CN106600008A - HAZOP-based aircraft use maintenance process safety analysis method - Google Patents
HAZOP-based aircraft use maintenance process safety analysis method Download PDFInfo
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- CN106600008A CN106600008A CN201611086209.XA CN201611086209A CN106600008A CN 106600008 A CN106600008 A CN 106600008A CN 201611086209 A CN201611086209 A CN 201611086209A CN 106600008 A CN106600008 A CN 106600008A
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Abstract
The invention provides a HAZOP-based aircraft use maintenance process safety analysis method and belongs to the technical field of aircraft safety analysis. The method comprises: first collecting aircraft system data; decomposing the operation flow of a work card, extracting a number of nodes, describing each node; determining the design intention and the ideal state of the selected node; determining the deviation of the selected node; and finally, analyzing all reasons of the deviation of the selected node, determining whether the present safety measures are adequate according to the reasons, providing recommended measures if not in order to form an analysis report. The HAZOP-based aircraft use maintenance process safety analysis method can effectively identify safety risks of the key operations and the characteristic parameters in aircraft user technical information, provides recommendations for improvement in order to eliminate or control the danger and avoid man-made and design deviation in the complication and use of the user technical information, and effectively improve the safety of the user technical information.
Description
Technical field
The invention belongs to airborne vehicle safety analysis technique field, and in particular to a kind of airborne vehicle based on HAZOP is using dimension
Shield flow process Safety Analysis Method.
Background technology
The operation and maintenance process of helicopter is related to helicopter, flight unit, ground service engineering, user's technical data, makes
With key elements such as environment, core therein is the operating process of man-machine interaction.In this course, if equipment fault, artificial mistake
The reasons such as mistake, environmental effect cause flight unit, the operation of ground service engineering or equipment operation to deviate from rule of operation requirement, it is possible to
Cause dangerous generation.
The firsthand information of user's technical data as helicopter operation and maintenance, is that flight unit and ground service engineering are used
With the important evidence of attended operation.Therefore, the safety of user's technical data is directly connected to helicopter line and maintenance
Safety.But, conventional model user technical data does not carry out safety evaluation, and the safety of user's technical data is past
Toward the experience by designer and the responsibility of auditor.
Although also having carried out safety and operability verification in model to part handbook, such as flight airmanship, master are minimum
The chapters and sections affected on not resulting in helicopter flight safety and device damage in equipment list (MMEL) carried out Flight and
The direct fault location verification experimental verification in kind of the half of stand joint-trial, maintenance handbook have been carried out, but exist following
It is not enough:
Only it is checking, rather than comprehensively assesses in advance, does not meet security of system theory;
Flight, half direct fault location test in kind of stand joint-trial, on machine checking there is potential safety hazard;
Helicopter need to be arranged to take a flight test sortie or shutdown, expend substantial amounts of Sortie, man power and material.
Helicopter development and civil aircraft Certification experience have shown that, using the safety of the analytical technologies such as FHA, FTA, FMEA, ZSA
Property appraisal procedure be also recognize and control danger effective way, obtained the accreditation of user drawn game side.In consideration of it, for user
The dangerous discernment of technical data and control, the safety evaluation for carrying out certain analytical technology will also be effective methods.
Hazard and operability (HAZOP) is a kind of technical process risk analysis technology of chemical industry application angle, it
A kind of based on " introducer " seminar by multi-specialized composition of personnel by a series of meeting come it is implementing, to system
The method for qualitative analysis of the various deviations of detrimental consequences system identification in addition may be caused present in technique or operating process, can
For recognizing the structural workflow net of design defect, technical process danger and operational problem.
The content of the invention
This patent is based on HAZOP analytical technologies, it is proposed that airborne vehicle user's technical data safety evaluation flow process, node are carried
Take method, offset determination methods and analytical technology.User's technical data, as the random products for paying user, is that airborne vehicle is used
Main Basiss with safeguarding, there may be during being to look for user's technical data use based on the core of HAZOP analytical technologies
Deviation, and deviation is analyzed, determines reason and impact, recognize that the risk of current safety protective measure simultaneously proposes that improvement is built
View.
Airborne vehicle working service flow process Safety Analysis Method of the present invention based on HAZOP, including:
S1, the collection aircraft system data, the system documentation include Helicopter System and device performance parameters, set
Meter scheme and operation instruction, system and the layout of equipment, standard technology handbook and safety evaluation data;
S2, operating process decomposition is carried out to job card, if extracting dry contact, and each node is described, the section
Point refers to the point with design idea;
S3, the design idea and perfect condition that determine selected node;
S4, the deviation for determining selected node;
There are all reasons of deviation in S5, analysis selected node, determine whether existing safety measure fills according to the reason
Foot, if inadequate, there is provided suggestion and measure, ultimately forms analysis report.
Preferably, the node includes the pair of the key operations and description key operations degree of job card operating process
Word, the key operations refer to the work with design idea.
In such scheme preferably, the node includes the characteristic parameter and Expressive Features of job card operating process
The noun of parameter, the characteristic parameter refer to the parameter with design idea.
In such scheme preferably, the deviation in step S4 includes introducer and node.
In such scheme preferably, the reason for deviation occurs in the determination node includes determining the deviating cause
Dangerous key element, trigger mechanism and threat target danger three elements.
In such scheme preferably, the suggestion and measure includes that work for correction card and security protection code, modification set
Meter scheme, monitoring system, designer's protective measure are set, emergency response scheme, redundant system, more new equipment, again is formulated
One or more in selecting servicing area, test and strengthening training and train.
Based on the airborne vehicle O&M flow process safety analysiss technology of HAZOP analytical technologies, boat can be effectively recognized
The safety risks of the middle key operations and characteristic parameter of pocket user's technical data, propose that recommendation on improvement is eliminated or controls danger
Danger, it is to avoid the artificial deviation, design deviation during the establishment of user's technical data and use, effectively increases user's technical data
Safety, and then realize improve airborne vehicle operation and maintenance safety final purpose.
Description of the drawings
Fig. 1 is a preferred embodiment of the present invention based on the airborne vehicle working service flow process Safety Analysis Method of HAZOP
Flow chart.
Specific embodiment
To make purpose, technical scheme and the advantage of present invention enforcement clearer, below in conjunction with the embodiment of the present invention
Accompanying drawing, the technical scheme in the embodiment of the present invention is further described in more detail.In the accompanying drawings, identical from start to finish or class
As label represent same or similar element or the element with same or like function.Described embodiment is the present invention
A part of embodiment, rather than the embodiment of whole.It is exemplary below with reference to the embodiment of Description of Drawings, it is intended to use
It is of the invention in explaining, and be not considered as limiting the invention.Based on the embodiment in the present invention, ordinary skill people
The every other embodiment obtained under the premise of creative work is not made by member, belongs to the scope of protection of the invention.Under
Face combines accompanying drawing and embodiments of the invention is described in detail.
In describing the invention, it is to be understood that term " " center ", " longitudinal direction ", " horizontal ", "front", "rear",
The orientation or position relationship of the instruction such as "left", "right", " vertical ", " level ", " top ", " bottom " " interior ", " outward " is based on accompanying drawing institute
The orientation for showing or position relationship, are for only for ease of the description present invention and simplify description, rather than indicate or imply the dress of indication
Put or element with specific orientation, with specific azimuth configuration and operation, therefore it is not intended that must be protected to the present invention
The restriction of scope.
The present invention is described in further details below by embodiment.
Airborne vehicle working service flow process Safety Analysis Method of the present invention based on HAZOP, as shown in figure 1, including:
S1, the collection aircraft system data, the system documentation include Helicopter System and device performance parameters, set
Meter scheme and operation instruction, system and the layout of equipment, standard technology handbook and safety evaluation data;
S2, operating process decomposition is carried out to job card, if extracting dry contact, and each node is described, the section
Point refers to the point with design idea;
S3, the design idea and perfect condition that determine selected node;
S4, the deviation for determining selected node;
There are all reasons of deviation in S5, analysis selected node, determine whether existing safety measure fills according to the reason
Foot, if inadequate, there is provided suggestion and measure, ultimately forms analysis report.
This patent is based on HAZOP analytical technologies, it is proposed that airborne vehicle user's technical data safety evaluation flow process, node are carried
Take method, offset determination methods and analytical technology.User's technical data, as the random products for paying user, is that airborne vehicle is used
Main Basiss with safeguarding, there may be during being to look for user's technical data use based on the core of HAZOP analytical technologies
Deviation, and deviation is analyzed, determines reason and impact, recognize that the risk of current safety protective measure simultaneously proposes that improvement is built
View.
(1) analysis object, collection system data are determined.Including helicopter, system and device performance parameters, design and
Operation instruction, system/device layout drawing, standard technology handbook, safety evaluation data etc..
(2) object, partitioning site are decomposed.Operating process decomposition is carried out to job card, if dry contact is extracted, and to each section
Point is accurately described, and makes each node have independent design idea.Each node is generally job card operating process
Key operations, characteristic parameter, and adverbial word, the noun (object) of Expressive Features parameter of description key operations degree.It is crucial dynamic
Such as open, close, close, press, check;Characteristic parameter such as speed, moment of torsion, oil mass, angle, overload factor, lever operation
Amount etc.;Description key operations degree adverbial word such as promptly, little by little, lentamente, less than, be not more than, be not less than;Description
The noun (object) of characteristic parameter should be related to design configuration or maintained equipment, instrument in extract operation program or operation instruction
Noun, such as steering wheel, electrodynamic pump, stick, rotor rotating speed etc..
(3) clear and definite nodal function.Confirm selected node, specify its design idea, perfect condition.Design idea or reason
Think that state is determined according to system documentation and the design requirement collected, it is the acceptable criterion of the node, including the conjunction of key operations
The boundary condition of reason state and characteristic parameter.For example to operating process " controlling rotor rotating speed 90%~120% ", " rotor turns
Speed 90%~120% " is extracted as node, and according to the system documentation for collecting, " rotor rotating speed should be maintained at 90%~120%
(275r/m i n~367r/m i n) ", so the node meets design idea.
(4) determine significant deviation.All previously given introducers are applied successively, determine that each node is significant partially
Difference, i.e., the deviation that each node is likely to occur, deviation are the combination of introducer and node.HAZOP analysis methods are based on introducer
, main introducer includes "None", " deficiency ", " exceeding ", " adjoint ", " part ", " contrary ", "abnormal".Deviation=guiding
Word+node (adverbial word+verb, eigenvalue).Introducer is combined one by one with node, deviation is constituted, according to design idea, is filtered out
Significant deviation, as the object of variance analyses.It is for example with " rotor rotating speed 90%~120% " as node, significant inclined
Difference including " being not specified by the rotor range of speeds 90%~120% ", " the rotor range of speeds of regulation be less than 90% ", " regulation
The rotor range of speeds is higher than 120% ".
(5) deviation is analyzed.Dangerous key element, trigger mechanism and threat target danger three elements are analyzed, are known
The dangerous three elements not deviated, and analyze the reason for each node causes deviation and impact.Should analyze causes all originals of deviation
Cause, may cause different impacts, and then whether the existing safety precautions of analysis is sufficient, and propose under different reason situations
With regard to the recommendation on improvement of safety measure.The corrective measure one of the analysis of causes, impact analysis, existing safety precautions and suggestion
As it is as follows:
The analysis of causes:Carry out meeting during the analysis of causes different because node type, deviation are different, but should in concrete analysis
Consider based on node itself and input and output.It should be noted that herein the reason for be not only equipment fault, more to
Consider the mistake of human operational error and job card establishment.It is general to consider from the following aspects:Mechanical clamping stagnation, control failure,
Exotic entrance, the failure of burn into pipeline, operational error, operation require that imprecise, operation requires to retouch beyond plan boundary, word
State and be not inconsistent with material object;
Impact analysis:The impact that analysis deviation brings is considered as to flight unit, ground service engineering, helicopter, equipment and ring
The impact in border, and do not consider existing safety precautions.Whole machine/systemic-function hazard analysises (FHA), system/set can be used for reference
Standby failure mode and effect analysis (FMEA), system/device fault tree analysiss (FTA), region security analysis (ZSA) and occupation
The safety evaluation material such as health hazard analysis.It is general to consider from the following aspects:Fire, blast, toxic gas, the energy are damaged
Mistake, helicopter/device damage, casualties etc..
Existing safety precautions:Refer to security protection code of safety prevention measure or regulation of design etc., to inclined
When difference is analysed, the generation that can existing safety precautions effectively eliminate or control danger should be analyzed, to identify design
Leak and potential safety hazard in terms of defect or operation sequence, to be corrected in time.General safety precautions has:Report to the police
Device, preventer, security protection code, personal protection measure, inspection detection, flight unit/ground service engineering training etc..
Suggestion and measure:It is general to consider from the following aspects:Work for correction card and security protection code, Amending design side
Case, monitoring system, designer's protective measure are set, are formulated emergency response scheme, redundant system, more new equipment, reselected
Servicing area, test, reinforcement training and training.
(6) interpretation of result work out report.According to above-mentioned analysis result, it is confirmed whether also there is deviation.If nothing, analyze
Complete, work out HAZOP analysis reports.
Based on the airborne vehicle O&M flow process safety analysiss technology of HAZOP analytical technologies, boat can be effectively recognized
The safety risks of the middle key operations and characteristic parameter of pocket user's technical data, propose that recommendation on improvement is eliminated or controls danger
Danger, it is to avoid the artificial deviation, design deviation during the establishment of user's technical data and use, effectively increases user's technical data
Safety, and then realize improve airborne vehicle operation and maintenance safety final purpose.
It is last it is to be noted that:Above example only to illustrate technical scheme, rather than a limitation.To the greatest extent
Pipe has been described in detail to the present invention with reference to the foregoing embodiments, it will be understood by those within the art that:Which is still
Technical scheme described in foregoing embodiments can be modified, or equivalent is carried out to which part technical characteristic and replace
Change;And these modifications or replacement, do not make the essence of appropriate technical solution depart from the essence of various embodiments of the present invention technical scheme
God and scope.
Claims (6)
1. a kind of airborne vehicle working service flow process Safety Analysis Method based on HAZOP, it is characterised in that include:
S1, the collection aircraft system data, the system documentation include Helicopter System and device performance parameters, design side
Case and operation instruction, system and the layout of equipment, standard technology handbook and safety evaluation data;
S2, operating process decomposition is carried out to job card, if extracting dry contact, and each node is described, the node is
Finger includes the point with design idea;
S3, the design idea and perfect condition that determine selected node;
S4, the deviation for determining selected node;
There are all reasons of deviation in S5, analysis selected node, determine whether existing safety measure is sufficient according to the reason, if
It is inadequate, there is provided suggestion and measure, ultimately form analysis report.
2. the airborne vehicle working service flow process Safety Analysis Method based on HAZOP as claimed in claim 1, its feature exist
In the node includes the adverbial word of the key operations of job card operating process and description key operations degree, described crucial dynamic
Refer to the work with design idea.
3. the airborne vehicle working service flow process Safety Analysis Method based on HAZOP as claimed in claim 1, its feature exist
In the node includes the noun of the characteristic parameter of job card operating process and Expressive Features parameter, and the characteristic parameter is
Refer to the parameter with design idea.
4. the airborne vehicle working service flow process Safety Analysis Method based on HAZOP as claimed in claim 1, its feature exist
In the deviation in step S4 includes introducer and node.
5. the airborne vehicle working service flow process Safety Analysis Method based on HAZOP as claimed in claim 1, its feature exist
In described to determine that node includes determining dangerous key element, trigger mechanism and the threat of the deviating cause the reason for there is deviation
Target danger three elements.
6. the airborne vehicle working service flow process Safety Analysis Method based on HAZOP as claimed in claim 1, its feature exist
In the suggestion and measure includes work for correction card and security protection code, Amending design scheme, arranges monitoring system, arranges people
Member protective measure, formulate emergency response scheme, redundant system, more new equipment, reselect servicing area, test and strengthen training
One or more in instruction and training.
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Cited By (4)
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CN109146228A (en) * | 2018-06-26 | 2019-01-04 | 沈阳透平机械股份有限公司 | The data analysing method and device of centrifugal compressor |
CN109711747A (en) * | 2019-01-03 | 2019-05-03 | 济南大学 | A kind of HAZOP analysis method of amusement facility |
CN110356582A (en) * | 2018-04-09 | 2019-10-22 | 株式会社斯巴鲁 | Aircraft management system |
CN111489076A (en) * | 2020-04-07 | 2020-08-04 | 顾敏 | Integrated process hazard analysis method, system and storage medium |
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Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110356582A (en) * | 2018-04-09 | 2019-10-22 | 株式会社斯巴鲁 | Aircraft management system |
CN109146228A (en) * | 2018-06-26 | 2019-01-04 | 沈阳透平机械股份有限公司 | The data analysing method and device of centrifugal compressor |
CN109146228B (en) * | 2018-06-26 | 2023-01-06 | 沈阳透平机械股份有限公司 | Data analysis method and device for centrifugal compressor |
CN109711747A (en) * | 2019-01-03 | 2019-05-03 | 济南大学 | A kind of HAZOP analysis method of amusement facility |
CN111489076A (en) * | 2020-04-07 | 2020-08-04 | 顾敏 | Integrated process hazard analysis method, system and storage medium |
CN111489076B (en) * | 2020-04-07 | 2023-09-15 | 顾敏 | Integrated process hazard analysis method, system and storage medium |
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Application publication date: 20170426 |