CN110027729A - A kind of Unmanned Aerial Vehicle Powerplants system rapid detection method - Google Patents
A kind of Unmanned Aerial Vehicle Powerplants system rapid detection method Download PDFInfo
- Publication number
- CN110027729A CN110027729A CN201910386055.3A CN201910386055A CN110027729A CN 110027729 A CN110027729 A CN 110027729A CN 201910386055 A CN201910386055 A CN 201910386055A CN 110027729 A CN110027729 A CN 110027729A
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- CN
- China
- Prior art keywords
- power plant
- ground
- aerial vehicle
- plant system
- unmanned aerial
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- 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.)
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/40—Maintaining or repairing aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/60—Testing or inspecting aircraft components or systems
Abstract
The invention discloses a kind of Unmanned Aerial Vehicle Powerplants system rapid detection methods to be arranged opposite opened quick-release power hatch cover using fluorescence antirust paint label is smeared at power plant system installation interface and pipeline interface；By visual observation or white light flashlight tool finds the installation question in use；If label is damaged, further opens quick-release type power hatch cover and confirmed and overhauled, or check comprehensively, safeguard below deck equipment and engine.Power plant system installation check in place after, using ground checkout equipment, state of ground detection, job control and malfunction elimination are carried out to power plant system.The efficiency for improving power plant system ground safeguard, reduces the scale of system maintenance, while reducing work difficulty and intensity, increases the flexibility of detection, improves detection efficiency.By simple operations, realize that Unmanned Aerial Vehicle Powerplants system ground is quick, check comprehensively and test, the quick engineering guarantee of realization unmanned plane ensure that unmanned plane is reliably let fly away.
Description
Technical field
The present invention relates to Unmanned Aerial Vehicle Powerplants surface detection techniques, specifically, being related to a kind of Unmanned Aerial Vehicle Powerplants
System rapid detection method.
Background technique
The ground check of Unmanned Aerial Vehicle Powerplants system and test are the important composition portions of unmanned aerial vehicle engineering safeguard work
Point, it is the important means for guaranteeing engine reliable work, unmanned plane and reliably letting fly away.
The engineering guarantee of Unmanned Aerial Vehicle Powerplants system ground is divided into inspection and functional test two parts.At present due to unmanned plane
Scale is smaller, and the design of power plant system is by simply gradually developing to complexity, after the installation of Unmanned Aerial Vehicle Powerplants system
Ground check and test and not formed system, specification, simple, effective planning and method.Before unmanned vehicle engine is driven, one
As using visual inspection and carried out by the way of ground control station joint test, if unmanned plane is smaller or is architectural limitation, piggyback pod
It is not in place to safeguard that lid opens up, is difficult to carry out comprehensive visual inspection of dynamical system equipment, using tool inspection and repair more
Difficulty, largely need disassembly power hatch cover, heavy workload, for medium-sized, large-scale unmanned plane will also by ancillary equipment and specially
With tool, time-consuming for engineering preparation；If the non-connection of Unmanned Aerial Vehicle Data Link, it is not available ground control station detection power plant system
The integrity of electrical equipment and system function.
With constantly widening for unmanned plane application field, user to unmanned plane emergency response, quick engineering prepares, checks,
Let that more stringent requirements are proposed fly away, accessibility, the convenience for reinforcing power plant system Inspection and maintenance are imperative.
Summary of the invention
In order to avoid the shortcomings of the prior art, the present invention proposes a kind of Unmanned Aerial Vehicle Powerplants system quickly side of detection
Method, the detection method can realize that Unmanned Aerial Vehicle Powerplants system ground checks and tests quickly, comprehensively, reach the quick machine of unmanned plane
The requirement that business is ensured, let fly away in time.
The technical solution adopted by the present invention to solve the technical problems is: a kind of Unmanned Aerial Vehicle Powerplants system quickly detects
Method, it is characterised in that the following steps are included:
Step 1. determines installation interface japanning label；Interface, clip, electricity are installed in piggyback pod intrinsic motivation, equipment, pipeline
Cable interface applies fluorescent paint label；By engine inlet and outlet channel, safeguard that lid carries out visually relevant position, or use
White light flashlight is checked that discovery paint mark is abnormal or need to further check, safeguards or repair, and is opened the cabin；
Step 2. opens the inspection of opposite opened quick-release power hatch cover, maintenance and maintenance；Press power hatch cover top quick-detachable lock, cabin
Cover separately falls from top, if discovery paint mark is impaired, tool need to be used to be confirmed and overhauled, or checks comprehensively, in maintenance cabin
Equipment and engine；
Step 3. is connected to power plant system ground function detection equipment, carries out Function detection；Power plant system installation
After checking in place, in unmanned aerial vehicle test interface connecting power device ground checkout equipment, pass through detection device human-computer interaction
Interface carries out the detection of the power plant system state of ground, job control and malfunction elimination；
Step 4. testing result uploads UAV system；Using ground function detection equipment, complete to power plant system
Monitoring, record and inquiry are implemented in work, are finally completed power plant system installation functional test.
Beneficial effect
A kind of Unmanned Aerial Vehicle Powerplants system rapid detection method proposed by the present invention, be it is a kind of quickly, effectively, check with
Test the Unmanned Aerial Vehicle Powerplants system detecting method combined.It is smeared at power plant system all devices and pipeline interface
Fluorescence antirust paint label, by visual observation or the installation question in the simple tools discovery use such as white light flashlight；Solving need to open up
Larger maintenance lid reserves the problem of enough working spaces are contradicted with aeroplane structure design to tool, effectively reduces inspection
Difficulty and intensity reduce using probability, shortening the review time, improve inspection efficiency for tool.
Unmanned Aerial Vehicle Powerplants system rapid detection method of the present invention and General Maintenance lid are visually assisted with specific purpose tool
Inspection, ground control station total system power-on test are compared, and are improved the efficiency of power plant system ground safeguard, are reduced system
The scale of maintenance, while work difficulty and intensity are reduced, it increases the flexibility of detection, improve detection efficiency.
Unmanned Aerial Vehicle Powerplants system rapid detection method of the present invention realizes Unmanned Aerial Vehicle Powerplants by simple operations
System ground checks quickly, comprehensively and test, and the review time shortens at least 30min than conventional method；Realize the quick machine of unmanned plane
Business ensures, ensures that unmanned plane is reliably let fly away.
Detailed description of the invention
With reference to the accompanying drawing with embodiment to a kind of Unmanned Aerial Vehicle Powerplants system rapid detection method of the present invention make into
One step is described in detail.
Fig. 1 is Unmanned Aerial Vehicle Powerplants system rapid detection method flow chart of the present invention.
Fig. 2 is that quick-release opposite opened power hatch cover of the invention opens schematic diagram.
Fig. 3 ground checkout equipment work-based logic block diagram.
In figure:
1. undercarriage or 2. power hatch cover open position of sled position, 3. power-equipment pipeline install 4. engine of profile
5. quick-release lock position of profile, 6. engine hatch cover closed position and firewall reinforce 7. hatch cover mooring line of edge profile, 8. power
9. hinge position of distance between hatch cover and ground
Specific embodiment
The present embodiment is a kind of Unmanned Aerial Vehicle Powerplants system rapid detection method.
Refering to fig. 1, Fig. 2, Fig. 3, the present embodiment Unmanned Aerial Vehicle Powerplants system rapid detection method using Mr. Yu's type nobody
The overall process that the engineering guarantee of power plants system ground and ground handling equipment quickly detect.
The first step determines installation interface japanning label；The installation interface of piggyback pod intrinsic motivation components, equipment,
Pipeline installs interface, and fluorescent paint label is applied at clip, cable interface；If relevant interface rises because of transport, engine operating, unmanned plane
Fly, landing shocks or big overload reason occur to loosen or displacement, label paint will damaged or fracture, check whether interface is deposited at this time
It is loosening or is leaking, if without exception, can let fly away again after mark locking and coating label paint.Piggyback pod maintenance lid compared with
Small, tool, which checks, to be used in the case of limited space or Maintenance free lid, visually or white light flashlight is examined through piggyback pod open channel
It looks into, can find the problem, simplify operation, shorten the review time.
Second step opens the inspection of opposite opened quick-release power hatch cover, maintenance and maintenance；Power hatch cover top quick-detachable lock is pressed,
Hatch cover separately falls from top, if discovery paint mark is impaired, tool need to be used to be confirmed and overhauled, or checks comprehensively, maintenance cabin
Interior equipment and engine；The connection of power hatch cover underneath hinges, will not wipe ground after opening hatch cover using hatch cover mooring line.Open type
It designs, tool use space is unrestricted in cabin, and detachable maintaining is convenient and efficient.Power plant system static check operation, checks
Time is short.
Third step, connection power plant system ground function detection equipment, carry out Function detection；Power plant system installation
After checking in place, in unmanned aerial vehicle test interface connecting power device ground checkout equipment, pass through detection device human-computer interaction
Interface carries out the detection of the power plant system state of ground, job control and malfunction elimination.Join without ground control station and data-link
It drives and detects with power plant system independence static debugging, test and engine dynamic can be completed, and to power device system
Monitoring, record and inquiry are implemented in the work of system, are finally completed power plant system installation functional test.
4th step, testing result upload UAV system；It is achievable to power device system using ground function detection equipment
Monitoring, record and inquiry are implemented in work of uniting, and are finally completed power plant system installation functional test.Power plant system installation inspection
After finding position, after the power-up of Unmanned Aerial Vehicle Powerplants system, using ground function detection equipment, power plant system can be effectively detected
Can whether communication, instruction works, data acquisition and the functions such as alarm, power distribution, cable connection be normal, it is winged to meet unmanned plane
Row requires；Can inquire simultaneously with download system relevant information, provided a strong guarantee with engine periodic maintenance for system troubleshooting.
Claims (1)
1. a kind of Unmanned Aerial Vehicle Powerplants system rapid detection method, it is characterised in that the following steps are included:
Step 1. determines installation interface japanning label；Interface is installed in piggyback pod intrinsic motivation, equipment, pipeline, clip, cable connect
Fluorescent paint label is applied at mouthful；By engine import/exhaust channel, safeguard that lid carries out visually relevant position, or use white light
Flashlight is checked that discovery paints mark exception or further checks, safeguards or maintenance, is opened the cabin；
Step 2. opens the inspection of opposite opened quick-release power hatch cover, maintenance and maintenance；Press power hatch cover top quick-detachable lock, hatch cover from
Top separately falls, if discovery paint mark is impaired, tool need to be used to be confirmed and overhauled, or checks comprehensively, maintenance below deck equipment
With engine；
Step 3. is connected to power plant system ground function detection equipment, carries out Function detection；Power plant system installation check
After in place, in unmanned aerial vehicle test interface connecting power device ground checkout equipment, pass through detection device human-computer interaction interface
Carry out the detection of the power plant system state of ground, job control and malfunction elimination；
Step 4. testing result uploads UAV system；Using ground function detection equipment, complete to work to power plant system
Implement monitoring, record and inquiry, is finally completed power plant system installation functional test.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910386055.3A CN110027729A (en) | 2019-05-09 | 2019-05-09 | A kind of Unmanned Aerial Vehicle Powerplants system rapid detection method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910386055.3A CN110027729A (en) | 2019-05-09 | 2019-05-09 | A kind of Unmanned Aerial Vehicle Powerplants system rapid detection method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110027729A true CN110027729A (en) | 2019-07-19 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
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| CN201910386055.3A Pending CN110027729A (en) | 2019-05-09 | 2019-05-09 | A kind of Unmanned Aerial Vehicle Powerplants system rapid detection method |
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Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104097781A (en) * | 2013-04-03 | 2014-10-15 | 波音公司 | Aircraft nacelle assembly |
| CN104803009A (en) * | 2015-04-27 | 2015-07-29 | 中国航空工业集团公司沈阳飞机设计研究所 | Unmanned aerial vehicle (UAV) ground comprehensive detection system and UAV ground comprehensive detection method |
| CN105873825A (en) * | 2013-10-24 | 2016-08-17 | 空客集团有限公司 | Collaborative robot for visually inspecting an aircraft |
-
2019
- 2019-05-09 CN CN201910386055.3A patent/CN110027729A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104097781A (en) * | 2013-04-03 | 2014-10-15 | 波音公司 | Aircraft nacelle assembly |
| CN105873825A (en) * | 2013-10-24 | 2016-08-17 | 空客集团有限公司 | Collaborative robot for visually inspecting an aircraft |
| CN104803009A (en) * | 2015-04-27 | 2015-07-29 | 中国航空工业集团公司沈阳飞机设计研究所 | Unmanned aerial vehicle (UAV) ground comprehensive detection system and UAV ground comprehensive detection method |
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20190719 |
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| RJ01 | Rejection of invention patent application after publication |