised in that the whirlpool The equipped starter power supply line failture evacuation of fan engine includes:To fanjet starter power, supply line breaks The failture evacuation on road, and the failture evacuation to fanjet starter power supply line insurance termination damage.
CN201510811673.XA 2015-11-20 2015-11-20 A kind of fanjet ground experiment starting failure method for removing Active CN105300698B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510811673.XA CN105300698B (en) 2015-11-20 2015-11-20 A kind of fanjet ground experiment starting failure method for removing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510811673.XA CN105300698B (en) 2015-11-20 2015-11-20 A kind of fanjet ground experiment starting failure method for removing

Publications (2)

Publication Number Publication Date
CN105300698A CN105300698A (en) 2016-02-03
CN105300698B true CN105300698B (en) 2018-01-09

Family

ID=55198213

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510811673.XA Active CN105300698B (en) 2015-11-20 2015-11-20 A kind of fanjet ground experiment starting failure method for removing

Country Status (1)

Country Link
CN (1) CN105300698B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106959213A (en) * 2017-05-28 2017-07-18 西安成立航空制造有限公司 A kind of method for removing of fanjet afterburner ignition failure

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113310701B (en) * 2021-06-15 2022-06-10 中国人民解放军93208部队 Complete machine tester for mechanical system of military turbofan engine

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007224862A (en) * 2006-02-24 2007-09-06 Toyota Motor Corp Abnormal combustion predicting device
US7841184B2 (en) * 2007-04-19 2010-11-30 Pratt & Whitney Canada Corp. Start flow measurement
CN102944789B (en) * 2012-11-13 2015-12-09 沈阳黎明航空发动机(集团)有限责任公司 A kind of fanjet complete machine electrical system Gernral Check-up device and method
CN104748967B (en) * 2013-12-27 2017-10-31 中国航发商用航空发动机有限责任公司 Inhale the fanjet performance simulation pad optimization method under rain operating mode

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106959213A (en) * 2017-05-28 2017-07-18 西安成立航空制造有限公司 A kind of method for removing of fanjet afterburner ignition failure

Also Published As

Publication number Publication date
CN105300698A (en) 2016-02-03

Similar Documents

Publication Publication Date Title
CN105300698B (en) A kind of fanjet ground experiment starting failure method for removing
CN102890237A (en) Method and device for detecting faults of main touch point of high-voltage direct-current contact
CN102720595B (en) Engine overspeed protection and control method
CN102723909A (en) Active bleeder circuit of motor controller for electric car and control method thereof
CN103528769A (en) Sealing leakage test device for oil-immersed transformer
CN102944789B (en) A kind of fanjet complete machine electrical system Gernral Check-up device and method
CN104460744A (en) Cooling control method and cooling control system of large-capacity transformer
CN104237714B (en) Overvoltage integrated monitoring fault diagnosing device and method for transformer substation
CN109230272A (en) A kind of belt feeder hydraulic tensioning control device
CN106841981A (en) A kind of DF10D series cabs are without auxiliary power generation fault handling method
CN106274880A (en) A kind of brake boost control system and brake boost control method
WO2008107753B1 (en) Automated anti-explosion system and method for integrated-drive-generator
CN203009460U (en) Uninterruptible power supply overhaul device for hydraulic pressure gauge
CN203906017U (en) Emergency intercept device for isolating test signal
CN206773149U (en) Portable pressure device for checking electric relay
CN205779620U (en) Hydraulic system oil pump testing circuit
CN201351539Y (en) Electric control pneumatic fuel cut-off anti-runaway device
CN202370941U (en) Test platform for spare part of hydraulic switching mechanism
CN201638457U (en) Electronic control engine fault simulation control box for teaching
CN102472234B (en) For monitoring method and the mechanism of the device connecting starter
CN203929524U (en) Steel pipe hydrostatic testing automaton
CN203114489U (en) Bulldozer starting safety protection device
CN106404369A (en) Device and method for testing deterioration performance of bus pile head contact finger spring of switch cabinet
CN205013181U (en) Automatically controlled engine injector failure diagnosis device
CN221033053U (en) New energy vehicle's compressor verifying attachment

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant
CP01 Change in the name or title of a patent holder

Address after: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6

Patentee after: Chinese Hangfa Shenyang Liming Aero engine limited liability company

Address before: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6

Patentee before: Liming Aeroplane Engine (Group) Co., Ltd., Shenyang City

CP01 Change in the name or title of a patent holder