CN104118572A - Fast installation plate - Google Patents

Fast installation plate Download PDF

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Publication number
CN104118572A
CN104118572A CN201410387282.5A CN201410387282A CN104118572A CN 104118572 A CN104118572 A CN 104118572A CN 201410387282 A CN201410387282 A CN 201410387282A CN 104118572 A CN104118572 A CN 104118572A
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CN
China
Prior art keywords
disc
top bottom
fast installation
closed position
radius
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Granted
Application number
CN201410387282.5A
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Chinese (zh)
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CN104118572B (en
Inventor
伍小图
吴奇文
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
GUANGZHOU KEYI PHOTO-ELECTRIC TECHNOLOGY Co Ltd
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GUANGZHOU KEYI PHOTO-ELECTRIC TECHNOLOGY Co Ltd
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Application filed by GUANGZHOU KEYI PHOTO-ELECTRIC TECHNOLOGY Co Ltd filed Critical GUANGZHOU KEYI PHOTO-ELECTRIC TECHNOLOGY Co Ltd
Priority to CN201410387282.5A priority Critical patent/CN104118572B/en
Publication of CN104118572A publication Critical patent/CN104118572A/en
Application granted granted Critical
Publication of CN104118572B publication Critical patent/CN104118572B/en
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Abstract

The invention discloses a fast installation plate. The fast installation plate comprises an upper bottom plate used for being installed on a helicopter hanger, a lower bottom plate used for being installed on a nacelle, and a locking structure used for locking the upper bottom plate and the lower bottom plate. An installation portion used for installing the lower bottom plate in a rotation mode is arranged on the periphery edge of the upper bottom plate and comprises a disassembly position and a fastening position. The lower bottom plate is provided with a fastener. The fastener rotates to the fastening position along the disassembly position, so that the lower bottom plate is connected to the upper bottom plate in a fastening mode. According to the fast installation plate, lifting the nacelle manually is avoided, screw holes of the upper bottom plate and the lower bottom plate can be aligned easily, and the helicopter electricity inspection nacelle connected with the lower bottom plate can be installed on the helicopter hanger connected with the upper bottom plate fast.

Description

Fast Installation dish
Technical field
The present invention relates to a kind of electric inspection process technical field, especially a kind of Fast Installation dish that gondola is arranged on to helicopter hanger.
Background technology
At present, electric inspection process more and more adopts helicopter to carry out Daily Round Check to electric power circuit, the image collecting device of Power Line Inspection System is housed in the gondola of helicopter, gondola is manually lifted in the many employings of installation of itself and helicopter, with the human eye aligning screw of gondola and the screw of helicopter hanger, install screwing additional, make it to be arranged in the hanging of helicopter, this method takes time and effort.
Summary of the invention
Task of the present invention is to provide a kind of Fast Installation dish, can easily be quick installed at helicopter hanger for the gondola that makes helicopter in electric inspection process.
The present invention realizes by following technical proposals:
Fast Installation dish, is characterized in that: comprises for being arranged on top bottom-disc on helicopter hanger, for being arranged on the low bottom-disc on gondola, and by the locking mechanism of top bottom-disc and low bottom-disc locking; Top bottom-disc circumferential edges is provided with the installation position of low bottom-disc being installed for rotating, and installation position comprises removed position and closed position, and low bottom-disc is provided with buckling piece, and buckling piece rotates to closed position along removed position, and low bottom-disc is fastened and connected on top bottom-disc.
The further improvement project of the present invention comprises:
The radius of described removed position is less than the radius of described closed position; The end of described buckling piece is radially provided with a protrusion, and the apical position of protrusion is in the radial direction between removed position and closed position;
The radius of removed position is the distance of the top bottom-disc center of circle to removed position;
The radius of closed position is the distance of the top bottom-disc center of circle to closed position.
The radius of described closed position is less than the radius of described top bottom-disc; The root position of described buckling piece is radially between closed position and position, top bottom-disc edge;
The radius of top bottom-disc refers to the distance of the top bottom-disc center of circle to top bottom-disc edge.
Described locking mechanism comprises screw and the screw coordinating with it, and screw is separately positioned on the described top bottom-disc position corresponding with described low bottom-disc.
Described top bottom-disc is provided with lug boss, has for screw and reinforce the fixing threaded hole on helicopter hanger on lug boss, and fixing threaded hole is laid along even circumferential; The hanging screw of the corresponding a kind of type of six one group of above-mentioned fixing threaded hole also has the hanging screw of the corresponding another kind of type of quaternate fixing threaded hole simultaneously on lug boss.
Described top bottom-disc is provided with groove along circumference, and this groove makes the space of described lug boss and described low bottom-disc composition be communicated with outside.
Described top bottom-disc and described low bottom-disc are provided with locating notch.
Described buckling piece is detachable on described low bottom-disc.
Between described removed position and closed position, be provided with an arc portion.
Described top bottom-disc comprises at least two installation positions, and described low bottom-disc comprises at least two buckling pieces, and the quantity of installation position and position are corresponding with buckling piece.
Advantage of the present invention:
(1) application of Fast Installation dish of the present invention can buckle the buckling piece of the low bottom-disc that connects gondola to hang over aircraft to hang on the top bottom-disc being connected straight, has exempted manually lifting gondola and aiming at the screw of helicopter hanger, then in screw, has reinforced screw.
(2) top bottom-disc circumference of the present invention is provided with groove, and this groove makes the space of described lug boss and described low bottom-disc composition be communicated with outside, and rainwater can go out by this concentrated flow, prevents rain erosion reinforcing screw.
(3) top bottom-disc lug boss of the present invention has six one group and quaternate fixing threaded hole simultaneously, the hanging screw of its respectively corresponding two kinds of different type of machines, and commonality is good.
Brief description of the drawings
Fig. 1 is not-connected status figure of the present invention;
Fig. 2 is coupled condition figure of the present invention.
Wherein: 1-top bottom-disc, 101a-removed position, 101b-closed position, 102-top bottom-disc edge, 103-lug boss, 104-screw, 105-fixing threaded hole, 106-groove, 107-arc portion, 2-low bottom-disc, 3-buckling piece, 31-protrusion, 32-apical position, 33-root, 4-locating notch.
Detailed description of the invention
Below in conjunction with accompanying drawing, Fast Installation of the present invention is further described:
Fast Installation dish comprises for being arranged on top bottom-disc 1 on helicopter hanger, for being arranged on the low bottom-disc 2 on gondola, and the locking mechanism that top bottom-disc 1 and low bottom-disc 2 are locked; Top bottom-disc 1 circumferential edges is provided with the installation position of low bottom-disc 2 being installed for rotating, installation position comprises removed position 101a and closed position 101b, low bottom-disc 2 is provided with buckling piece 3, and buckling piece 3 rotates to closed position 101b along removed position 101a, and low bottom-disc 2 is fastened and connected on top bottom-disc 1.
The radius of removed position is less than the radius of closed position, the end of buckling piece 3 is radially provided with a protrusion 31, the apical position 32 of protrusion 31 is in the radial direction between removed position 101a and closed position 101b, while making the buckling piece 3 of low bottom-disc 2 insert removed position 101a, protrusion 31 has enough spaces to enter removed position 101a, when buckling piece 3 rotate to time when closed position 101b, protrusion 31 has overlapping part with the radius of closed position, this overlapping part plays low bottom-disc 2 buttons and hangs over the position-limiting action on top bottom-disc 1, thereby the gondola that low bottom-disc 2 connects is linked together with the helicopter hanger being connected with top bottom-disc 1,
The radius of removed position is the distance of the top bottom-disc center of circle to removed position 101a;
The radius of closed position is the distance of the top bottom-disc center of circle to closed position 101b.
Preferably, the radius of closed position is less than the radius of top bottom-disc; Root 33 positions of buckling piece, radially between closed position 101b and 102 positions, top bottom-disc edge, make the buckling piece 3 of low bottom-disc 2 in the time of closed position 101b, and top bottom-disc edge 102 plays spacing effect to the root 33 of buckling piece on hand of rotation;
The radius of top bottom-disc refers to the distance of the top bottom-disc center of circle to top bottom-disc edge 102.
Top bottom-disc 1 and low bottom-disc 2 are provided with locating notch 4.
Locking mechanism comprises screw 104 and the screw coordinating with it, and screw 104 is separately positioned on top bottom-disc 1 and the corresponding position of low bottom-disc 2.
In rotary course, because the apical position 32 of buckling piece 3 is radially between removed position 101a and closed position 101b, the buckling piece 3 of low bottom-disc 2 inserts from removed position 101a, while rotating to closed position 101b, protrusion 31 is withheld on top bottom-disc 1 under gondola Action of Gravity Field, again the locating notch of low bottom-disc 24 rotation is adjusted to when consistent with the locating notch 4 of top bottom-disc, the screw 104 that is arranged on top bottom-disc 1 and low bottom-disc 2 is corresponding on corresponding position, be now that available screw is through top bottom-disc 1 screw 104 corresponding with low bottom-disc 2, and locking top bottom-disc 1 and low bottom-disc 2.The present invention has avoided manually lifting gondola, can easily aim at the screw 104 of top bottom-disc 1 and low bottom-disc 2, fast the helicopter in electric inspection process gondola being connected with low bottom-disc 2 is arranged on the helicopter hanger being connected with top bottom-disc 1.
Preferably, between removed position 101a and closed position 101b, be provided with an arc portion 107, make to connect the low bottom-disc installation or removal smoothness of gondola.
Top bottom-disc 1 is provided with lug boss 103, has for screw and reinforce the fixing threaded hole 105 on helicopter hanger on lug boss 103, and fixing threaded hole 105 is laid along even circumferential; The hanging screw of the corresponding a kind of type of 105 6 one group of above-mentioned fixing threaded hole also has the hanging screw of quaternate fixing threaded hole 105 corresponding another kind of types simultaneously on lug boss 103, make the commonality of Fast Installation dish good.
Top bottom-disc 1 is provided with groove 106 along circumference, and groove 106 makes the space that lug boss 103 and low bottom-disc 2 form be communicated with outside, and rainwater can flow out by groove 106, prevents that rain erosion from reinforcing screw, prolongation gondola service life.
Buckling piece 3 is detachable on low bottom-disc 2, facilitates processing and manufacturing.
Top bottom-disc 1 comprises at least two installation positions, and low bottom-disc 2 comprises at least two buckling pieces 3, and the quantity of installation position and position are corresponding with buckling piece 3.
The present invention is not limited to above-mentioned detailed description of the invention, and the further expansion that those of ordinary skill in the art makes according to the present invention all falls into protection scope of the present invention.

Claims (10)

1. Fast Installation dish, is characterized in that: comprises for being arranged on top bottom-disc on helicopter hanger, for being arranged on the low bottom-disc on gondola, and by the locking mechanism of top bottom-disc and low bottom-disc locking; Top bottom-disc circumferential edges is provided with the installation position of low bottom-disc being installed for rotating, and installation position comprises removed position and closed position, and low bottom-disc is provided with buckling piece, and buckling piece rotates to closed position along removed position, and low bottom-disc is fastened and connected on top bottom-disc.
2. Fast Installation dish according to claim 1, is characterized in that: the radius of described removed position is less than the radius of described closed position; The end of described buckling piece is radially provided with a protrusion, and the apical position of protrusion is in the radial direction between removed position and closed position;
The radius of removed position is the distance of the top bottom-disc center of circle to removed position;
The radius of closed position is the distance of the top bottom-disc center of circle to closed position.
3. Fast Installation dish according to claim 2, is characterized in that: the radius of described closed position is less than the radius of described top bottom-disc; The root position of described buckling piece is radially between closed position and position, top bottom-disc edge;
The radius of top bottom-disc refers to the distance of the top bottom-disc center of circle to top bottom-disc edge.
4. Fast Installation dish according to claim 1, is characterized in that: described locking mechanism comprises screw and the screw coordinating with it, and screw is separately positioned on the described top bottom-disc position corresponding with described low bottom-disc.
5. Fast Installation dish according to claim 1, is characterized in that: described top bottom-disc is provided with lug boss, has for screw and reinforce the fixing threaded hole on helicopter hanger on lug boss, and fixing threaded hole is laid along even circumferential; The hanging screw of the corresponding a kind of type of six one group of above-mentioned fixing threaded hole also has the hanging screw of the corresponding another kind of type of quaternate fixing threaded hole simultaneously on lug boss.
6. Fast Installation dish according to claim 5, is characterized in that: described top bottom-disc is provided with groove along circumference, and this groove makes the space of described lug boss and described low bottom-disc composition be communicated with outside.
7. according to the arbitrary Fast Installation dish described in claim 1-6, it is characterized in that: described top bottom-disc and described low bottom-disc are provided with locating notch.
8. according to the arbitrary Fast Installation dish described in claim 1-6, it is characterized in that: described buckling piece is detachable on described low bottom-disc.
9. according to the arbitrary Fast Installation dish described in claim 1-6, it is characterized in that: between described removed position and closed position, be provided with an arc portion.
10. Fast Installation dish according to claim 1, is characterized in that: described top bottom-disc comprises at least two installation positions, described low bottom-disc comprises at least two buckling pieces, and the quantity of installation position and position are corresponding with buckling piece.
CN201410387282.5A 2014-08-08 2014-08-08 Fast Installation disk Active CN104118572B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410387282.5A CN104118572B (en) 2014-08-08 2014-08-08 Fast Installation disk

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410387282.5A CN104118572B (en) 2014-08-08 2014-08-08 Fast Installation disk

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CN104118572A true CN104118572A (en) 2014-10-29
CN104118572B CN104118572B (en) 2017-03-29

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106672251A (en) * 2016-12-06 2017-05-17 中国航空工业集团公司成都飞机设计研究所 Installing structure of optoelectronic pod
CN108910067A (en) * 2018-08-21 2018-11-30 北京量子星光科技有限公司 Aerial survey gondola and aircraft
CN109649669A (en) * 2018-12-26 2019-04-19 成都优艾维智能科技有限责任公司 A rotatory auto-lock probe connection structure for unmanned aerial vehicle
CN112412933A (en) * 2019-08-23 2021-02-26 金恩斯智能装备(天津)有限公司 Mechanical arm mounting disc of automatic tool lifting mechanism

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201365012Y (en) * 2009-02-27 2009-12-16 李玉刚 Safe power socket
US20100027281A1 (en) * 2008-07-31 2010-02-04 Waters Stanley E LED Anti-Collision Light for Commercial Aircraft
CN102036858A (en) * 2008-05-21 2011-04-27 芦森工业株式会社 Airbag cover and airbag device
CN103659311A (en) * 2012-09-14 2014-03-26 深圳富泰宏精密工业有限公司 Fixing assembly
CN203707530U (en) * 2013-07-09 2014-07-09 古河电气工业株式会社 Rotary connector
CN204037917U (en) * 2014-08-08 2014-12-24 广州科易光电技术有限公司 Fast Installation dish

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102036858A (en) * 2008-05-21 2011-04-27 芦森工业株式会社 Airbag cover and airbag device
US20100027281A1 (en) * 2008-07-31 2010-02-04 Waters Stanley E LED Anti-Collision Light for Commercial Aircraft
CN201365012Y (en) * 2009-02-27 2009-12-16 李玉刚 Safe power socket
CN103659311A (en) * 2012-09-14 2014-03-26 深圳富泰宏精密工业有限公司 Fixing assembly
CN203707530U (en) * 2013-07-09 2014-07-09 古河电气工业株式会社 Rotary connector
CN204037917U (en) * 2014-08-08 2014-12-24 广州科易光电技术有限公司 Fast Installation dish

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106672251A (en) * 2016-12-06 2017-05-17 中国航空工业集团公司成都飞机设计研究所 Installing structure of optoelectronic pod
CN108910067A (en) * 2018-08-21 2018-11-30 北京量子星光科技有限公司 Aerial survey gondola and aircraft
CN109649669A (en) * 2018-12-26 2019-04-19 成都优艾维智能科技有限责任公司 A rotatory auto-lock probe connection structure for unmanned aerial vehicle
CN112412933A (en) * 2019-08-23 2021-02-26 金恩斯智能装备(天津)有限公司 Mechanical arm mounting disc of automatic tool lifting mechanism

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Denomination of invention: Quick installation disk

Effective date of registration: 20210604

Granted publication date: 20170329

Pledgee: Development Zone sub branch of Bank of Guangzhou Co.,Ltd.

Pledgor: GUANGZHOU KEII ELECTRO OPTICS TECHNOLOGY Co.,Ltd.

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Date of cancellation: 20220721

Granted publication date: 20170329

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Denomination of invention: Quick installation disk

Effective date of registration: 20230324

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Pledgor: GUANGZHOU KEII ELECTRO OPTICS TECHNOLOGY Co.,Ltd.

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