CN106226820A - A kind of lightweight inflation ring supporting construction for pod propulsion time domain aviation transient electromagnetic exploration system - Google Patents
A kind of lightweight inflation ring supporting construction for pod propulsion time domain aviation transient electromagnetic exploration system Download PDFInfo
- Publication number
- CN106226820A CN106226820A CN201610515453.7A CN201610515453A CN106226820A CN 106226820 A CN106226820 A CN 106226820A CN 201610515453 A CN201610515453 A CN 201610515453A CN 106226820 A CN106226820 A CN 106226820A
- Authority
- CN
- China
- Prior art keywords
- time domain
- adherent buckle
- nylon adherent
- transient electromagnetic
- exploration system
- 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.)
- Pending
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Classifications
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01V—GEOPHYSICS; GRAVITATIONAL MEASUREMENTS; DETECTING MASSES OR OBJECTS; TAGS
- G01V3/00—Electric or magnetic prospecting or detecting; Measuring magnetic field characteristics of the earth, e.g. declination, deviation
Abstract
A kind of lightweight inflation ring supporting construction for pod propulsion time domain aviation transient electromagnetic exploration system, belong to time domain aviation transient electromagnetic exploration system field, solving the supporting construction of current pod propulsion time domain aviation transient electromagnetic exploration system, generally to there is construction weight bigger, the problems such as transportation volume is big, it comprises inflated supporting ring, signal cable and nylon adherent buckle, the tube wall of inflated supporting ring is made up of the inner liner of inner side and the bearing layer in outside, inner liner uses high modulus polyethylene thin film, can ensure that sealing, bearing layer uses glass fibre integrated weaved, overall structure is light and voltage endurance capability is high, by high-pressure aerated lifting overall structure rigidity；Signal cable is laid two weeks or the most all along the circumference of inflated supporting ring, and signal cable is connected with inflated supporting ring by nylon adherent buckle；The present invention is used for electromagnetic survey.
Description
Technical field
The invention belongs to time domain aviation transient electromagnetic exploration system field, be specifically related to a kind of for pod propulsion time domain
The lightweight inflation ring supporting construction of aviation transient electromagnetic exploration system.
Background technology
Pod propulsion time domain aviation transient electromagnetic exploration system can be used for the resource exploration such as mineral products, oil gas, has detection deep
The advantages such as degree is big, and detection accuracy is high, have broad application prospects；The helicopter time domain aviation of China's independent research in 2012
Electromagnetic survey system is in Tongbo County, Henan Province initial test flight success, at present, pod propulsion time domain aviation transient electromagnetic exploration system
Supporting construction mainly use glass reinforced plastic pipe or wooden truss structure, generally there is construction weight and ask compared with big, transportation volume is big etc.
Topic；For increasing the physical dimension of pod propulsion time domain aviation transient electromagnetic exploration system, reduce construction weight, propose this programme.
Summary of the invention
The invention aims to solve the supporting construction of current pod propulsion time domain aviation transient electromagnetic exploration system
The problems referred to above existed, it is provided that a kind of lightweight inflation ring for pod propulsion time domain aviation transient electromagnetic exploration system supports
Structure, its technical scheme is as follows:
A kind of lightweight inflation ring supporting construction for pod propulsion time domain aviation transient electromagnetic exploration system, it comprises inflation
Pushing out ring, signal cable and nylon adherent buckle, the tube wall of inflated supporting ring is made up of the inner liner of inner side and the bearing layer in outside, airtight
Layer uses high modulus polyethylene thin film, it is ensured that sealing, and bearing layer uses glass fibre integrated weaved, and overall structure is light
And voltage endurance capability is high, by high-pressure aerated lifting overall structure rigidity；Signal cable is laid two weeks along the circumference of inflated supporting ring
Or the most all, signal cable is connected with inflated supporting ring by nylon adherent buckle, and the tube wall around inflated supporting ring sews a plurality of Buddhist nun
One side in the villous surface of dragon thread gluing or glochild face, according to signal cable in the one side of the sewing every nylon adherent buckle on tube wall
Lay week number and the another side of nylon adherent buckle of position sewing respective amount, one end of the another side of every described nylon adherent buckle
Sew up with the one side of sewing nylon adherent buckle on tube wall, the part beyond stitching surround signal cable corresponding part and with seam
The one side of system nylon adherent buckle on tube wall is bonding.
The invention have the benefit that the incompressible carrying effect introducing the blowing pressure, by the gas of inflated supporting ring
Hold rigidity and substitute glass reinforced plastic pipe or the material stiffness of wooden truss structure, it is achieved that pod propulsion time domain aviation transient electromagnetic is explored
The lightweight of system support structure, and Assembling is convenient, and venting curling volume after folding is minimum, it is simple to transport, cable exists
While playing electrical property, moreover it is possible to the rigidity of structure providing certain supports so that overall structure weight is little, performance is high.
Accompanying drawing explanation
Fig. 1 is the overall structure schematic diagram of the present invention；
Fig. 2 is the schematic cross-section of the tube wall of inflated supporting ring；
Fig. 3 is the schematic cross-section of inflated supporting ring and signal cable junction；
Fig. 4 is the decomposing schematic representation of Fig. 3.
Detailed description of the invention
Referring to figs. 1 through Fig. 4, a kind of lightweight inflation ring for pod propulsion time domain aviation transient electromagnetic exploration system supports
Structure, it comprises inflated supporting ring 1, signal cable 2 and nylon adherent buckle 3, and the tube wall of inflated supporting ring 1 is by the inner liner 1-of inner side
1 and outside bearing layer 1-2 constitute, inner liner 1-1 uses high modulus polyethylene thin film, it is ensured that sealing, bearing layer 1-2
Employing glass fibre is integrated weaved, and overall structure is light and voltage endurance capability is high, by high-pressure aerated lifting overall structure rigidity；Letter
Number cable 2 is laid two weeks along the circumference of inflated supporting ring 1 or how week, and signal cable 2 is by nylon adherent buckle 3 and inflated supporting ring
1 connects, and the tube wall around inflated supporting ring 1 sews the one side in the villous surface of a plurality of nylon adherent buckle 3 or glochild face, sews at pipe
According to all numbers of the laying of signal cable 2 and the nylon stick of position sewing respective amount in the one side of every the nylon adherent buckle 3 on wall
The another side of button 3, the one side seam of one end of the another side of every described nylon adherent buckle 3 and the sewing nylon adherent buckle 3 on tube wall
Closing, part beyond stitching is surrounded the corresponding part of signal cable 2 and glues with the one side of sewing nylon adherent buckle 3 on tube wall
Connect.
The carry-on signal sources such as the two ends of signal cable 2 and helicopter are connected, and entirety can be by many hoist cables or draw
Net is connected with aircraft multi-point suspended, it is easy to implement lifting.
Claims (4)
1. the lightweight inflation ring supporting construction for pod propulsion time domain aviation transient electromagnetic exploration system, it is characterised in that
It comprises inflated supporting ring (1), signal cable (2) and nylon adherent buckle (3), airtight by inner side of the tube wall of inflated supporting ring (1)
The bearing layer (1-2) in layer (1-1) and outside is constituted；Signal cable (2) is laid two weeks or many along the circumference of inflated supporting ring (1)
In week, signal cable (2) is connected with inflated supporting ring (1) by nylon adherent buckle (3).
A kind of lightweight inflation ring for pod propulsion time domain aviation transient electromagnetic exploration system supports
Structure, it is characterised in that inner liner (1-1) uses high modulus polyethylene thin film.
A kind of lightweight inflation ring for pod propulsion time domain aviation transient electromagnetic exploration system supports
Structure, it is characterised in that bearing layer (1-2) uses glass fibre integrated weaved.
A kind of lightweight inflation ring for pod propulsion time domain aviation transient electromagnetic exploration system supports
Structure, it is characterised in that around inflated supporting ring (1) tube wall sew a plurality of nylon adherent buckle (3) villous surface or glochild face in
Simultaneously, according to the laying week number and position sewing of signal cable (2) in the one side of the sewing every nylon adherent buckle (3) on tube wall
The another side of the nylon adherent buckle (3) of respective amount, one end of the another side of every described nylon adherent buckle (3) and sewing are on tube wall
The one side of nylon adherent buckle (3) sew up, part beyond stitching surrounds the corresponding part of signal cable (2) and with sewing at tube wall
On the one side of nylon adherent buckle (3) bonding.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610515453.7A CN106226820A (en) | 2016-07-04 | 2016-07-04 | A kind of lightweight inflation ring supporting construction for pod propulsion time domain aviation transient electromagnetic exploration system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610515453.7A CN106226820A (en) | 2016-07-04 | 2016-07-04 | A kind of lightweight inflation ring supporting construction for pod propulsion time domain aviation transient electromagnetic exploration system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106226820A true CN106226820A (en) | 2016-12-14 |
Family
ID=57519060
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610515453.7A Pending CN106226820A (en) | 2016-07-04 | 2016-07-04 | A kind of lightweight inflation ring supporting construction for pod propulsion time domain aviation transient electromagnetic exploration system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106226820A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114001946A (en) * | 2021-11-11 | 2022-02-01 | 哈尔滨工业大学 | Comprehensive test system for bearing performance of inflatable ring structure |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101981469A (en) * | 2008-02-25 | 2011-02-23 | 吉欧泰科航空物探有限公司 | Airborne electromagnetic transmitter coil system |
| CN102249005A (en) * | 2011-04-14 | 2011-11-23 | 陈斌 | Towed bird helicopter-borne time domain airborne electromagnetic detection system |
| CN103560333A (en) * | 2013-11-14 | 2014-02-05 | 哈尔滨工业大学 | Flexible paraboloid satellite-borne antenna with reinforcing frame |
| WO2014169317A1 (en) * | 2013-04-15 | 2014-10-23 | Nrg Exploration Cc | Transmitter coil system for airborne surveys |
| WO2015000021A1 (en) * | 2013-07-05 | 2015-01-08 | Outer-Rim Developments Pty Ltd | A support structure |
| CN105261818A (en) * | 2015-11-06 | 2016-01-20 | 哈尔滨工业大学 | Air inflation support ring for space-borne radial rib inflation expansion antenna |
-
2016
- 2016-07-04 CN CN201610515453.7A patent/CN106226820A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101981469A (en) * | 2008-02-25 | 2011-02-23 | 吉欧泰科航空物探有限公司 | Airborne electromagnetic transmitter coil system |
| CN102249005A (en) * | 2011-04-14 | 2011-11-23 | 陈斌 | Towed bird helicopter-borne time domain airborne electromagnetic detection system |
| WO2014169317A1 (en) * | 2013-04-15 | 2014-10-23 | Nrg Exploration Cc | Transmitter coil system for airborne surveys |
| WO2015000021A1 (en) * | 2013-07-05 | 2015-01-08 | Outer-Rim Developments Pty Ltd | A support structure |
| CN103560333A (en) * | 2013-11-14 | 2014-02-05 | 哈尔滨工业大学 | Flexible paraboloid satellite-borne antenna with reinforcing frame |
| CN105261818A (en) * | 2015-11-06 | 2016-01-20 | 哈尔滨工业大学 | Air inflation support ring for space-borne radial rib inflation expansion antenna |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114001946A (en) * | 2021-11-11 | 2022-02-01 | 哈尔滨工业大学 | Comprehensive test system for bearing performance of inflatable ring structure |
| CN114001946B (en) * | 2021-11-11 | 2024-04-16 | 哈尔滨工业大学 | Comprehensive test system for bearing performance of inflatable ring structure |
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20161214 |
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| RJ01 | Rejection of invention patent application after publication |