CN113942648A - Unmanned aerial vehicle throwing device and method of monitoring equipment - Google Patents
Unmanned aerial vehicle throwing device and method of monitoring equipment Download PDFInfo
- Publication number
- CN113942648A CN113942648A CN202111468425.1A CN202111468425A CN113942648A CN 113942648 A CN113942648 A CN 113942648A CN 202111468425 A CN202111468425 A CN 202111468425A CN 113942648 A CN113942648 A CN 113942648A
- Authority
- CN
- China
- Prior art keywords
- unmanned aerial
- aerial vehicle
- monitoring equipment
- limiting
- throwing device
- 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
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
- B64D1/12—Releasing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/60—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons
Abstract
The invention discloses an unmanned aerial vehicle throwing device of monitoring equipment, which comprises an unmanned aerial vehicle and monitoring equipment, wherein the unmanned aerial vehicle comprises a machine body, a rotary cylinder is arranged at the bottom of the machine body, a rotary end is arranged at the bottom of the rotary cylinder, hooks are arranged on two sides of the bottom end of the rotary end, inner fixing threads are arranged on the inner sides of the bottom ends of the hooks on two sides, the detection device comprises a detector, a fixed seat and a bottom plate, the detector is arranged at the center of the top of the fixed seat, the bottom plate is positioned under the fixed seat, outer fixing threads are arranged on the outer edge of the top end of the fixed seat, the hooks on two sides are in butt joint with the outer fixing threads arranged on the outer side of the fixed seat through the inner fixing threads, a limiting sleeve is arranged at the center of the bottom of the rotary cylinder, and a limiting insertion column is arranged at the center of the top of the detector. The unmanned aerial vehicle throwing device and the unmanned aerial vehicle throwing method for the monitoring equipment are stable in structure, free of clamping and stable in control.
Description
Technical Field
The invention relates to the field of unmanned aerial vehicle throwing, in particular to an unmanned aerial vehicle throwing device and method for monitoring equipment.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand the industrial application and develop the unmanned aerial vehicle technology.
But the phenomenon of blocking often appears in traditional unmanned aerial vehicle input mechanism, influences normal input operation.
Based on the above, the invention designs an unmanned aerial vehicle throwing device and method of monitoring equipment, so as to solve the problems.
Disclosure of Invention
The invention aims to provide an unmanned aerial vehicle throwing device and method for monitoring equipment, which are provided by the background technology.
In order to achieve the purpose, the invention provides the following technical scheme:
an unmanned aerial vehicle throwing device of monitoring equipment, which comprises a reconnaissance unmanned aerial vehicle and a monitoring device assembly and is characterized in that, the reconnaissance unmanned aerial vehicle comprises a machine body, wherein a rotary cylinder is arranged at the bottom of the machine body, a rotary end is arranged at the bottom of the rotary cylinder, hooks are arranged on both sides of the bottom end of the rotating end, internal fixing threads are arranged on the inner sides of the bottom ends of the hooks on both sides, the detection device comprises a detector, a fixed seat and a bottom plate, the detector is arranged in the center of the top of the fixed seat, the bottom plate is positioned under the fixed seat, the outer edge of the top end of the fixed seat is provided with an outer fixed thread, the hooks at two sides are in butt joint with the outer fixed thread arranged at the outer side of the fixed seat through the inner fixed thread, the center of the bottom of the rotary air cylinder is provided with a limiting sleeve, and the center of the top of the detector is provided with a limiting inserting column.
As a further scheme of the invention, the limit inserting column is clamped inside the limit sleeve when the monitoring equipment is integrally connected to the bottom end of the reconnaissance unmanned aerial vehicle.
As a further scheme of the invention, four limiting grooves are equidistantly arranged in the limiting sleeve, four limiting teeth are equidistantly arranged on the outer side of the limiting inserted column, and the four limiting teeth are slidably inserted into the four limiting grooves.
As a further scheme of the invention, a plurality of supports are arranged at the top end of the machine body, a propeller is arranged at one end of the outer side of each support, and a central processing unit is arranged in the machine body.
As a further scheme of the invention, a cushion pad is arranged in the center between the bottom of the fixed seat and the bottom plate, and a plurality of cushion springs are arranged around the bottom of the fixed seat and the bottom plate at equal intervals.
As a further scheme of the invention, four guide columns are equidistantly arranged on the periphery of the top of the bottom plate, and the four guide columns are respectively inserted into four guide holes arranged at the bottom of the fixed seat in a sliding manner.
As a further scheme of the invention, a plurality of support legs are equidistantly arranged at the bottom of the bottom plate.
As a further scheme of the invention, solar panels are arranged on two sides of the detector, and foot pads are arranged on the outer sides of the bottom ends of the hooks.
As a further scheme of the invention, firstly, a reconnaissance unmanned aerial vehicle carries out flight planning and throw point selection, the reconnaissance unmanned aerial vehicle carries out high-precision positioning navigation, after the place is selected, a central processing unit receives a command to start a rotary cylinder to drive a rotary end at the bottom end to rotate, and further drives hooks at two sides to rotate, at the moment, a limiting sleeve limits a limiting inserting column to not rotate, and then an internal fixing thread of each hook is separated from an external fixing thread on a fixing seat, so that the effect of releasing integration of detection equipment is achieved.
Compared with the prior art, the invention has the beneficial effects that:
(1) the unmanned aerial vehicle is firstly surveyed to carry out flight planning and throw point selection, the surveyed unmanned aerial vehicle carries out high-precision positioning navigation, the central processing unit receives a command to start the rotary cylinder to drive the rotary end at the bottom end to rotate after the place is selected, then the hooks at two sides are driven to rotate, the limiting insertion column is limited by the limiting sleeve pipe to not rotate, then the internal fixing threads of the hooks are separated from the external fixing threads on the fixing base, the effect of releasing the integration of the detection equipment is achieved, the structure is stable, the phenomenon of blocking cannot occur, and the control is more stable.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings used in the description of the embodiments will be briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art that other drawings can be obtained according to the drawings without creative efforts.
In the description of the present invention, it should be noted that the terms "top", "bottom", "one side", "the other side", "front", "back", "middle part", "inside", "top", "bottom", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of describing the present invention and simplifying the description, but do not indicate or imply that the referred device or element must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention; the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance; furthermore, unless expressly stated or limited otherwise, the terms "mounted," "connected," and "connected" are to be construed broadly, as they may be fixedly connected, detachably connected, or integrally connected, for example; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Fig. 1 is a schematic structural view of a reconnaissance drone of a drone throwing device of a monitoring device according to the invention;
fig. 2 is a schematic structural diagram of the monitoring equipment integration of the unmanned aerial vehicle throwing device of the monitoring device according to the invention;
fig. 3 is a schematic structural diagram of a limiting sleeve of an unmanned aerial vehicle throwing device of the monitoring equipment;
fig. 4 is a schematic structural diagram of a limiting inserting column of the unmanned aerial vehicle throwing device and the unmanned aerial vehicle throwing method of the monitoring equipment;
fig. 5 is a schematic diagram of the overall structure of the unmanned aerial vehicle throwing device of the monitoring equipment.
In the drawings, the components represented by the respective reference numerals are listed below:
1. surveying the unmanned aerial vehicle; 2. integrating monitoring equipment; 3. a body; 4. a rotating cylinder; 5. a rotating end; 6. hooking; 7. internal fixing threads; 8. a limiting sleeve; 9. a foot pad; 10. a support; 11. a propeller; 12. limiting and inserting the column; 13. a detector; 14. a fixed seat; 15. external fixing threads; 16. a base plate; 17. a cushion pad; 18. a guide hole; 19. a guide post; 20. a buffer spring; 21. a support leg; 22. a solar panel; 23. a limiting groove; 24. limiting teeth; 25. a central processing unit.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
As shown in fig. 1-4, the invention provides an unmanned aerial vehicle throwing device of a monitoring device, which comprises a surveying unmanned aerial vehicle 1 and a monitoring equipment assembly 2, and is characterized in that the surveying unmanned aerial vehicle 1 comprises a machine body 3, a rotating cylinder 4 is arranged at the bottom of the machine body 3, a rotating end 5 is arranged at the bottom of the rotating cylinder 4, hooks 6 are arranged on two sides of the bottom end of the rotating end 5, inner fixing threads 7 are arranged on the inner sides of the bottom ends of the hooks 6 on two sides, the detecting device 2 comprises a detector 13, a fixed seat 14 and a bottom plate 16, the detector 13 is arranged at the center of the top of the fixed seat 14, the bottom plate 16 is positioned under the fixed seat 14, outer fixing threads 15 are arranged on the outer side edge of the top end of the fixed seat 14, the hooks 6 on two sides are butted with the outer fixing threads 15 arranged on the outer side of the fixed seat 14 through the inner fixing threads 7, the center of the bottom of the rotary cylinder 4 is provided with a limiting sleeve 8, and the center of the top of the detector 13 is provided with a limiting inserting column 12.
Through the scheme of the invention, the limiting inserting column 12 is clamped in the limiting sleeve 8 when the monitoring equipment assembly 2 is butted with the bottom end of the unmanned reconnaissance plane 1.
Through the scheme of the invention, four limiting grooves 23 are equidistantly arranged in the limiting sleeve 8, four limiting teeth 24 are equidistantly arranged on the outer side of the limiting inserted column 12, and the four limiting teeth 24 are slidably inserted into the four limiting grooves 23.
Through the scheme of the invention, the top end of the machine body 1 is provided with a plurality of supports 10, one end of the outer side of each support 10 is provided with a propeller 11, and a central processing unit 25 is arranged in the machine body 1.
Through the scheme of the invention, the center between the bottom of the fixed seat 14 and the bottom plate 16 is provided with the cushion pad 17, and the periphery between the bottom of the fixed seat 14 and the bottom plate 16 is equidistantly provided with the plurality of cushion springs 20.
Through the scheme of the invention, four guide columns 19 are equidistantly arranged on the periphery of the top of the bottom plate 16, and the four guide columns 19 are respectively inserted into four guide holes 18 arranged at the bottom of the fixed seat 14 in a sliding manner.
With the above solution of the present invention, the bottom of the bottom plate 16 is provided with a plurality of support legs 21 at equal intervals.
Through the scheme of the invention, solar panels 22 are arranged on two sides of the detector 13, and the outside of the bottom end of the hook 6 is provided with the foot pad 9.
In practical application, at first reconnaissance unmanned aerial vehicle carries out flight planning and throws the throwing point and select, reconnaissance unmanned aerial vehicle carries out high accuracy location navigation, central processing unit received the order and starts the rotatory end that revolving cylinder drove the bottom and rotate after the place is selected, and then drive both sides couple and rotate, spacing post of inserting of spacing sleeve pipe restriction was not rotatory this moment, the internal fixation screw thread of couple breaks away from the external fixation screw thread on the fixing base afterwards, reach the integrated effect of release detection equipment, the phenomenon that blocks can not appear in stable structure, control is more stable.
It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.
Claims (9)
1. The utility model provides an unmanned aerial vehicle jettison device of monitoring facilities, equips integrated (2) including reconnaissance unmanned aerial vehicle (1) and monitoring, its characterized in that, reconnaissance unmanned aerial vehicle (1) includes organism (3), organism (3) bottom is provided with revolving cylinder (4), revolving cylinder (4) bottom is provided with rotatory end (5), rotatory end (5) bottom both sides all are provided with couple (6), both sides the inboard of couple (6) bottom all is provided with internal fixation screw thread (7), detection device (2) are including detector (13), fixing base (14) and bottom plate (16), detector (13) set up in fixing base (14) top center, bottom plate (16) are located under fixing base (14), fixing base (14) outside edge top is provided with external fixation screw thread (15), both sides couple (6) pass through internal fixation screw thread (7) dock in fixing base (14) outside edge (7) butt joint The device is characterized in that the external fixed thread (15) is arranged, a limiting sleeve (8) is arranged at the center of the bottom of the rotary cylinder (4), and a limiting insertion column (12) is arranged at the center of the top of the detector (13).
2. The unmanned aerial vehicle throwing device of monitoring equipment of claim 1, wherein the limiting insertion column (12) is clamped inside the limiting sleeve (8) when the monitoring equipment assembly (2) is butted against the bottom end of the reconnaissance unmanned aerial vehicle (1).
3. The unmanned aerial vehicle throwing device of monitoring equipment according to claim 2, wherein four limiting grooves (23) are equidistantly formed in the limiting sleeve (8), four limiting teeth (24) are equidistantly formed on the outer side of the limiting inserted column (12), and the four limiting teeth (24) are slidably inserted into the four limiting grooves (23).
4. The unmanned aerial vehicle throwing device of monitoring equipment according to claim 1, characterized in that a plurality of supports (10) are arranged on the top end of the machine body (1), a propeller (11) is arranged at one end of the outer side of each support (10), and a central processing unit (25) is arranged inside the machine body (1).
5. The unmanned aerial vehicle throwing device of monitoring equipment of claim 1, wherein a cushion pad (17) is arranged in the center between the bottom of the fixing seat (14) and the bottom plate (16), and a plurality of cushion springs (20) are arranged around the bottom of the fixing seat (14) and the bottom plate (16) at equal intervals.
6. The unmanned aerial vehicle throwing device of monitoring equipment of claim 5, characterized in that four guide posts (19) are equidistantly arranged around the top of the bottom plate (16), and the four guide posts (19) are respectively inserted into four guide holes (18) arranged at the bottom of the fixing base (14) in a sliding manner.
7. The unmanned aerial vehicle throwing device of monitoring equipment of claim 1, wherein the bottom of the base plate (16) is equidistantly provided with a plurality of feet (21).
8. The unmanned aerial vehicle throwing device of monitoring equipment of claim 1, characterized in that, the detector (13) both sides are provided with solar panel (22), the outside of couple (6) bottom is provided with the pad foot (9).
9. The unmanned aerial vehicle throwing method of monitoring equipment according to claim 1, characterized in that, firstly, the reconnaissance unmanned aerial vehicle (1) performs flight planning and throwing point selection, the reconnaissance unmanned aerial vehicle (1) performs high-precision positioning navigation, after the point selection, the central processing unit (25) receives a command to start the rotary cylinder (4) to drive the rotary end (5) at the bottom end to rotate, and then drives the hooks (6) at the two sides to rotate, at the moment, the limiting sleeve (8) limits the limiting insertion column (12) not to rotate, and then the internal fixed thread (7) of the hook (6) is separated from the external fixed thread (15) on the fixing seat (14), so as to achieve the effect of releasing the detection equipment assembly (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111468425.1A CN113942648A (en) | 2021-12-03 | 2021-12-03 | Unmanned aerial vehicle throwing device and method of monitoring equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111468425.1A CN113942648A (en) | 2021-12-03 | 2021-12-03 | Unmanned aerial vehicle throwing device and method of monitoring equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN113942648A true CN113942648A (en) | 2022-01-18 |
Family
ID=79338843
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202111468425.1A Pending CN113942648A (en) | 2021-12-03 | 2021-12-03 | Unmanned aerial vehicle throwing device and method of monitoring equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN113942648A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN210000591U (en) * | 2019-05-24 | 2020-01-31 | 河北润阔农业科技有限公司 | unmanned aerial vehicle rescue goods and materials throwing device |
| CN111038700A (en) * | 2020-01-06 | 2020-04-21 | 吉林省翼启飞科技有限公司 | Unmanned aerial vehicle carries automatic throwing device of formula |
| CN112478173A (en) * | 2020-12-01 | 2021-03-12 | 哈尔滨铭川运输有限公司 | Light package clamping and fixing device convenient for unmanned aerial vehicle transportation and using method |
| WO2021189167A1 (en) * | 2020-03-22 | 2021-09-30 | 南京唐壹信息科技有限公司 | Throwing-type unmanned aerial vehicle having cushioning support |
| CN214356690U (en) * | 2021-02-19 | 2021-10-08 | 广西一号农服航空科技有限公司 | Aerial goods hook formula unmanned aerial vehicle of jettisoninging |
| CN214397245U (en) * | 2021-01-12 | 2021-10-15 | 深圳市慧明捷科技有限公司 | A visual case of jettisoninging for unmanned aerial vehicle |
-
2021
- 2021-12-03 CN CN202111468425.1A patent/CN113942648A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN210000591U (en) * | 2019-05-24 | 2020-01-31 | 河北润阔农业科技有限公司 | unmanned aerial vehicle rescue goods and materials throwing device |
| CN111038700A (en) * | 2020-01-06 | 2020-04-21 | 吉林省翼启飞科技有限公司 | Unmanned aerial vehicle carries automatic throwing device of formula |
| WO2021189167A1 (en) * | 2020-03-22 | 2021-09-30 | 南京唐壹信息科技有限公司 | Throwing-type unmanned aerial vehicle having cushioning support |
| CN112478173A (en) * | 2020-12-01 | 2021-03-12 | 哈尔滨铭川运输有限公司 | Light package clamping and fixing device convenient for unmanned aerial vehicle transportation and using method |
| CN214397245U (en) * | 2021-01-12 | 2021-10-15 | 深圳市慧明捷科技有限公司 | A visual case of jettisoninging for unmanned aerial vehicle |
| CN214356690U (en) * | 2021-02-19 | 2021-10-08 | 广西一号农服航空科技有限公司 | Aerial goods hook formula unmanned aerial vehicle of jettisoninging |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP2013189036A (en) | Flying object for measuring | |
| CN107187587B (en) | A intelligent unmanned aerial vehicle for film and television aerial photography | |
| CN212074451U (en) | Can stabilize fixed laser radar's unmanned aerial vehicle support | |
| CN106516089A (en) | Unmanned aerial vehicle | |
| CN206407100U (en) | A kind of horn attachment structure and unmanned plane | |
| KR102110970B1 (en) | Preprocessing automation system using hyperspectral drone | |
| CN113942648A (en) | Unmanned aerial vehicle throwing device and method of monitoring equipment | |
| CN219524265U (en) | Laser range unit for unmanned aerial vehicle | |
| KR101665236B1 (en) | Multi rotor frame of unmanned vehicle and assembly method of the frame using the same | |
| Rawashdeh et al. | Microraptor: A low-cost autonomous quadrotor system | |
| CN205916345U (en) | Small -size fixed wing uavs launching cradle | |
| CN215043694U (en) | Middle and low altitude atmospheric environmental pollution source analysis environment monitoring unmanned aerial vehicle | |
| CN211001835U (en) | Unmanned aerial vehicle positioner that charges | |
| Walton et al. | Passive CubeSats for remote inspection of space vehicles | |
| CN212099341U (en) | Foldable many rotors rescue unmanned aerial vehicle | |
| CN211494496U (en) | Novel keep away barrier unmanned aerial vehicle | |
| CN214216152U (en) | Investigation type is alert with unmanned aerial vehicle | |
| Schairer et al. | Shape and Angle-of-Attack Measurements of Ram-Air Parachutes by Stereo Photogrammetry in the National Full-Scale Aerodynamics Complex | |
| CN106005467B (en) | A kind of small-sized fixed-wing unmanned aerial vehicle ejecting frame | |
| CN214377068U (en) | Teaching aid for unmanned aerial vehicle training | |
| Cunha et al. | ASSEMBLY OF A REMOTELY PILOTED AIRCRAFT OF LOW COST APPLIED TO AGRICULTURE | |
| CN213473511U (en) | Rotor fixing piece for unmanned aerial vehicle | |
| CN218786106U (en) | Non-deformable's unmanned aerial vehicle anticollision skeleton | |
| CN212899521U (en) | Unmanned aerial vehicle hangs damping device | |
| CN214729744U (en) | Oblique photogrammetry camera carrying device of unmanned aerial vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination |