CN105883000A - Captive carrying test device - Google Patents
Captive carrying test device Download PDFInfo
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- CN105883000A CN105883000A CN201610348743.7A CN201610348743A CN105883000A CN 105883000 A CN105883000 A CN 105883000A CN 201610348743 A CN201610348743 A CN 201610348743A CN 105883000 A CN105883000 A CN 105883000A
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Abstract
The invention provides a captive carrying test device. The captive carrying test device comprises an in-cabin part and an out-cabin part, wherein the in-cabin part comprises a transition plate, a plurality of support columns, a battery and a signal recorder; the out-cabin part comprises a hanging rack, a left support, a right support, a shaft, a left lateral plate, a right lateral plate, a slider and a fixing plate; the transition plate is mounted at the observation window position on an aircraft base plate, the support columns are vertically fixed below the transition plate, the signal recorder is fixed on the transition plate, and the battery is fixedly clamped to the transition plate through a fixing clamp. The captive carrying test device has the advantages that the captive carrying test requirements of a product can be satisfied, the product and the test device can be mounted on an aircraft at the same time, flight test stability is guaranteed, flight over an appointed test site according to required speed and flight trajectory can be achieved through an aircraft carrying test device, the motion conditions of a product in a real environment are simulated, the index and performance features of the product during the flight are verified, and the product can be examined comprehensively.
Description
Technical field
The present invention relates to a kind of extension and fly assay device.
Background technology
In the field such as aircraft, unmanned plane, most products will carry out field trial, with checking
Product index under true environment and Performance Characteristics.The method of field trial at present mainly has examination
Test an actual experimental and sled test, but test site actual experimental somewhat expensive, and many times
Not reproducible, and be also impossible to implement in the development stage, and sled test is due to test site
Condition limits, and landform is single, and index and Performance Characteristics examination to product be not comprehensive, Zhi Nengzuo
For a kind of initial test of knowing the real situation.
Summary of the invention
For solving above-mentioned technical problem, the invention provides a kind of extension and fly assay device, this extension flies
Assay device passes through
The present invention is achieved by the following technical programs.
A kind of extension that the present invention provides flies assay device, including part in cabin and part out of my cabin；Institute
State internal point of cabin and include rebound, pillar, battery, signal recorder；Described cabin outer part
Include hanger, left socle, right support, axle, left plate, right plate, slide block, fixed disk；Institute
Stating rebound and be arranged on observation window position on aircraft cabin inner bottom plating, a plurality of pillar is vertically fixed on
Below rebound, rebound is fixed with on signal recorder, and rebound and is pressed from both sides by fixation clamp
Fasten battery；Described lower rod end fixes the hanger of level, bottom the opposite end of hanger
Fix left socle and right support, left socle and right support inner face respectively and be fixed with a left side by axle respectively
Side plate and right plate, right plate is provided with the chute of strip, and slide block is slidably mounted on cunning
In groove, product to be tested is fixed by fixed disk in its center position；Described fixed disk center
Position is provided with cable-through hole, and described signal recorder, battery connect product by cable-through hole cable,
Between battery and signal recorder, also cable connects.
Described left plate and right plate top are arc-shaped, have eyelid covering from left plate and right plate
Space between left plate and right plate is wrapped up in the way of Open Side Down by side, top, covers
Intradermal face is fixed with absorbing material, and product is fully wrapped around.
Being additionally provided with antenna on described product, antenna is integrated is arranged on product lower end.
Described cable connects, and uses low-frequency cable.
It is additionally provided with on the fixing rebound of display lamp and switch, display lamp and switch, and with circuit
The mode of series connection controls and indicates power supply and the power-off of product.
The beneficial effects of the present invention is: the extension that can meet product flies test requirements document, it is possible to will produce
Product and test device are mounted simultaneously on aircraft, it is ensured that the stability during flight test, energy
Assay device speed on request and flight path is carried in the test site specified by aircraft
Flying overhead, analog equipment motion conditions in true environment, checking product is at flight course
In index and Performance Characteristics, product is comprehensively examined, therefore have high reliability,
Good repeatability, operability, and experimentation cost is the highest, effective.
Accompanying drawing explanation
Fig. 1 is the schematic top plan view of the present invention；
Fig. 2 is the A-A face sectional view of Fig. 1；
Fig. 3 is the side view that Fig. 1 is perpendicular to A-A face.
In figure: 1-rebound, 2-pillar, 3-hanger, 4-left socle, 5-right support, 6-eyelid covering,
7-axle, 8-left plate, 9-right plate, 10-slide block, 11-fixed disk, 12-chute, 13-product,
14-antenna, 15-absorbing material, 16-mounting groove, 17-cable-through hole, 18-fixation clamp, 19-battery,
20-signal recorder, 21-display lamp, 22-switchs.
Detailed description of the invention
Technical scheme is described further below, but claimed scope is not limited to
In described.
Present invention essentially provides a kind of extension as shown in Figure 1 to Figure 3 and fly assay device, including
Part, out of my cabin part in cabin, internal point of its middle deck is arranged on observation window on aircraft cabin inner bottom plating
Position, is partially installed under aircraft ventral out of my cabin, device and out of my cabin in low-frequency cable connecting cabin
Device, the transmission of signal, electric current when flight test.
Internal point of described cabin includes rebound 1, pillar 2, signal recorder 20, battery 19, opens
Close 22, display lamp 21 and fixation clamp 18.
Described it is partially installed on out of my cabin under aircraft ventral, including hanger 3, left socle 4, right support
5, left plate 8, right plate 9, axle 7, eyelid covering 6, absorbing material 15, product 13, antenna 14,
Fixed disk 11 and slide block 10.
Described pillar 2, signal recorder 20, battery 19, switch 22, display lamp 21 and fixing
Folder 18 is arranged on rebound 1.
Described battery 19, switch 22, display lamp 21 are used for the power supply to product 13 and power-off.
Described signal recorder 20 is used for the record in flight test to product 13 signal, in real time
Ground characterizes the product (working condition of 13 in flight course.
Battery 19 is firmly fixed on rebound 1 by described fixation clamp 18.
Described pillar 2 is through the observation window bottom aircraft, for the outer device of connecting cabin.
Described eyelid covering 6 is fixed on left plate 8, right plate 9 composition gondola, is used for installing product
13 and absorbing material 15, for semicircular arc, it is open type towards one end, ground.
Described axle 7 is two, is separately mounted on left plate 8, right plate 9；Described left socle 4,
Right support 5 is set on two axles 7, and fastens with nut.Hanger 3 one end connects a left side
Frame 4, right support 5, the other end is connected with device in cabin by pillar 2.
Described product 13 is arranged on fixed disk 11, and can be by slide block 10 along on right plate 9
Chute 12 move up and down regulation product 13 position.Antenna 14 is placed in product 13 lower end, with
Product 13 becomes one.
Following steps can be taked when the present invention uses:
1. by being partially installed on observation window position on aircraft cabin inner bottom plating in cabin, then by cabin
Outer portion is arranged under aircraft ventral, is connected fastening by pillar 2 with device in cabin；
2. the test job before utilizing test equipment to test product, before record product test
Parameters, product qualified for performance indications is loaded in the fixed disk 11 in part out of my cabin；
3. by part in low-frequency cable connection product and cabin, and debug, in record debugging
Signal also carries out data readback, confirms that each equipment is working properly；
4. aircraft carries assay device speed on request and flight path at the test site specified
Ground flying overhead, analog equipment motion conditions in true environment, checking product was flying
Index in journey and Performance Characteristics；
Before entering test place the most each time, switch 22 is pulled " on " position, and to flight
Landform image immediately below track is carried out taking photo by plane record, will switch when exiting examination place each time
22 pull " off " position；
6., after completing a predetermined number of tasks of sortie, aircraft landing comes to a complete stop, to signal record
The product output signal of instrument record is analyzed, and confirms the effectiveness of data, extracts spy therein
The amount of levying, according to the duty of the time history analysis product of each signal, is carried out result of the test
Statistical analysis, determines indices and the Performance Characteristics of product.
Thus, the present invention can meet the extension of product and flies test requirements document, it is possible to by product and test dress
Put and be mounted simultaneously on aircraft, it is ensured that the stability during flight test, can be taken by aircraft
Girdle tests device speed on request and flight path are at the test site flying overhead specified, mould
Intend product motion conditions in true environment, verify product index in flight course and property
Energy characteristic, comprehensively examines product.Therefore, the present invention has high reliability, good
Repeatability well, operability, and experimentation cost is the highest, effective.
Claims (5)
1. extension flies an assay device, including part in cabin and part out of my cabin, it is characterised in that:
Internal point of described cabin includes rebound (1), pillar (2), battery (19), signal recorder
(20)；Described part out of my cabin includes hanger (3), left socle (4), right support (5), axle
(7), left plate (8), right plate (9), slide block (10), fixed disk (11)；Described mistake
Cab apron (1) is arranged on observation window position on aircraft cabin inner bottom plating, and a plurality of pillar (2) is vertical
It is fixed on rebound (1) lower section, rebound (1) is fixed with signal recorder (20),
And be fixedly clamped battery (19) by fixation clamp (18) on rebound (1)；Described pillar
(2) hanger (3) of level is fixed in lower end, fixes respectively bottom the opposite end of hanger (3)
Left socle (4) and right support (5), left socle (4) and right support (5) inner face lead to respectively
Crossing axle (7) and be fixed with left plate (8) and right plate (9), right plate is provided with on (9)
The chute (12) of strip, slide block (10) is slidably mounted in chute (12), slide block
(10) center is by the fixing product (13) to be tested of fixed disk (11)；Described solid
Price fixing (11) center is provided with cable-through hole (17), described signal recorder (20), electricity
Pond (19) connects product (13), battery (19) and signal by cable-through hole (17) cable
Between monitor (20), also cable connects.
2. as claimed in claim 1 extension flies assay device, it is characterised in that: described left plate
(8) and right plate (9) top is arc-shaped, there is eyelid covering (6) from left plate (8) and the right side
The side of side plate (9), top by the space between left plate (8) and right plate (9) with
The mode that Open Side Down is wrapped up, and eyelid covering (6) inner face is fixed with absorbing material (15) by product
(13) fully wrapped around.
3. as claimed in claim 1 extension flies assay device, it is characterised in that: described product (13)
On be additionally provided with antenna (14), antenna (14) integrated installation is in product (13) lower end.
4. as claimed in claim 1 extension flies assay device, it is characterised in that: described cable is even
Connect, use low-frequency cable.
5. as claimed in claim 1 extension flies assay device, it is characterised in that: it is additionally provided with finger
Show the fixing rebound (1) of lamp (21) and switch (22), display lamp (21) and switch (22)
On, and in the way of circuit connected in series, control and indicate power supply and the power-off of product (13).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610348743.7A CN105883000A (en) | 2016-05-24 | 2016-05-24 | Captive carrying test device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610348743.7A CN105883000A (en) | 2016-05-24 | 2016-05-24 | Captive carrying test device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105883000A true CN105883000A (en) | 2016-08-24 |
Family
ID=56717191
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610348743.7A Pending CN105883000A (en) | 2016-05-24 | 2016-05-24 | Captive carrying test device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105883000A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106564817A (en) * | 2016-08-31 | 2017-04-19 | 贵州航天电子科技有限公司 | Aircraft test platform cableway stepless lifting device |
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|---|---|---|---|---|
| US20030071165A1 (en) * | 2001-03-05 | 2003-04-17 | Fiebick Wayne A. | Integral data acquisition capacity |
| CN201240505Y (en) * | 2008-07-22 | 2009-05-20 | 山西亚太数字遥感新技术有限公司 | Apparatus for hitching airborne laser LIDAR apparatus with helicopter |
| CN202797773U (en) * | 2012-09-29 | 2013-03-13 | 江苏省电力公司徐州供电公司 | Auxiliary hanging device of electric power inspection air vehicle |
| CN202783800U (en) * | 2012-09-11 | 2013-03-13 | 江西洪都航空工业集团有限责任公司 | Captive flight verification test support with double guide heads |
| CN203521593U (en) * | 2013-09-24 | 2014-04-02 | 上海无线电设备研究所 | Dual-antenna interference airborne captive flight structure |
| CN204574971U (en) * | 2015-04-23 | 2015-08-19 | 贵州航天电子科技有限公司 | A kind of suction wave apparatus of electronic fuse |
| KR20150104842A (en) * | 2014-03-06 | 2015-09-16 | 국방과학연구소 | Appatatus for aircraft captive flight test for guided anti-tank missile |
| CN105521836A (en) * | 2016-02-04 | 2016-04-27 | 广州苏试众博环境实验室有限公司 | Low-air-pressure testing system |
| CN205633097U (en) * | 2016-05-24 | 2016-10-12 | 贵州航天电子科技有限公司 | Hang and fly test device |
-
2016
- 2016-05-24 CN CN201610348743.7A patent/CN105883000A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20030071165A1 (en) * | 2001-03-05 | 2003-04-17 | Fiebick Wayne A. | Integral data acquisition capacity |
| CN201240505Y (en) * | 2008-07-22 | 2009-05-20 | 山西亚太数字遥感新技术有限公司 | Apparatus for hitching airborne laser LIDAR apparatus with helicopter |
| CN202783800U (en) * | 2012-09-11 | 2013-03-13 | 江西洪都航空工业集团有限责任公司 | Captive flight verification test support with double guide heads |
| CN202797773U (en) * | 2012-09-29 | 2013-03-13 | 江苏省电力公司徐州供电公司 | Auxiliary hanging device of electric power inspection air vehicle |
| CN203521593U (en) * | 2013-09-24 | 2014-04-02 | 上海无线电设备研究所 | Dual-antenna interference airborne captive flight structure |
| KR20150104842A (en) * | 2014-03-06 | 2015-09-16 | 국방과학연구소 | Appatatus for aircraft captive flight test for guided anti-tank missile |
| CN204574971U (en) * | 2015-04-23 | 2015-08-19 | 贵州航天电子科技有限公司 | A kind of suction wave apparatus of electronic fuse |
| CN105521836A (en) * | 2016-02-04 | 2016-04-27 | 广州苏试众博环境实验室有限公司 | Low-air-pressure testing system |
| CN205633097U (en) * | 2016-05-24 | 2016-10-12 | 贵州航天电子科技有限公司 | Hang and fly test device |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106564817A (en) * | 2016-08-31 | 2017-04-19 | 贵州航天电子科技有限公司 | Aircraft test platform cableway stepless lifting device |
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Application publication date: 20160824 |
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| RJ01 | Rejection of invention patent application after publication |