CN114038358A - Automatic draw and take off slogan canning - Google Patents
Automatic draw and take off slogan canning Download PDFInfo
- Publication number
- CN114038358A CN114038358A CN202111382200.4A CN202111382200A CN114038358A CN 114038358 A CN114038358 A CN 114038358A CN 202111382200 A CN202111382200 A CN 202111382200A CN 114038358 A CN114038358 A CN 114038358A
- Authority
- CN
- China
- Prior art keywords
- sheath
- slogan
- friction block
- counterweight
- sheath body
- 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.)
- Granted
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Classifications
-
- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09F—DISPLAYING; ADVERTISING; SIGNS; LABELS OR NAME-PLATES; SEALS
- G09F17/00—Flags; Banners; Mountings therefor
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- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09F—DISPLAYING; ADVERTISING; SIGNS; LABELS OR NAME-PLATES; SEALS
- G09F21/00—Mobile visual advertising
- G09F21/06—Mobile visual advertising by aeroplanes, airships, balloons, or kites
- G09F21/12—Mobile visual advertising by aeroplanes, airships, balloons, or kites the advertising matter being towed by the aircraft
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Abstract
The invention provides an automatic pull-off slogan sheath, which comprises: the sheath comprises a sheath body (1), a sheath balance weight (2), a slogan balance weight (3) and an upper end friction block (4); the upper-end friction block (4) is connected to the outer hanging device of the helicopter, the bottom of the upper-end friction block is connected with the slogan, and the bottom of the slogan is connected with the slogan counterweight (3); the sheath body (1) wraps the upper end friction block (4), the folded slogan and the slogan counterweight (3), and the sheath counterweight (2) is arranged at the bottom of the sheath body (1); the friction force between the sheath body (1) and the upper-end friction block (4) is greater than the gravity of the sheath body (1) and less than the gravity of the sheath body (1) and the sheath counterweight (2). The problem that the slogan can not be pulled off or wound by sticking the slogan by the magic tape in the existing slogan sheath is solved by the sheath capable of automatically loosening and releasing when the helicopter is lifted and the corresponding balancing weight.
Description
Technical Field
The invention belongs to the aviation technology, and particularly relates to an automatic pull-off slogan sheath.
Background
When the helicopter is used for hanging the large-format slogan, the slogan is wrapped by the sheath and pulled off when the slogan balancing weight is lifted off in order to prevent the slogan from being wound under the action of the rotor wing downwash before taking off and in the taking off process. Whether the sheath is pulled off successfully or not is the key for displaying whether the flight is successful or not by hanging the slogan, and if the sheath is pulled off unsuccessfully, the flight safety is possibly influenced.
The present slogan canning is the magic and pastes the straining design, is connected with on slogan canning upper portion and draws and takes off the rope, and when the helicopter hoisted the balancing weight, the frictional force between slogan and the slogan canning drove the slogan canning and also was drawn, need draw from the rear at this moment and draw and take off the rope and make the magic subsides separation and draw the canning and take off. The current sheath design all has the requirement to pulling off opportunity and position, and pulls off power great, needs many people to cooperate, occasionally has the sheath to pull off or the magic subsides both ends to be blown open in advance and lead to the winding phenomenon of slogan when the in-service use.
Disclosure of Invention
The invention provides an automatic pull-off slogan sheath, which can be automatically released when a helicopter is lifted and a corresponding balancing weight thereof, and solves the problem that the existing slogan sheath is stuck by a magic tape and has the risk that a slogan cannot be pulled off or wound.
The invention provides an automatic pull-off slogan sheath, which comprises: the jacket comprises a jacket body 1, a jacket counterweight 2, a slogan counterweight 3 and an upper end friction block 4; wherein the content of the first and second substances,
the top of the upper-end friction block 4 is connected to an external hanging device of the helicopter through a hook, the bottom of the upper-end friction block is connected with an upper-end steel cable of the slogan through the hook, and the top of the slogan counterweight 3 is connected with a lower-end steel cable of the slogan through the hook;
the sheath body 1 wraps the upper end friction block 4, the folded slogan and the slogan counterweight 3, the sheath counterweight 2 is arranged at the bottom of the sheath body 1, and the bottom of the sheath body 1 and the sheath counterweight 2 are placed on the ground;
the friction force between the sheath body 1 and the upper end friction block 4 is larger than the gravity of the sheath body 1, the sheath body 1 is driven to lift when the slogan is lifted by the helicopter, the friction force is smaller than the gravity of the sheath body 1 and the sheath counter weight 2, and the sheath counter weight 2 is used for separating the sheath body 1 from the upper end friction block 4, the folded slogan and the slogan counter weight 3 when the sheath body 1 is completely straightened by the helicopter and continuously ascends.
Optionally, the sheath body 1 is strip-shaped, two side edges along the length direction are provided with zippers, and the zipper is cylindrical after being pulled up.
Optionally, the zipper is a split zipper.
Optionally, the bottom of the sheath body 1 is provided with an opening, and the sheath counterweight 2 is hung on the opening through a hook.
Optionally, friction lines are arranged on the surface of the upper end friction block 4, which is in contact with the jacket body 1.
Optionally, a magic tape is arranged between the upper end friction block 4 and the sheath body 1;
the rough surface of the magic tape is arranged on the upper end friction block 4, and the soft surface of the magic tape is arranged on the top of the sheath body 1, so that the sheath body 1 is prevented from damaging the slogan.
Optionally, the sheath weight 2 is at least one weight sandbag;
optionally, the bottom of the sheath body 1 is provided with a containing cavity for containing the counterweight sandbag.
Optionally, a rubber strip is arranged on the side edge of the upper portion of the sheath body 1, the sheath body 1 is in a ring shape after being pulled up by a zipper, and is in contact with the upper end friction block 4, so that the friction force between the sheath body 1 and the upper end friction block 4 is increased, and the sheath body 1 is pulled up.
The invention provides an automatic pull-off slogan sheath, which comprises: the jacket comprises a jacket body 1, a jacket counterweight 2, a slogan counterweight 3 and an upper end friction block 4; the upper end friction block 4 is connected to the outer hanging device of the helicopter, the bottom of the upper end friction block is connected with the slogan, and the bottom of the slogan is connected with the slogan counterweight 3; the sheath body 1 is wrapped by the upper end friction block 4, the folded slogan and the slogan counterweight 3, and the sheath counterweight 2 is arranged at the bottom of the sheath body 1; the friction force between the sheath body 1 and the upper end friction block 4 is larger than the gravity of the sheath body 1, the sheath body 1 is driven to lift when the helicopter lifts the slogan, the friction force is smaller than the gravity of the sheath body 1 and the sheath balance weight 2, and the sheath balance weight 2 is used for separating the sheath body 1 from the upper end friction block 4, the folded slogan and the slogan balance weight 3 when the helicopter completely straightens the sheath body 1 and continues to lift. The automatic pull-off slogan sheath provided by the invention can realize automatic pull-off, can effectively avoid sheath pull-off loss and sheath early opening accidents, saves the labor required for pulling off the sheath, and reduces the potential safety hazard of an outfield.
Drawings
FIG. 1 is a schematic structural view of an automatic pull-off banner jacket according to the present invention;
description of reference numerals:
1-a sheath body;
2-sheath counterweight;
3-balance weight of slogan;
4-upper friction block.
Detailed Description
The following explains the automatic pull-off slogan jacket provided by the present invention with reference to the accompanying drawings.
Fig. 1 is a schematic structural diagram of an automatic pull-off banner jacket according to the present invention, and as shown in fig. 1, the present invention provides an automatic pull-off banner jacket, including: the jacket comprises a jacket body 1, a jacket counterweight 2, a slogan counterweight 3 and an upper end friction block 4.
Illustratively, the sheath body 1 is of a strip-shaped structure, the lower end of the sheath body is provided with a plurality of openings, the sheath body is made of canvas or jean, and sectional zippers are arranged on two sides of the sheath body;
the sheath counterweight 2 is a cylinder poured by cement, and a hook is buried and exposed out of the upper part of the hook;
the slogan counterweight 3 is a cylinder cast by metal, and the material can be selected from high-density metal such as steel or tungsten alloy according to the task condition;
the upper end friction block 4 is made of rubber and is cut into a cylinder;
optionally, the lower end of the sheath body 1 can be sewn with a sandbag accommodating cavity;
optionally, a rubber strip can be additionally attached to the upper end of the sheath body 1; the attached rubber strip is parallel to the short edge of the sheath body 1, and the rubber strip is annular after the zipper of the sheath body 1 is closed;
optionally, in a possible embodiment, the slogan weight 3 is designed to be a cylinder, and the diameter of the cylinder is slightly smaller than that of the sheath body 1, and the length of the cylinder can be designed according to the weight requirement, and lead can be injected or a tungsten alloy material can be adopted as necessary.
Optionally, the sheath counterweight 2 can also be a sand bag, and when the sheath counterweight 2 is the sand bag, the sheath body 1 needs to sew a sand bag accommodating cavity at the lower end;
the upper end friction block 4 is arranged, so that the gravity of the pulled part of the sheath is borne by the upper end friction block instead of the slogan before the sheath is detached, the diameter of the sheath can be randomly set within a certain limit, and meanwhile, the abrasion of the slogan is reduced; the maximum static friction force (depending on the diameter of the friction block) of the upper-end friction block 4 and the sheath body 1 is greater than the gravity of the sheath body 1 and less than the sum of the gravity of the sheath body 1 and the sheath counter weight 2, so that the sudden change of the hanging load outside the helicopter is too large when the slogan sheath is pulled off, the maximum static friction force of the friction block only needs to be slightly greater than the gravity of the sheath body, and a magic tape can be arranged between the friction block and the sheath to adjust the friction force when necessary.
The invention adopts the slogan automatic pull-off design, can effectively avoid sheath pull-off loss and sheath early opening accidents, saves the labor required for pulling off the sheath and reduces the potential safety hazard of an outfield.
The sizes of the parts in fig. 1 need to be determined according to actual tasks, and the order of size determination is as follows: determining the weight of the slogan counterweight according to the length of the slogan, determining the lower limit of the diameter of the sheath according to the width of the slogan, determining the diameter, the length and the material of the slogan counterweight according to the diameter of the sheath, determining the length of the sheath according to the length of the slogan counterweight and the length of the slogan counterweight, determining the diameter of the upper friction block and whether a magic tape is added according to the mass of the sheath, and determining the weight of the sheath counterweight according to the maximum static friction force of the upper friction block.
Illustratively, the sizes of the parts are 5mx14m, the sheath body 1 is in a strip shape, the length is 17m, the width is 1.4m, and 4 circular holes with the diameter of 5cm are formed at the bottom; the sheath counterweight 2 is a cylinder poured by cement, the radius of the bottom surface is 20cm, the height is 40cm, and the hook is buried in the cement to expose the upper part of the hook; the mass of the slogan counterweight 3 is 500kg, the material is tungsten alloy, and the slogan counterweight is cast into a cylinder, the radius of the bottom surface of the cylinder is 20cm, and the height of the cylinder is 30 cm; the upper end friction block 4 is made of rubber and is cut into a cylinder, and the radius of the bottom surface of the cylinder is 23cm, and the height of the cylinder is 10 cm.
The invention can solve the problem that the sheath is difficult to pull off when the helicopter hangs the slogan display flight. After the friction block, the slogan, the sheath and the sheath counterweight are sequentially arranged, personnel can evacuate after the hook at the upper part of the friction block is connected with the helicopter hanging device, and the upper friction block and the slogan are pulled up after the helicopter takes off. Because the maximum static friction force between the upper end friction block and the inner surface of the slogan sheath is larger than the gravity of the sheath, the sheath is also pulled up. The helicopter continues to rise, when the slogan sheath is completely pulled up, the balance weight of the slogan sheath, which is originally offset by the ground support force, is gradually transferred to the friction block at the upper end, and when the maximum static friction force of the friction block is exceeded, the sheath is pulled off.
Claims (8)
1. An automatic pull-off banner packet, comprising: the sheath comprises a sheath body (1), a sheath balance weight (2), a slogan balance weight (3) and an upper end friction block (4); wherein the content of the first and second substances,
the top of the upper-end friction block (4) is connected to an external hanging device of the helicopter through a hook, the bottom of the upper-end friction block is connected with an upper-end steel cable of the slogan through the hook, and the top of the slogan counterweight (3) is connected with a lower-end steel cable of the slogan through the hook;
the sheath body (1) wraps the upper-end friction block (4), the folded slogan and the slogan counterweight (3), the sheath counterweight (2) is arranged at the bottom of the sheath body (1), and the bottom of the sheath body (1) and the sheath counterweight (2) are placed on the ground;
the sheath comprises a sheath body (1), an upper end friction block (4), a sheath counterweight (2), a sheath body (1) and a sheath counterweight (2), wherein the friction force between the sheath body (1) and the upper end friction block (4) is greater than the gravity of the sheath body (1), the sheath body is used for driving the sheath body (1) to lift when the slogan lifts, the friction force is smaller than the gravity of the sheath body (1) and the sheath counterweight (2), and the sheath body (1) is separated from the upper end friction block (4), the folded slogan and the slogan counterweight (3) when the helicopter completely straightens the sheath body (1) and continues to lift.
2. The placard jacket according to claim 1, characterized in that the jacket body (1) is long, and zippers are provided on both sides in the length direction, and the jacket body is cylindrical after being pulled up.
3. The banner wrap of claim 2, wherein the zipper is a segmented zipper.
4. The slogan sheath according to claim 2, characterized in that the bottom of the sheath body (1) is provided with an opening, and the sheath weight (2) is hung on the opening through a hook.
5. The slogan jacket according to claim 1, characterized in that the surface of the upper friction block (4) in contact with the jacket body (1) is provided with friction lines.
6. The slogan capsule according to claim 1, characterized in that a magic tape is arranged between the upper friction block (4) and the capsule body (1);
the rough surface of the magic tape is arranged on the upper end friction block (4), and the soft surface of the magic tape is arranged at the top of the sheath body (1) to prevent the sheath body (1) from damaging the slogan.
7. The placard jacket according to claim 1, wherein the jacket weight (2) is at least one weighted sandbag;
the bottom of the sheath body (1) is provided with a containing cavity for containing the counterweight sand bag.
8. The slogan jacket as claimed in claim 1, wherein the upper side edge of the jacket body (1) is provided with a rubber strip which is in a ring shape after the jacket body (1) is zipped up and is contacted with the upper end friction block (4) for increasing the friction force between the jacket body (1) and the upper end friction block (4) so as to zip up the jacket body (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111382200.4A CN114038358B (en) | 2021-11-19 | 2021-11-19 | Automatic pull-out slogan sheath |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111382200.4A CN114038358B (en) | 2021-11-19 | 2021-11-19 | Automatic pull-out slogan sheath |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN114038358A true CN114038358A (en) | 2022-02-11 |
| CN114038358B CN114038358B (en) | 2023-04-28 |
Family
ID=80138244
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202111382200.4A Active CN114038358B (en) | 2021-11-19 | 2021-11-19 | Automatic pull-out slogan sheath |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN114038358B (en) |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0999127A2 (en) * | 1998-11-02 | 2000-05-10 | Michael Konzok | Aerial towing device, in particular for aerial advertising display |
| JP2001260992A (en) * | 2000-03-22 | 2001-09-26 | Koyo:Kk | Airborne advertisement body |
| CN1394321A (en) * | 2000-01-13 | 2003-01-29 | 肖恩·帕特里克·赫伯特 | Emergency drop system for aircraft advertising display |
| ES2234400A1 (en) * | 2003-05-19 | 2005-06-16 | Publiski, S.L. | Safety transportation device for transporting placards in helicopter, has connector, electrical wiring, power supply battery, solenoid unit, piston rod and pawl system connected to counterbalance unit |
| CN1705968A (en) * | 2002-10-14 | 2005-12-07 | 格哈德·席曼茨 | Flag |
| BRMU8402115U (en) * | 2004-08-31 | 2006-04-25 | Fernando Carlos Da Silv Telles | inflatable banner layout for air show |
| US20110271567A1 (en) * | 2010-05-10 | 2011-11-10 | Butler James L | Aerial Advertising Device |
| CN104106108A (en) * | 2012-01-04 | 2014-10-15 | 帕布里维亚有限公司 | Aircraft banner |
| CN206789263U (en) * | 2017-02-22 | 2017-12-22 | 毛智樵 | Unmanned plane aerial display board |
-
2021
- 2021-11-19 CN CN202111382200.4A patent/CN114038358B/en active Active
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0999127A2 (en) * | 1998-11-02 | 2000-05-10 | Michael Konzok | Aerial towing device, in particular for aerial advertising display |
| CN1394321A (en) * | 2000-01-13 | 2003-01-29 | 肖恩·帕特里克·赫伯特 | Emergency drop system for aircraft advertising display |
| JP2001260992A (en) * | 2000-03-22 | 2001-09-26 | Koyo:Kk | Airborne advertisement body |
| CN1705968A (en) * | 2002-10-14 | 2005-12-07 | 格哈德·席曼茨 | Flag |
| ES2234400A1 (en) * | 2003-05-19 | 2005-06-16 | Publiski, S.L. | Safety transportation device for transporting placards in helicopter, has connector, electrical wiring, power supply battery, solenoid unit, piston rod and pawl system connected to counterbalance unit |
| BRMU8402115U (en) * | 2004-08-31 | 2006-04-25 | Fernando Carlos Da Silv Telles | inflatable banner layout for air show |
| US20110271567A1 (en) * | 2010-05-10 | 2011-11-10 | Butler James L | Aerial Advertising Device |
| CN104106108A (en) * | 2012-01-04 | 2014-10-15 | 帕布里维亚有限公司 | Aircraft banner |
| CN206789263U (en) * | 2017-02-22 | 2017-12-22 | 毛智樵 | Unmanned plane aerial display board |
Also Published As
| Publication number | Publication date |
|---|---|
| CN114038358B (en) | 2023-04-28 |
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