CN207482206U - Unmanned plane airborne geophysical prospecting magnetic puts crystal detection nacelle device - Google Patents
Unmanned plane airborne geophysical prospecting magnetic puts crystal detection nacelle device Download PDFInfo
- Publication number
- CN207482206U CN207482206U CN201721487904.7U CN201721487904U CN207482206U CN 207482206 U CN207482206 U CN 207482206U CN 201721487904 U CN201721487904 U CN 201721487904U CN 207482206 U CN207482206 U CN 207482206U
- Authority
- CN
- China
- Prior art keywords
- magnetic
- crystal detection
- unmanned plane
- geophysical prospecting
- detection
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Landscapes
- Geophysics And Detection Of Objects (AREA)
Abstract
The utility model discloses a kind of unmanned plane airborne geophysical prospecting magnetic to put crystal detection nacelle device, it includes housing, circuit board, fixator and magnetic put crystal detection, the housing includes front fairing, cylindrical body and rear radome fairing, the fixator is the structure that two block baffles are fixed by strut connection, crystal detection is put for fixing the magnetic, the magnetic is put crystal detection and is placed in sponge, it is positioned over after being fixed by fixator in the cylindrical body, the circuit board is set on the baffle, crystal detection is put via the baffle with magnetic to be electrically connected, the front fairing and rear radome fairing are connected by the baffle with the cylindrical body.The utility model magnetic is enable to put crystal detection safely carry aboard, and can effectively reduce the influence that shock, vibrations, low temperature etc. bring crystal, ensure being smoothed out for detection operations, can be widely applied to airborne geophysical prospecting field of operation.
Description
Technical field
Crystal detection nacelle device is put the utility model is related to a kind of airborne geophysical prospecting magnetic more particularly to a kind of unmanned plane boat is put
Crystal nacelle device can be applied to airborne geophysical prospecting field of operation.
Background technology
At present, aerogeophysical survey (airborne geophysical prospecting) is one kind of geophysical prospecting method, special by what is equipped on aircraft
Geophysical prospecting equipment detects the variation of various geophysical fields, research and searching subsurface geological structure and mineral products during navigation.Boat
Empty visit with have it is man-machine based on want carrier, also facing a danger property is big, cost is high while good achievement is obtained, flexibility is poor
And the problems such as operating efficiency is low.
Unmanned plane airborne geophysical prospecting has that efficient, at low cost, risk is small, it is excellent not influenced etc. by orographic condition and human factor
Point is the effective way to solve the above problems.However, unmanned plane is still faced with many difficulties applied to Aero Geophysical Survey,
One of them is how to realize the carry that magnetic puts crystal detection.
Tradition, which has, man-machine put crystal detection by magnetic often in airborne geophysical prospecting and is placed in airframe, but due to unmanned plane volume
Small, it is little to place load space in fuselage, and it is larger to put crystal detection volume for magnetic in addition, cannot be by rain, snow and low during work
Temperature influence, if no special protection magnetic put crystal detection crystal case will be unable to complete airborne geophysical prospecting operation.
Therefore, before unmanned plane carries out airborne geophysical prospecting job task, determine that magnetic is put crystal detection fixes aboard simultaneously
It is a highly important ring in load system to make its safety, the method for normal work.At present, the country there is no successful magnetic to put detection
The airborne fixing device of crystal.
Utility model content
The purpose of this utility model is that filling up the blank of the prior art, magnetic puts spy when providing a kind of unmanned plane airborne geophysical prospecting
Survey crystal nacelle device, it is ensured that magnetic puts the safety of crystal detection in flight operation, evades unmanned aerial vehicle onboard magnetic and puts crystal detection and exists
By the possibility destroyed in flight course, the work of unmanned plane airborne geophysical prospecting is effectively ensured in crystal is subject to when reducing flight resistance
Make.
The unmanned plane airborne geophysical prospecting magnetic of the utility model puts crystal detection nacelle device and includes housing, circuit board, fixator
Crystal detection is put with magnetic, the housing includes front fairing, cylindrical body and rear radome fairing, and the fixator is connects by strut
The structure of two block baffles is fixed, crystal detection is put for fixing the magnetic, the magnetic is put crystal detection and is placed in sponge, by solid
Determine to be positioned in the cylindrical body after device is fixed, the circuit board is set on the baffle, and spy is put via the baffle and magnetic
Crystal electrical connection is surveyed, the front fairing and rear radome fairing are connected by the baffle with the cylindrical body.
It is preferred that the sponge has the groove that the magnetic is coordinated to put detection crystalline form shape.
It is preferred that front and rear two magnetic placed side by side puts crystal detection in the cylindrical body, it is brilliant to put detection with the front side magnetic
The circuit board arrangement of body connection is in front fairing, radome fairing after putting the circuit board arrangement that crystal detection connect with the rear side magnetic
In.
It is preferred that two baffles are the poroid plate with through-hole, it is full of sponge between two baffles.
It is preferred that fixed iron hoop is provided on the housing, for hanging in airframe.
The utility model is compared with prior art：
(1) magnetic can be put to crystal detection carry on unmanned plane, and equipped with operating circuit, ensure airborne geophysical prospecting operation
It smoothly completes.
(2) crystal case shell has advanced aerodynamic configuration, can effectively reduce resistance during unmanned plane physical prospecting flight operation
Power increases endurance and voyage.
(3) crystal case shell is made of reinforced plastic glass fibre, and internal structure is cellular structure, has good shock resistance
Property and larger intensity, and weight is smaller compared with other materials and structure, can effectively avoid crystal case because striking bird
It is crushed when class or other objects.
(4) magnetic is put and is surrounded by sponge outside crystal detection, and the environment of bradyseism and heat preservation is provided for crystal, magnetic is made to put detection
Crystal still can be with steady operation in the mal-condition that temperature change is very fast, vibrations are larger.
Description of the drawings
Fig. 1 puts crystal detection nacelle device appearance diagram for unmanned plane airborne geophysical prospecting magnetic.
Fig. 2 puts crystal detection nacelle device biopsy cavity marker devices schematic diagram for unmanned plane airborne geophysical prospecting magnetic.
Fig. 3 is fixer structure schematic diagram.
Each component in figure：1. front fairing 2. fixes 4. circuit board of radome fairing, 5. fixator, 6. sponge after iron hoop 3.
7. magnetic puts 8. baffle of crystal detection
Specific embodiment
The technical solution of the utility model is described in detail below in conjunction with the accompanying drawings：
The utility model from structure fixed iron hoop 2 and crystal case shell as shown in Figure 1, be mainly made of.Fixed iron hoop 2
Upper part is a metal derby, and main function is intensity when ensureing crystal case carry aboard, is one outside metal derby
A fixation iron hoop 2 being made of sheet metal structural reduces the cost needed for production while fixed iron hoop weight is reduced.Crystal
Case shell includes front fairing 1, rear radome fairing 3 and cylindrical body, and material therefor is reinforced plastic glass fibre, and using cellular knot
Structure increases structural strength and shock resistance compared with other materials while weight is mitigated.
As shown in Figure 2,3, in cylindrical body crystal detection 7 is put by two magnetic placed side by side before and after 5 sponge 6 of fixator.
As shown in figure 3, fixator 5 is the structure that two block baffles 8 are fixed by strut connection, baffle 8 is the poroid plate with through-hole, is borrowed
The fixed magnetic of through-hole installation is helped to put crystal detection 7 and circuit board 4, and realizes that circuit board 4 and magnetic put the electricity of crystal detection 7 via through-hole
Connection.The present embodiment fixes two magnetic by two fixators 4 and puts crystal detection 7, can also be fixed by two fixators 4
One magnetic puts the both ends of crystal detection 7.Fixed magnetic fills up sponge between putting two pieces of plate washers of 7 one end of crystal detection.Sponge 6 has
The groove of 7 shape of crystal detection cooperation is put with magnetic.Sponge, which can mitigate magnetic in operation, puts crystal detection 7 and shakes, and put to magnetic
Crystal detection 7 is kept the temperature, and magnetic is made to put crystal detection still can stablize work in the mal-condition that temperature change is very fast, vibrations are larger
Make.
Front fairing 1 and rear radome fairing 3 are separately fixed on the baffle 8 of rear and front end, are connected with cylindrical body.Two
Circuit board 4 is arranged respectively in front and rear radome fairing, and front and rear radome fairing is that have outstanding gas by what aerodynamics was calculated
The structure of dynamic shape, can greatly reduce air drag in carry, and the voyage and endurance when making carry crystal case are longer, progress
It is responded faster during TRAJECTORY CONTROL.
When mounted, first the sponge of middle section 6 is put into inside cylindrical body, then two magnetic is put crystal detection 7 and are put into
In sponge 6, two baffles 8 are then placed at 6 both ends of the sponge of middle section, and fixator 5 is packed at crystal both ends, to ensure
Axial dipole field does not occur for fixator in flight course, thus reduces the displacement that magnetic puts crystal detection 7.By the baffle 8 at both ends with
Circuit board 4 connects, and connects electric wire and cable, then installs, pacifies the sponge 6 of circuit, fixator 5, circuit board 4 is connected
After installing, two circuit boards 4 are housed in respectively in former and later two radome fairings.Rectification before finally being loaded onto in the rear and front end of crystal case
Cover 1 and rear radome fairing 3, put on fixed iron hoop 2.
Fixator 5, circuit board 4, baffle 8 and magnetic put crystal detection 7 and link together, composition magnetic put crystal detection power supply and
Data transmission module；The data that electric wire and cable pass through sponge 6 to power for crystal and put magnetic measured by crystal detection 7 are transmitted to
On aircraft；Magnetic is put crystal detection 7 and is placed in sponge 6, and the effect of sponge 6 is to mitigate the vibrations that magnetic puts crystal detection 7 in operation,
And crystal detection heat preservation is put to magnetic, prevent it from can not work due to temperature change is excessive.
Magnetic can be put crystal detection 7 and is fixed on unmanned plane by the utility model, prevented in flight course crystal by
It hits, reduce the vibrations of crystal and it is kept the temperature, is powered so that crystal safety, normal work.
The examples detailed above of the utility model is only intended to clearly illustrate the utility model example, and is not pair
The restriction of the embodiment of the utility model.For those of ordinary skill in the art, on the basis of the above description
It can also make other variations or changes in different ways.Here all embodiments can not be exhaustive.It is every to belong to
The obvious changes or variations that the technical solution of the utility model is extended out are still in the scope of protection of the utility model
Row.
Claims (6)
1. a kind of unmanned plane airborne geophysical prospecting magnetic puts crystal detection nacelle device, it is characterised in that：Including housing, circuit board, fixation
Device and magnetic put crystal detection, and the housing includes front fairing, cylindrical body and rear radome fairing, and the fixator is connects by strut
The structure for fixing two block baffles is connect, puts crystal detection for fixing the magnetic, the magnetic is put crystal detection and is placed in sponge, passes through
Fixator is positioned over after fixing in the cylindrical body, and the circuit board is set on the baffle, is put via the baffle with magnetic
Crystal detection is electrically connected, and the front fairing and rear radome fairing are connected by the baffle with the cylindrical body.
2. a kind of unmanned plane airborne geophysical prospecting magnetic as described in claim 1 puts crystal detection nacelle device, it is characterized in that being：Institute
Stating sponge has the groove that the magnetic is coordinated to put detection crystalline form shape.
3. a kind of unmanned plane airborne geophysical prospecting magnetic as described in claim 1 puts crystal detection nacelle device, it is characterized in that being：Institute
It states front and rear two magnetic placed side by side in cylindrical body and puts crystal detection, the circuit board that crystal detection connect is put with the front side magnetic
Configuration is in front fairing, after putting the circuit board arrangement that crystal detection connect with the rear side magnetic in radome fairing.
4. a kind of unmanned plane airborne geophysical prospecting magnetic as described in any one of claim 1-3 puts crystal detection nacelle device, special
Sign is to be：Two baffles are the poroid plate with through-hole, are full of sponge between two baffles.
5. a kind of unmanned plane airborne geophysical prospecting magnetic as described in claim 1 puts crystal detection nacelle device, it is characterized in that being：Institute
It states and is provided with nacelle device hanging the fixation iron hoop on airframe on housing.
6. a kind of unmanned plane airborne geophysical prospecting magnetic as described in claim 1 puts crystal detection nacelle device, it is characterized in that being：Institute
Housing is stated to be made of cellular structure reinforced plastic glass fibre.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721487904.7U CN207482206U (en) | 2017-11-09 | 2017-11-09 | Unmanned plane airborne geophysical prospecting magnetic puts crystal detection nacelle device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721487904.7U CN207482206U (en) | 2017-11-09 | 2017-11-09 | Unmanned plane airborne geophysical prospecting magnetic puts crystal detection nacelle device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207482206U true CN207482206U (en) | 2018-06-12 |
Family
ID=62476382
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721487904.7U Active CN207482206U (en) | 2017-11-09 | 2017-11-09 | Unmanned plane airborne geophysical prospecting magnetic puts crystal detection nacelle device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207482206U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109367800A (en) * | 2018-08-28 | 2019-02-22 | 郑州郑飞机电技术有限责任公司 | A kind of novel gondola for aviation loading |
| CN111824426A (en) * | 2020-06-15 | 2020-10-27 | 成都飞机工业（集团）有限责任公司 | Pod appearance structure for launching dropsonde |
| CN112124606A (en) * | 2020-09-30 | 2020-12-25 | 中航(成都)无人机系统股份有限公司 | But modularization equipment's airborne nacelle |
| CN112415612A (en) * | 2020-10-30 | 2021-02-26 | 哈尔滨飞机工业集团有限责任公司 | Helicopter cantilever magnetic probe rod |
| CN115447794A (en) * | 2022-09-26 | 2022-12-09 | 中铁二院工程集团有限责任公司 | Unmanned aerial vehicle aerial geophysical prospecting crystal nacelle device |
-
2017
- 2017-11-09 CN CN201721487904.7U patent/CN207482206U/en active Active
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109367800A (en) * | 2018-08-28 | 2019-02-22 | 郑州郑飞机电技术有限责任公司 | A kind of novel gondola for aviation loading |
| CN109367800B (en) * | 2018-08-28 | 2021-10-15 | 郑州郑飞机电技术有限责任公司 | Novel nacelle for aerial cargo |
| CN111824426A (en) * | 2020-06-15 | 2020-10-27 | 成都飞机工业（集团）有限责任公司 | Pod appearance structure for launching dropsonde |
| CN112124606A (en) * | 2020-09-30 | 2020-12-25 | 中航(成都)无人机系统股份有限公司 | But modularization equipment's airborne nacelle |
| CN112415612A (en) * | 2020-10-30 | 2021-02-26 | 哈尔滨飞机工业集团有限责任公司 | Helicopter cantilever magnetic probe rod |
| CN112415612B (en) * | 2020-10-30 | 2024-05-24 | 哈尔滨飞机工业集团有限责任公司 | Helicopter cantilever magnetism probe rod |
| CN115447794A (en) * | 2022-09-26 | 2022-12-09 | 中铁二院工程集团有限责任公司 | Unmanned aerial vehicle aerial geophysical prospecting crystal nacelle device |
| CN115447794B (en) * | 2022-09-26 | 2023-09-05 | 中铁二院工程集团有限责任公司 | Unmanned aerial vehicle aviation geophysical prospecting detection crystal nacelle device |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN207482206U (en) | Unmanned plane airborne geophysical prospecting magnetic puts crystal detection nacelle device | |
| CN106218881B (en) | Vertical layout fuel power quadrotor flying platform | |
| CN206639924U (en) | A kind of aircraft antenna radome fairing | |
| CN103407569B (en) | A kind of frequency-variable controller for air bag pressure control system of stratospheric airship | |
| US20160161625A1 (en) | Geophysical survey system using hybrid aircraft | |
| CN105346710A (en) | Six-rotor unmanned plane | |
| CN207602785U (en) | One kind has high wave-penetrating composite material antenna radar cover | |
| CN202609078U (en) | Tail control system for unmanned helicopter | |
| CN204998767U (en) | Double -deck rotor unmanned aerial vehicle of modified | |
| CN108227023A (en) | CH-3 unmanned plane airborne geophysical prospecting magnetic puts combined station application system | |
| ITMI20112145A1 (en) | TEST CAP OF AVIONIC SENSORS AND METHOD FOR TESTING AVIONIC SENSORS | |
| CN104931228A (en) | Double-body super-high aspect ratio aircraft wind tunnel force measurement test supporting device | |
| CN204223179U (en) | A kind of three rotor wing unmanned aerial vehicles high with flexible hook accurate positioning intensity | |
| CN203937860U (en) | A kind of Y type model of an airplane helical mount | |
| CN203199177U (en) | Multi-shaft aircraft rack improvement structure | |
| CN105947174A (en) | Airplane | |
| CN209617517U (en) | A kind of dynamic quadrotor of double hair oil | |
| CN207450269U (en) | For the radiator structure of the dynamic unmanned plane of oil | |
| CN106741999A (en) | A kind of reception gondola for being applied to unmanned plane time domain aviation electromagnetic system | |
| CN209337010U (en) | A kind of radiator structure of the dynamic unmanned plane of oil | |
| CN209258410U (en) | A kind of fuel system for the dynamic unmanned plane of oil | |
| CN108750126A (en) | A kind of dynamic quadrotor of double hair oil | |
| CN209241302U (en) | A kind of unmanned aerial vehicle body and unmanned plane | |
| CN205239894U (en) | Super short range unmanned aerial vehicle system of small -size folding wing | |
| CN206218240U (en) | A kind of battery cabin structure of multi-rotor unmanned aerial vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |