CN108229705B - Missile weapon equipment damage mode and influence analysis method - Google Patents

Missile weapon equipment damage mode and influence analysis method Download PDF

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CN108229705B
CN108229705B CN201810082412.2A CN201810082412A CN108229705B CN 108229705 B CN108229705 B CN 108229705B CN 201810082412 A CN201810082412 A CN 201810082412A CN 108229705 B CN108229705 B CN 108229705B
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陶小创
何俊
曲丽丽
倪晓峰
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Beijing Institute of Electronic System Engineering
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Abstract

The invention discloses a method for analyzing damage modes and influences of missile weaponry, which comprises the following steps: 1) analyzing a damage mechanism; 2) determining a damage mode; 3) evaluating the technical process and the potential damage risk level thereof; 4) designing an improvement measure; 5) and determining a damage maintenance support work project. The invention constructs a damage mode and an influence analysis method of missile weaponry in which the battle threats, special events and technical processes are comprehensively considered, makes up the limitation and one-sidedness that the current DMEA method only considers the battle damage, and has strong operability and higher engineering application value.

Description

Missile weapon equipment damage mode and influence analysis method
Technical Field
The invention relates to a damage mode and an influence analysis method, in particular to a missile weapon equipment damage mode and an influence analysis method.
Background
Along with the continuous improvement of the informatization, intellectualization and integration level of missile weaponry equipment, the equipment technology advancement, the function integration and the structural complexity are higher and higher, and simultaneously, the missile weaponry equipment faces more harsh and harsh working and operating environments and complex and variable, omnibearing and multi-factor attack threatening operation environments. The equipment maintenance guarantee problem caused by the damage multifarities, fatality, randomness and crosslinking is prominent day by day, the high survivability, the high reliability, the high task safety and the high success rate are ensured to become the core requirements of the missile weapon equipment on the high fighting capacity, and the damage mode and the influence analysis related engineering application research are particularly urgent in the fields of missile weapon equipment reliability engineering and comprehensive guarantee engineering.
Damage Mode and Effects Analysis (DMEA) is a process and technique for analyzing the form and extent of Damage due to combat Damage. The DMEA takes various combat damage modes suffered by equipment in combat as objects, analyzes the influence of different combat damages on the equipment and the functions and performances of the equipment, finds out weak links according to the analysis result, and proposes improved measures and suggestions such as design, maintenance, operation and the like. Therefore, the DMEA method recommended by GJB/Z1391-2006 and the current DMEA engineering application research mainly focus on the battle damage caused by the threat of hostile attack, and the limitations are shown as follows: damage caused by related special events (such as abnormal use, loading, unloading, storage, transportation and natural environment) in the use and operation processes of the equipment and damage caused by damage sensitivity of a new technology process adopted by the equipment are not systematically considered, so that all possible damage modes and damage mechanisms of the equipment in the use process cannot be comprehensively mastered, and high-viability design and rapid first-aid repair work analysis of the equipment are severely limited.
Therefore, it is necessary to provide an analysis method which can comprehensively analyze all possible damage modes in the use process of missile weaponry and simultaneously provide a scientific, realistic and feasible system for designing equipment survivability, reliability and task safety and analyzing rapid first-aid repair work.
Disclosure of Invention
The invention aims to provide a missile weapon equipment damage mode and an influence analysis method considering battle threats, special events and technical processes, and solves the problems that the equipment damage mode and mechanism analysis are incomplete and not deep in the existing DMEA method, and equipment survivability, reliability, task safety design and rapid repair work analysis are not complete due to the incomplete problem.
In order to achieve the purpose, the invention adopts the following technical scheme:
the invention provides a method for analyzing damage modes and influences of missile weaponry, which comprises the following steps:
1) analyzing a damage mechanism:
according to the equipment life section, the mission section and the environment section, carrying out damage mechanism analysis from three aspects of battle threats, special events and technical processes;
2) determining a damage mode:
decomposing and analyzing all task stages and working modes of the equipment according to the service life section and the task section of the equipment; on the basis of comprehensively decomposing and identifying task stages and working modes, various damage mechanisms are superposed on each task stage and working mode of the equipment using process, and all possible damage modes of the equipment caused by the action process of specific mechanisms of battle threats, special events and technical processes in each task stage and each working mode are analyzed and identified one by one;
3) evaluating the technical process and the potential damage risk level:
analyzing the technical processes adopted by each subsystem or equipment of the equipment, associating the technical processes adopted by the equipment with a damage mode, analyzing and evaluating the risk of the equipment due to the potential damage of the technical process in a correlation manner from two aspects of the maturity of the technical process and the potential damage sensitivity of the technical process, and evaluating the level of the potential damage risk of the technical process;
4) designing improvement measures:
aiming at various analyzed damage modes, by combining damage mechanism and technical process analysis, researching and determining design improvement measures for avoiding or eliminating the damage modes from four aspects of enemy prevention finding design, damage prevention design, technical process optimization and damage maintenance guarantee design and maintenance, testability and guarantee design measures for improving equipment damage recovery capacity;
5) determining damage maintenance guarantee work items:
and analyzing and determining damage maintenance guarantee work items which are necessary to be adopted for repairing the corresponding damage mode according to the damage mode, the task stage and the working mode, the damage mechanism and the damage risk information obtained by analysis, and further analyzing the requirements of related maintenance guarantee resources.
Further, the battle threat in step 1) is all possible causes or factors of equipment damage caused by enemy attack, enemy attack (i.e. own use) or own use behavior of the battle environment in the battlefield environment;
the special event is an abnormal use action or unexpected condition that causes accidental damage to equipment during a life cycle;
the technical process is a potentially damage sensitive technique and process conditions employed in the design and manufacture of equipment.
Further, the task stage in the step 2) comprises technical preparation, marching maneuvering, unfolding, withdrawing, launching preparation, launching, active flight, passive flight, transportation, loading and unloading, transshipment, storage, training, maintenance and the like;
the modes of operation include full load, partial load, continuous operation, intermittent operation, remote operation, in-situ operation, parallel operation, serial operation, degraded use, normal use, and the like.
The damage modes include perforation, deformation, separation, shattering, fracture, rupture, breaking, sticking, dislocation, plugging, shedding, fire, explosion, burnout, fragment impact, nuclear contamination, biochemical contamination, gas leak, water leak, oil leak, tire burst, exposure to moisture, corrosion, delamination, open circuit, short circuit, ionization, burn-through, blindness, stall, system crash, runaway, power outage, localized high temperature, condensation, accidental ignition, breakage, and the like.
Further, the maturity of the technical process in the step 3) is divided into a mature technical process, a relatively mature technical process and a novel technical process; wherein, the mature technical process means that the technical process is already applied to a plurality of similar equipment; the mature technical process means that the technical process is already applied to part of similar equipment, but a little improvement is made in the equipment; the novel technical process means that the technical process has been applied in a similar new device, but lacks relevant feedback information.
The potential damage sensitivity of the technical process is divided into extremely low sensitivity, medium sensitivity, high sensitivity and extremely high sensitivity; wherein, the extremely low sensitivity is in the whole life cycle of the equipment, and the technical process has extremely low damage chance; the low sensitivity is in the whole life cycle of the equipment, and the technical process has lower damage chance; the medium sensitivity is that the technology has low chance of damage during the whole life cycle of the equipment; the high sensitivity is that the technical process is likely to be damaged in the whole life cycle of the equipment; the extremely high sensitivity is that the technical process is very likely to be damaged during the whole life cycle of the equipment.
Further, the enemy prevention discovery design in the step 4) refers to various design measures such as recessive technologies, electronic interference and camouflage technologies and the like adopted by equipment; for example, missile combat equipment has the capability of preventing multi-spectral-band reconnaissance of visible light, infrared, radar, hyperspectral and the like, reduces the height and the front profile, improves the maneuverability, and ensures that the reconnaissance and identification of enemies can be avoided under the traveling and field standby states.
The damage prevention design is to control or reduce the damage probability and damage harmfulness of equipment by adopting a design technology or utilizing certain equipment; the method mainly comprises the following steps: a) conventional protection and nuclear, biochemical protection; b) functions are dispersed, and equipment positions are reasonably distributed; c) designing redundancy; d) designing a safety coefficient; e) active and passive lesion suppression techniques.
The technical process optimization refers to improving and adjusting the technical process for reducing the damage of the equipment caused by the technical process; for example, for a metal base plate which is easy to be damaged by corrosion, a coating film or material design process is improved;
the damage repair guarantee refers to a damage repair technology adopted for restoring the equipment to the necessary service performance in the task execution process and maintainability, testability and supportability design measures adopted for improving the equipment damage restoration capacity; such as electroless welding, structural patch repair, interchangeability, modular design.
Further, the damage maintenance support work items in the step 5) include a damage maintenance item name, a damage detection method, a damage maintenance mode, an emergency maintenance method, and a maintenance support resource requirement.
Wherein the emergency maintenance method comprises simplified repair, substitution, reconstruction, bypass, switching, temporary distribution and the like.
The invention has the following beneficial effects:
(1) the invention constructs a DMEA method which comprehensively considers the battle threats, special events and technical processes, and makes up the limitation and one-sidedness that the current DMEA method only considers the battle damages;
(2) the method takes damage mode analysis as target guidance, breaks through and optimizes the flow thought of analyzing the damage mechanism after combing the damage mode at present, firstly proposes that various damage mechanisms are superposed on each task stage and working mode of the equipment using process on the basis of comprehensively analyzing the damage mechanism, and the system analyzes various damage modes of the equipment, has clear thought, clear target and reasonable flow;
(3) the first system of the invention combs three damage mechanisms of battle threats, special events and technical processes, the reason types and related factor examples, gives comprehensive typical task stages and working modes, typical damage modes, damage detection methods, maintenance modes and emergency maintenance methods, and provides technical support and normative guidance for comprehensive and deep development of analysis work;
(4) the invention firstly provides a concept of potential damage risk of the technical process, firstly considers the influence of the technical process in equipment damage mode analysis, and constructs a method system for evaluating maturity of the technical process, evaluating potential damage sensitivity of the technical process and evaluating the potential damage risk level of the technical process;
(5) the invention breaks through the main purpose of the current DMEA that war damage maintenance work project analysis is taken as the main purpose, the system provides four aspects of design improvement measures such as enemy discovery design, damage prevention design, technical process optimization, damage maintenance guarantee design and the like, and provides all-round technical support for high survivability, high reliability, high task safety and success and high first-aid repair performance of equipment;
(6) the method of the invention is an extended induction analysis on the basis of fully utilizing the traditional DMEA analysis result, and has strong operability and higher engineering application value.
Drawings
The following describes embodiments of the present invention in further detail with reference to the accompanying drawings.
FIG. 1 shows a flow chart of a method of damage pattern and impact analysis of missile weaponry of the present invention.
FIG. 2 shows a flow diagram of an integrated DMEA implementation of the present invention.
Detailed Description
In order to more clearly illustrate the invention, the invention is further described below with reference to preferred embodiments and the accompanying drawings. Similar parts in the figures are denoted by the same reference numerals. It is to be understood by persons skilled in the art that the following detailed description is illustrative and not restrictive, and is not to be taken as limiting the scope of the invention.
The invention relates to a damage mode and influence analysis method of missile weapon equipment considering battle threats, special events and technical processes, which is mainly designed according to equipment survivability, reliability and task safety and quick repair work analysis requirements and is based on a traditional DMEA analysis method, the connotation of DMEA is expanded, and a comprehensive DMEA analysis method is built, namely, on the basis of the traditional DMEA analysis, damage mechanisms are analyzed from three aspects of battle threats, special events and technical processes, and various damage mechanisms are applied to each task stage and working mode of the equipment, so that all possible damage modes are comprehensively identified; meanwhile, associating the technical process adopted by the equipment with a damage mode, analyzing the maturity of the technical process and the sensitivity of the technical process to potential damage, and determining the damage risk level of the technical process; on the basis of damage mechanism and technical process analysis, design improvement measures for clearly avoiding or eliminating damage modes are taken from four aspects of enemy discovery design, damage prevention design, technical process optimization and damage maintenance guarantee design, damage maintenance guarantee work items are determined, a table shown in a table 1 is finally obtained, and an implementation flow is shown in a figure 2.
TABLE 1 comprehensive DMEA analysis Table
Figure BDA0001561402180000051
Specifically, a missile weapon equipment damage mode and influence analysis method considering battle threats, special events and technical processes, as shown in fig. 1, includes the following steps:
first step analysis of Damage mechanism
The damage mechanism refers to all possible conditions or condition combinations such as enemy attack which may cause equipment damage, behavior factors such as attack enemy or combat environment, special events, and technical processes adopted by equipment in the processes of combat, training, maintenance, use guarantee and the like.
According to the equipment life profile, the mission profile and the environment profile, the damage mechanism analysis is carried out from three aspects of combat threats, special events and technical processes, and the damage mechanism types and relevant factors are shown in a table 2:
(1) a combat threat refers to all possible causes or factors of equipment damage in a battlefield environment due to an enemy attack, attacking an enemy or the combat environment.
(2) Special event classes refer to abnormal use actions or unexpected conditions that lead to unexpected damage to equipment during the life cycle.
(3) The technology process class refers to technologies and process conditions that are sensitive to potential damage employed in the design and manufacture of equipment.
TABLE 2 Damage mechanism
Figure BDA0001561402180000061
Figure BDA0001561402180000071
Second step determination of injury patterns
All task stages and working modes of the equipment are analyzed according to the service life section and the task section, and typical task stages and working modes of the missile weapon equipment are shown in a table 3.
On the basis of comprehensively decomposing and identifying the task stage and the working mode of the equipment, various damage mechanisms are superposed on each task stage and working mode in the using process of the equipment, and all possible damage modes of the equipment caused by the action process of the fighting threat, the special event and the specific mechanism of the technical process in each task stage and each working mode are analyzed and identified one by one; typical injury patterns are shown in table 4.
Analysis to determine damage patterns should be done with care to distinguish them from failure modes, which are typically intrinsic failures caused by the failure mechanism of the product itself or the system, whereas damage patterns are often extrinsic failure modes due to battlefield conditions, abnormal use, abnormal conditions. Since the fuel tank rarely malfunctions during the normal life cycle of the missile launcher, the failure mode of the fuel tank is not important for analysis in failure mode influence and hazard analysis (FMEA), but when the fuel tank is subjected to damage mode analysis, the fuel tank is exposed to a large area and accumulated energy, and is likely to be severely damaged by various attacks, and thus the damage mode is to be analyzed.
TABLE 3 typical task phases and modes of operation
Figure BDA0001561402180000072
Figure BDA0001561402180000081
Table 4 exemplary injury modes
Figure BDA0001561402180000082
Third step of evaluating the technical process and the potential damage risk level thereof
Because the technical process has certain sensitivity to damage, analyzing the technical processes adopted by each subsystem or equipment of the equipment, associating the technical processes adopted by the equipment with a damage mode, analyzing and evaluating the risk of the equipment due to the potential damage of the technical process in a correlation manner from two aspects of the maturity of the technical process and the potential damage sensitivity of the technical process, and evaluating the potential damage risk level of the technical process; the following is mainly considered:
(1) is the technical process mature, is a new technology and a new process?
(2) Is the technical process susceptible to certain damage or has been shown to cause damage by application?
The technical process adopted by each subsystem or equipment is characterized by the maturity of the technical process, and is qualitatively described by applying a table 5, and the accuracy of the grade can be adjusted by combining the characteristics of the equipment.
TABLE 5 technical Process maturity rating
Figure BDA0001561402180000091
And analyzing and evaluating the sensitivity of the adopted technical process to the potential damage mode by combining the identified possible damage mode, and qualitatively describing the potential damage sensitivity level of the potential damage mode by applying the table 6, wherein the accuracy of the level can be adjusted by combining the equipment characteristics.
TABLE 6 susceptibility rating of potential lesions
Grade Sensitivity of the device Description of the invention
1 Is extremely low The technology has extremely low damage chance in the whole life cycle of the equipment
2 Is low The technology has lower damage chance in the whole life cycle of the equipment
3 Moderate in quality The technology has low damage chance in the whole life cycle of the equipment
4 High is The technical process is likely to be damaged in the whole life cycle of the equipment
5 Extremely high The technical process is highly likely to be damaged in the whole life cycle of the equipment
And performing correlation analysis on the maturity grade and the damage sensitivity grade of the technical process, defining the damage risk grade of the technical process, and determining a risk threshold value by combining with the actual requirement of equipment to perform further damage analysis as shown in table 7.
TABLE 7 risk rating of potential damage to technical process
Figure BDA0001561402180000092
Figure BDA0001561402180000101
Fourth step of design improvement
Aiming at various analyzed damage modes, a damage mechanism and technical process analysis are combined, and design improvement measures for eliminating the damage modes and maintainability, testability and supportability design measures for improving equipment damage recovery capability are researched and determined from four aspects of enemy discovery design, damage prevention design, technical process optimization and damage maintenance support design.
(1) The design for finding the enemy prevention refers to various design measures such as recessive technologies, electronic interference and camouflage technologies and the like adopted by equipment. If the missile combat equipment has the capability of preventing the reconnaissance of visible light, infrared, radar, hyperspectral and other multi-spectral bands, the height is reduced, the front profile is reduced, the maneuverability is improved, and the reconnaissance and identification of enemies can be avoided under the traveling and field standby states.
(2) The damage prevention design means that the damage probability and damage harmfulness of equipment are controlled or reduced by adopting a design technology or utilizing certain equipment. The anti-damage design measures often taken are: conventional protection and nuclear, biochemical protection; functions are dispersed, and equipment positions are reasonably distributed; designing redundancy; designing a safety coefficient; active and passive damage suppression techniques.
(3) The technical process optimization refers to the improvement and adjustment of the technical process for reducing the damage of the equipment caused by the technical process. For example, for a metal base plate which is easy to be damaged by corrosion, a coating film or a material design process is improved.
(4) The damage maintenance guarantee design refers to a damage repair technology adopted for restoring equipment to necessary service performance in the task execution process and maintainability, testability and supportability design measures adopted for improving the equipment damage restoration capacity. Such as electroless welding, structural patch repair, interchangeability, modular design.
Fifthly, determining damage maintenance guarantee work items
Analyzing and determining damage maintenance guarantee work items which are necessary to be adopted for repairing the corresponding damage mode according to the information of the damage mode, the task stage, the work mode, the damage mechanism, the damage risk and the like obtained by analysis, and further analyzing the requirements of related maintenance guarantee resources; the damage maintenance support work items mainly include the names of the damage maintenance items, the damage detection methods, the damage maintenance modes, the emergency maintenance methods, and the requirements of the maintenance support resources, as shown in table 8.
Table 8 Damage maintenance support work item table
Figure BDA0001561402180000102
(1) The name of the damage maintenance work project should include product or function mark information and a maintenance mode; such as delayed repair of radar array surface and replacement of aiming equipment.
(2) The damage detection method is used for analyzing the damage detection method aiming at each damage mode so as to provide a basis for the maintainability and testability design of the equipment and the damage maintenance work of the equipment; the damage detection method generally comprises: visual inspection, in situ testing, use inspection, decomposition review, and the like.
(3) The damage repair method should determine the repair measures to be taken to achieve the maximum availability of the damage repair resources during the mission, including: delayed repair, in-situ repair, replacement or replacement.
(4) An emergency maintenance method, which is a rapid emergency repair measure taken in a complex use environment to ensure that equipment can continuously execute a current task and recover the basic function of the equipment; a typical emergency repair method is shown in table 9.
(5) And the requirements on maintenance support resources are definitely met, and the requirements on related maintenance support resources such as manpower and personnel, spare parts and consumables, maintenance support equipment, technical data, computer software and hardware and the like required by each damaged maintenance work project are definitely met.
Table 9 example Emergency repair method
Figure BDA0001561402180000111
It should be understood that the above-mentioned embodiments of the present invention are only examples for clearly illustrating the present invention, and are not intended to limit the embodiments of the present invention, and it will be obvious to those skilled in the art that other variations or modifications may be made on the basis of the above description, and all embodiments may not be exhaustive, and all obvious variations or modifications belonging to the technical solutions of the present invention are within the scope of the present invention.

Claims (9)

1. A method for analyzing damage modes and influences of missile weaponry is characterized by comprising the following steps:
1) analyzing a damage mechanism: according to the equipment life profile, the mission profile and the environment profile, carrying out damage mechanism analysis from three aspects of battle threats, special events and technical processes;
2) determining a damage mode: decomposing and analyzing all task stages and working modes of the equipment according to the service life section and the task section of the equipment; on the basis of comprehensively decomposing and identifying task stages and working modes, various damage mechanisms are superposed on each task stage and working mode of the equipment using process, and all possible damage modes of the equipment caused by battle threats, special events and specific mechanism action processes of technical processes in each task stage and each working mode are analyzed and identified one by one;
3) evaluating the technical process and the potential damage risk level: analyzing the technical processes adopted by each subsystem or equipment of the equipment, associating the technical processes adopted by the equipment with a damage mode, analyzing and evaluating the risk of the equipment due to the potential damage of the technical process in a correlation manner from two aspects of the maturity of the technical process and the potential damage sensitivity of the technical process, and evaluating the potential damage risk level of the technical process;
4) designing improvement measures: aiming at various analyzed damage modes, by combining damage mechanism and technical process analysis, design improvement measures for avoiding or eliminating the damage modes and maintainability, testability and supportability design measures for improving equipment damage recovery capability are researched and determined from four aspects of enemy discovery design, damage prevention design, technical process optimization and damage maintenance support design;
5) determining damage maintenance guarantee work items: and analyzing and determining damage maintenance guarantee work items which are necessary to be adopted for repairing the corresponding damage mode according to the damage mode, the task stage and the working mode, the damage mechanism and the damage risk information obtained by analysis, and further analyzing the requirements of related maintenance guarantee resources.
2. The damage pattern and impact analysis method as claimed in claim 1, wherein the battle threat in step 1) is all possible causes or factors of equipment damage caused by enemy attack, attack enemy or battle environment behavior in battlefield environment;
the special event is an abnormal use action or unexpected condition that causes accidental damage to equipment during a life cycle;
the technical process is a potentially damage sensitive technique and process conditions employed in the design and manufacture of equipment.
3. The method for analyzing damage patterns and effects of claim 1, wherein the damage patterns in step 2) comprise perforation, deformation, separation, shattering, crack, fracture, rupture, fracture, seizing, dislocation, blockage, shedding, fire, explosion, burnout, fragment impact, nuclear contamination, biochemical contamination, gas leakage, water leakage, oil leakage, tire burst, moisture exposure, corrosion, delamination, open circuit, short circuit, ionization, burnthrough, blindness, stall, system collapse, crash, runaway, power outage, localized high temperature, condensation, accidental ignition, and breakage.
4. The method of claim 1, wherein the mission phase comprises technical preparation, marching maneuver, deployment, retraction, launch preparation, launch, active flight, passive flight, transportation, handling, transshipment, storage, training, maintenance;
the working modes comprise full load, partial load, continuous work, discontinuous work, remote operation, in-situ operation, parallel work, serial work, degraded use and normal use.
5. The method for analyzing damage patterns and influences as claimed in claim 1, wherein the maturity of the technical process in step 3) is divided into mature technical process, more mature technical process and novel technical process.
6. The method for analyzing damage patterns and influences as claimed in claim 1, wherein the sensitivity of potential damage of the process technology in step 3) is classified into an extremely low sensitivity, a medium sensitivity, a high sensitivity, and an extremely high sensitivity.
7. The damage pattern and influence analysis method according to claim 1, wherein the enemy discovery design in step 4) refers to various design measures such as recessive technologies, electronic interference and camouflage technologies and the like adopted by equipment;
the damage prevention design is to control or reduce the damage probability and damage harmfulness of equipment by adopting a design technology or utilizing certain equipment;
the technical process optimization refers to improving and adjusting the technical process for reducing the damage of the equipment caused by the technical process;
the damage repair guarantee refers to a damage repair technology adopted for restoring the equipment to the necessary service performance in the task execution process and maintainability, testability and supportability design measures adopted for improving the damage restoration capacity of the equipment.
8. The damage model and impact analysis method of claim 1, wherein the damage maintenance support work items in step 5) include a damage maintenance item name, a damage detection method, a damage maintenance mode, an emergency maintenance method, and a maintenance support resource requirement.
9. The method of claim 8, wherein the emergency repair method comprises repair simplification, substitution, reconstruction, bypass, switching, and temporary use.
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