CN103523240B - Airborne geophysical prospecting equipment props up extension structure for pod - Google Patents
Airborne geophysical prospecting equipment props up extension structure for pod Download PDFInfo
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- CN103523240B CN103523240B CN201210233027.6A CN201210233027A CN103523240B CN 103523240 B CN103523240 B CN 103523240B CN 201210233027 A CN201210233027 A CN 201210233027A CN 103523240 B CN103523240 B CN 103523240B
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- gondola
- back rest
- axle beam
- coil
- trailing edge
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- 238000009434 installation Methods 0.000 description 8
- 210000000038 chest Anatomy 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 239000013536 elastomeric material Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
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Abstract
The present invention relates to field of airplane design, a kind of airborne geophysical prospecting equipment is provided to prop up extension structure for pod, wherein, covering is fixed in coil hatch cover and coil cabin, and to synthesize a two in the middle of conical be columniform housing, built-in transmitter coil, gondola front-axle beam is parallel with the gondola back rest and binding clip position is enclosed within transmitter coil, nose ribs are connected on front side of gondola front-axle beam perpendicular to gondola front-axle beam, stage casing rib is connected between gondola front-axle beam and the gondola back rest perpendicular to gondola front-axle beam and the gondola back rest, trailing edge rib is connected on rear side of the gondola back rest perpendicular to the gondola back rest, nose ribs, stage casing rib, trailing edge rib in one plane forms water-drop-shaped structure, nose ribs outside face is covered with skins front edges, stage casing rib upper and lower surface is covered with stage casing covering, trailing edge rib outside face is covered with trailing edge skin, skins front edges, stage casing covering, trailing edge skin is connected with wing rounding off by wing-gondola fairing.The present invention can realize the reliable fixing of coil, and ensures setting accuracy.
Description
Technical field
The present invention relates to field of airplane design, particularly relate to a kind of airborne geophysical prospecting equipment and prop up extension structure for pod.
Background technology
Airborne geophysical prospecting equipment pod is used for installing aviation three frequently dispatch coil, and is connected with aircraft wing, domesticly at present there is no this kind of technology.
Summary of the invention
The technical problem to be solved in the present invention: provide a kind of airborne geophysical prospecting equipment to prop up extension structure for pod.
Technical scheme of the present invention: a kind of airborne geophysical prospecting equipment props up extension structure for pod, comprise: two is be semi-cylindrical coil hatch cover in the middle of half cone-shaped, two is fix covering for semi-cylindrical coil cabin in the middle of half cone-shaped, be respectively pincerlike gondola front-axle beam and the gondola back rest, covering is fixed in coil hatch cover and coil cabin, and to synthesize a two in the middle of conical be columniform housing, built-in transmitter coil, gondola front-axle beam is parallel with the gondola back rest and binding clip position is enclosed within transmitter coil, nose ribs are connected on front side of gondola front-axle beam perpendicular to gondola front-axle beam, stage casing rib is connected between gondola front-axle beam and the gondola back rest perpendicular to gondola front-axle beam and the gondola back rest, trailing edge rib is connected on rear side of the gondola back rest perpendicular to the gondola back rest, nose ribs, stage casing rib, trailing edge rib in one plane forms water-drop-shaped structure, nose ribs outside face is covered with skins front edges, stage casing rib upper and lower surface is covered with stage casing covering, trailing edge rib outside face is covered with trailing edge skin, skins front edges, stage casing covering, trailing edge skin is connected with wing rounding off by wing-gondola fairing.
A kind of airborne geophysical prospecting equipment props up extension structure for pod, comprise: two is be semi-cylindrical coil hatch cover in the middle of half cone-shaped, two is fix covering for semi-cylindrical coil cabin in the middle of half cone-shaped, be respectively pincerlike gondola front-axle beam and the gondola back rest, the gondola central sill of binding clip shape, covering is fixed in coil hatch cover and coil cabin, and to synthesize a two in the middle of conical be columniform housing, built-in receiving coil, gondola front-axle beam, gondola central sill is parallel with the gondola back rest and binding clip position is enclosed within receiving coil, gondola front-axle beam, gondola central sill and the gondola back rest are spirally connected with connecting panel respectively, connecting panel and angle section are spirally connected, angle section and bumper are spirally connected, coil reaction plate on bumper and receiving coil is spirally connected, nose ribs are connected on front side of gondola front-axle beam perpendicular to gondola front-axle beam, stage casing rib is connected between gondola front-axle beam and the gondola back rest perpendicular to gondola front-axle beam and the gondola back rest, trailing edge rib is connected on rear side of the gondola back rest perpendicular to the gondola back rest, nose ribs, stage casing rib, trailing edge rib in one plane forms water-drop-shaped structure, nose ribs outside face is covered with skins front edges, stage casing rib upper and lower surface is covered with stage casing covering, trailing edge rib outside face is covered with trailing edge skin, skins front edges, stage casing covering, trailing edge skin is connected with wing rounding off by wing-gondola fairing.
Beneficial effect of the present invention: airborne geophysical prospecting equipment provided by the invention props up extension structure for pod and connects safe and reliable, and safeguard easy maintenance, structure has good intensity, rigidity, maintainability.There is shock-absorbing function and antimagnetic performance, the reliable fixing of coil can be realized, and ensure setting accuracy.
Accompanying drawing explanation
Fig. 1 is starboard wing equipment pod structural representation of the present invention.
Fig. 2 is port wing equipment pod structural representation of the present invention.
Fig. 3 is transmitter coil scheme of installation of the present invention.
Fig. 4 is receiving coil scheme of installation of the present invention.
Fig. 5 is present device gondola schematic layout pattern.
Fig. 6 is present device gondola scheme of installation.
Detailed description of the invention
A kind of airborne geophysical prospecting equipment of the present invention props up the starboard wing gondola hanging structure for pod and adopts two-beam type configuration, is realized the transmission of equipment installation and Main Load by front and back twin beams.For avoiding occurring interference to coil working, forward and backward beam, rib, covering and fastener (except transmitter coil installs lid connecting element) all adopt non-metallic material, and its connection mode adopts glueds joint.
Starboard wing gondola comprises: two is be semi-cylindrical coil hatch cover in the middle of half cone-shaped, two is fix covering for semi-cylindrical coil cabin in the middle of half cone-shaped, be respectively pincerlike gondola front-axle beam and the gondola back rest, covering is fixed in coil hatch cover and coil cabin, and to synthesize a two in the middle of conical be columniform housing, built-in transmitter coil, gondola front-axle beam is parallel with the gondola back rest and binding clip position is enclosed within transmitter coil, nose ribs are connected on front side of gondola front-axle beam perpendicular to gondola front-axle beam, stage casing rib is connected between gondola front-axle beam and the gondola back rest perpendicular to gondola front-axle beam and the gondola back rest, trailing edge rib is connected on rear side of the gondola back rest perpendicular to the gondola back rest, nose ribs, stage casing rib, trailing edge rib in one plane forms water-drop-shaped structure, nose ribs outside face is covered with skins front edges, stage casing rib upper and lower surface is covered with stage casing covering, trailing edge rib outside face is covered with trailing edge skin, skins front edges, stage casing covering, trailing edge skin is connected with wing rounding off by wing-gondola fairing.
An embodiment of starboard wing gondola is shown in Fig. 1, is fixed covering 110, coil hatch cover 111, transmitter coil 112 etc. formed by gondola front-axle beam 101, the gondola back rest 102, nose ribs 103, stage casing rib 104, trailing edge rib 105, wing-gondola fairing 106, skins front edges 107, stage casing covering 108, trailing edge skin 109, coil cabin.
Gondola front-axle beam 101 glueds joint with nose ribs 103, stage casing rib 104 and uses rivet interlacement, the gondola back rest 102 glueds joint with stage casing rib 104, trailing edge rib 105 and uses rivet interlacement, the structural framework of above part composition gondola, wherein gondola front-axle beam 101, the gondola back rest 102, stage casing rib 104 are as primary load bearing box section, bear and transmit Main Load.Skins front edges 107, stage casing covering 108, trailing edge skin 109 are used for covered structure skeleton, provide rectification profile, and beam, glued joint between rib cage fixing.Coil cabin is fixed covering 110 and is gluedd joint with gondola front-axle beam 101, the gondola back rest 102, for coil cabin provides rectification profile; Coil hatch cover 111 is similarly coil cabin and provides rectification profile, installs as coil, the passage of dismounting simultaneously, fixes covering 110, gondola front-axle beam 101, the gondola back rest 102 be connected by screw, for removably connecting with coil cabin.Transmitter coil 112 is fixed on gondola front-axle beam 101 and the gondola back rest 102, uses bolt to connect, conveniently can install, dismantles and debug.Wing-gondola fairing 106 provides rectification profile for the outer hanging joint of wing and gondola and wing join domain, its one end is fixed on skins front edges 107, stage casing covering 108 and trailing edge skin 109, the other end is fixed on wing, uses screw to connect, convenient installation, dismounting.
A kind of airborne geophysical prospecting of the present invention equipment props up hangs that structure for pod port wing gondola is same with wing to be connected by front and back twin beams, but three beams are fixed before, during and after adopting on coil fixed way, the connection of beam and coil adopts non-rigid connection, by dampening assembly fixed coil.All the other versions and material are all consistent with right side.
Port wing gondola comprises: two is be semi-cylindrical coil hatch cover in the middle of half cone-shaped, two is fix covering for semi-cylindrical coil cabin in the middle of half cone-shaped, be respectively pincerlike gondola front-axle beam and the gondola back rest, the gondola central sill of binding clip shape, covering is fixed in coil hatch cover and coil cabin, and to synthesize a two in the middle of conical be columniform housing, built-in receiving coil, gondola front-axle beam, gondola central sill is parallel with the gondola back rest and binding clip position is enclosed within receiving coil, gondola front-axle beam, gondola central sill and the gondola back rest are spirally connected with connecting panel respectively, connecting panel and angle section are spirally connected, angle section and bumper are spirally connected, coil reaction plate on bumper and receiving coil is spirally connected, nose ribs are connected on front side of gondola front-axle beam perpendicular to gondola front-axle beam, stage casing rib is connected between gondola front-axle beam and the gondola back rest perpendicular to gondola front-axle beam and the gondola back rest, trailing edge rib is connected on rear side of the gondola back rest perpendicular to the gondola back rest, nose ribs, stage casing rib, trailing edge rib in one plane forms water-drop-shaped structure, nose ribs outside face is covered with skins front edges, stage casing rib upper and lower surface is covered with stage casing covering, trailing edge rib outside face is covered with trailing edge skin, skins front edges, stage casing covering, trailing edge skin is connected with wing rounding off by wing-gondola fairing.
An embodiment of port wing gondola is shown in Fig. 2, is fixed covering 210, coil hatch cover 211, gondola central sill 212, attachment angle 213, bumper 214, receiving coil 215 etc. formed by gondola front-axle beam 201, the gondola back rest 202, nose ribs 203, stage casing rib 204, trailing edge rib 205, wing-gondola fairing 206, skins front edges 207, stage casing covering 208, trailing edge skin 209, coil cabin.
Gondola front-axle beam 201 glueds joint with nose ribs 203, stage casing rib 204 and uses rivet interlacement, the gondola back rest 202 glueds joint with trailing edge rib 205, stage casing rib 204 and uses rivet interlacement, more than form the structural framework of gondola, wherein gondola front-axle beam 201, the gondola back rest 202, stage casing rib 204 are as primary load bearing box section, bear and transmit Main Load.Skins front edges 207, stage casing covering 208, trailing edge skin 209 are used for covered structure skeleton, provide rectification profile, and beam, glued joint between rib cage fixing.Coil cabin is fixed covering 210 and is gluedd joint with gondola front-axle beam 201, the gondola back rest 202, for coil cabin provides rectification profile; Coil hatch cover 211 is similarly coil cabin and provides rectification profile, installs as coil, the passage of dismounting simultaneously, fixes covering 210, gondola front-axle beam 201, the gondola back rest 202 be connected by screw, for removably connecting with coil cabin.Receiving coil 215 is fixed on gondola front-axle beam 201, the gondola back rest 202 and gondola central sill 212, uses bolt to connect, conveniently can install, dismantles and debug.Wing-gondola fairing 206 provides rectification profile for the outer hanging joint of wing and gondola and wing join domain, its one end is fixed on skins front edges 207, stage casing covering 208 and trailing edge skin 209, the other end is fixed on wing, uses screw to connect, convenient installation, dismounting.
The installation of transmitter coil: transmitter coil 304 is arranged in starboard wing equipment pod (covering 110 is fixed in coil cabin and coil hatch cover 111 is not shown), be connected with gondola front-axle beam 301 and the back rest 302 by its reaction plate 303, use bolt 305 to be connected and fixed, see Fig. 3.
The installation of receiving coil: receiving coil is arranged in port wing equipment pod (covering 210 is fixed in coil cabin and coil hatch cover 211 is not shown), be connected with bumper 404 outer ring by its reaction plate 406, be connected with attachment angle 408 in the middle part of bumper, then attachment angle 408 and connecting panel 409 respectively with gondola front-axle beam 401, central sill 402 and the back rest 403 connect, thus realize the connection of coil and gondola beam, more than connect and all use bolt 407 to fix, by elastomeric material in the middle part of bumper 404, bumper 404 can realize the damping on bolt axis direction (vertical direction), thus ensure coil working requirement, see Fig. 4.
The layout of equipment pod and mounting means: the left and right wing of aircraft respectively installs an equipment pod, wherein transmitter coil gondola 501 is arranged on starboard wing wing tip place, and receiving coil gondola 502 is arranged on port wing wing tip place, sees Fig. 5.Equipment pod is bolted with Front wing spar joint 602, rear beam splice 603 respectively by its front-axle beam 604, the back rest 605, when gondola is installed, wing-gondola fairing 606 need be slided along gondola exhibition on covering, expose the forward and backward beam splice of wing and the forward and backward beam of gondola, ensure that gondola has enough installing spaces, after gondola is installed, fixed wing-gondola fairing 606, it is connected and fixed by screw and wing 601 and gondola covering, sees Fig. 6.
Claims (2)
1. an airborne geophysical prospecting equipment props up extension structure for pod, it is characterized in that, comprise: two is be semi-cylindrical coil hatch cover in the middle of half cone-shaped, two is fix covering for semi-cylindrical coil cabin in the middle of half cone-shaped, be respectively pincerlike gondola front-axle beam and the gondola back rest, covering is fixed in coil hatch cover and coil cabin, and to synthesize a two in the middle of conical be columniform housing, built-in transmitter coil, gondola front-axle beam is parallel with the gondola back rest and binding clip position is enclosed within transmitter coil, nose ribs are connected on front side of gondola front-axle beam perpendicular to gondola front-axle beam, stage casing rib is connected between gondola front-axle beam and the gondola back rest perpendicular to gondola front-axle beam and the gondola back rest, trailing edge rib is connected on rear side of the gondola back rest perpendicular to the gondola back rest, nose ribs, stage casing rib, trailing edge rib in one plane forms water-drop-shaped structure, nose ribs outside face is covered with skins front edges, stage casing rib upper and lower surface is covered with stage casing covering, trailing edge rib outside face is covered with trailing edge skin, skins front edges, stage casing covering, trailing edge skin is connected with wing rounding off by wing-gondola fairing.
2. an airborne geophysical prospecting equipment props up extension structure for pod, it is characterized in that, comprise: two is be semi-cylindrical coil hatch cover in the middle of half cone-shaped, two is fix covering for semi-cylindrical coil cabin in the middle of half cone-shaped, be respectively pincerlike gondola front-axle beam and the gondola back rest, the gondola central sill of binding clip shape, covering is fixed in coil hatch cover and coil cabin, and to synthesize a two in the middle of conical be columniform housing, built-in receiving coil, gondola front-axle beam, gondola central sill is parallel with the gondola back rest and binding clip position is enclosed within receiving coil, gondola front-axle beam, gondola central sill and the gondola back rest are spirally connected with connecting panel respectively, connecting panel and angle section are spirally connected, angle section and bumper are spirally connected, coil reaction plate on bumper and receiving coil is spirally connected, nose ribs are connected on front side of gondola front-axle beam perpendicular to gondola front-axle beam, stage casing rib is connected between gondola front-axle beam and the gondola back rest perpendicular to gondola front-axle beam and the gondola back rest, trailing edge rib is connected on rear side of the gondola back rest perpendicular to the gondola back rest, nose ribs, stage casing rib, trailing edge rib in one plane forms water-drop-shaped structure, nose ribs outside face is covered with skins front edges, stage casing rib upper and lower surface is covered with stage casing covering, trailing edge rib outside face is covered with trailing edge skin, skins front edges, stage casing covering, trailing edge skin is connected with wing rounding off by wing-gondola fairing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210233027.6A CN103523240B (en) | 2012-07-06 | 2012-07-06 | Airborne geophysical prospecting equipment props up extension structure for pod |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210233027.6A CN103523240B (en) | 2012-07-06 | 2012-07-06 | Airborne geophysical prospecting equipment props up extension structure for pod |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103523240A CN103523240A (en) | 2014-01-22 |
| CN103523240B true CN103523240B (en) | 2015-10-28 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201210233027.6A Expired - Fee Related CN103523240B (en) | 2012-07-06 | 2012-07-06 | Airborne geophysical prospecting equipment props up extension structure for pod |
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Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107328319B (en) * | 2017-07-13 | 2019-04-19 | 江西洪都航空工业集团有限责任公司 | A kind of aircraft gun pod seat structure |
| CN109229418B (en) * | 2018-08-02 | 2021-07-16 | 哈尔滨飞机工业集团有限责任公司 | Installation method of wing hanging geophysical prospecting equipment nacelle |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3105934A (en) * | 1960-01-05 | 1963-10-01 | Selco Exploration Company Ltd | Method and apparatus for the remote detection of ore bodies utilizing pulses of short duration to induce transient polarization in the ore bodies |
| WO2006011893A1 (en) * | 2004-06-24 | 2006-02-02 | Barringer Anthony R | Remote sensing electric field exploration system |
| US7221164B1 (en) * | 2006-04-25 | 2007-05-22 | Barringer Anthony R | Airborne remote sensing electric field exploration system |
| CN101044416A (en) * | 2004-10-08 | 2007-09-26 | 菲格鲁空中勘测公司 | Unmanned airborne vehicle for geophysical surveying |
-
2012
- 2012-07-06 CN CN201210233027.6A patent/CN103523240B/en not_active Expired - Fee Related
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3105934A (en) * | 1960-01-05 | 1963-10-01 | Selco Exploration Company Ltd | Method and apparatus for the remote detection of ore bodies utilizing pulses of short duration to induce transient polarization in the ore bodies |
| WO2006011893A1 (en) * | 2004-06-24 | 2006-02-02 | Barringer Anthony R | Remote sensing electric field exploration system |
| CN101044416A (en) * | 2004-10-08 | 2007-09-26 | 菲格鲁空中勘测公司 | Unmanned airborne vehicle for geophysical surveying |
| US7221164B1 (en) * | 2006-04-25 | 2007-05-22 | Barringer Anthony R | Airborne remote sensing electric field exploration system |
Non-Patent Citations (3)
| Title |
|---|
| 墙内开花墙外香 中国支线客机的发展历程－运-12;老毕;《航空档案》;20100615;58-69 * |
| 我国频率域航空电磁法仪器系统研制回顾与展望;李文杰等;《物探化探计算技术》;20071015;第29卷;21-24 * |
| 航空物探技术在军事领域中的应用分析;王卫平等;《国家安全地球物理丛书（七）－地球物理与核探测》;20111101;199-204 * |
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| CN103523240A (en) | 2014-01-22 |
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