CN113665820A - Separable parachute system - Google Patents
Separable parachute system Download PDFInfo
- Publication number
- CN113665820A CN113665820A CN202111162404.7A CN202111162404A CN113665820A CN 113665820 A CN113665820 A CN 113665820A CN 202111162404 A CN202111162404 A CN 202111162404A CN 113665820 A CN113665820 A CN 113665820A
- Authority
- CN
- China
- Prior art keywords
- impact
- piece
- carrier
- bearing
- parachute
- 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
- 238000000926 separation method Methods 0.000 claims abstract description 21
- 238000012423 maintenance Methods 0.000 claims description 4
- 239000000843 powder Substances 0.000 claims 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract description 6
- 230000006872 improvement Effects 0.000 description 11
- 230000006698 induction Effects 0.000 description 5
- 239000003721 gunpowder Substances 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 239000000969 carrier Substances 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 241000251729 Elasmobranchii Species 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000003638 chemical reducing agent Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000003116 impacting effect Effects 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D17/00—Parachutes
- B64D17/22—Load suspension
- B64D17/38—Releasable fastening devices between parachute and load or pack
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Walking Sticks, Umbrellas, And Fans (AREA)
Abstract
The invention relates to the field of umbrella body devices, and discloses a separable parachute system, which comprises a parachute body and a bearing piece, wherein an umbrella cabin base is arranged at the bottom of the parachute body, a connecting piece is arranged between the bearing piece and the umbrella cabin base, and the connecting piece can realize the starting of a separating piece on the connecting piece through an impact sensing device arranged on the umbrella cabin base, so that the separation between the parachute body and the bearing piece is realized. The separable parachute system comprises a parachute cabin base, a bearing piece and a connecting piece, wherein the connecting piece is arranged between the parachute cabin base and the bearing piece, and the connecting piece is controlled to operate through impact on the bearing piece, so that the connecting piece is separated from the parachute cabin base or the bearing piece, the connecting piece can be started at the first time after the bearing piece falls to the ground or falls into water, a carrier on the bearing piece can be rapidly separated from a parachute body, and the subsequent working efficiency of the carrier is guaranteed.
Description
Technical Field
The invention relates to the field of umbrella body devices, in particular to a separable parachute system.
Background
The umbrella body is mainly a deployable aerodynamic reducer which is inflated and deployed relative to air movement by utilizing the principle of air resistance. The modern umbrella body is an aviation tool which enables people or objects to safely fall from the air to the ground.
In the process of landing a person or an object, a worker can manually separate the umbrella body from the person after the worker safely lands, and then the worker can conveniently perform subsequent work and tasks. However, after most materials or tools and the like fall, people can only wait for the tools at fixed points to fetch the tools, and with the continuous development of the existing robots and intelligent equipment technologies, the intelligent equipment often has greatly reduced working efficiency due to the obstruction of the umbrella body and the like after falling.
The intelligent parachute system is characterized in that operations such as exploration or transportation are required after the existing intelligent device and other carriers land, in the prior art, a releasing module with the parachute body is usually added in the intelligent device, and the intelligent device and the parachute body are disassembled through a remote control technology and the like.
Disclosure of Invention
In view of one or more of the above-identified deficiencies in the art or needs for improvement, the present invention provides a separable parachute system for achieving direct separation of a carrier from a parachute body after descent.
To achieve the above object, the present invention provides a separable parachute system comprising:
the parachute body is used for decelerating and landing of the carrier, and a parachute cabin base is arranged at the bottom of the parachute body;
the bearing part is used for bearing or placing the carrier;
the connecting piece is arranged between the umbrella cabin base and the bearing piece and is used for connecting the umbrella cabin base and the bearing piece;
the bottom of the bearing piece is also provided with an impact sensing device which is used for sensing external impact on the bearing piece and transmitting an impact signal to the connecting piece;
the connecting piece is provided with a separating piece corresponding to the impact sensing device, the separating piece is electrically connected with the impact sensing device and used for receiving an impact signal and driving the connecting piece to be separated from the bearing piece or the umbrella cabin base
As a further improvement of the invention, the connecting piece comprises a connecting seat connected with the bearing piece and an impact plate connected with the umbrella cabin base, and the impact plate is detachably connected with the connecting seat;
the connecting seat is provided with an impact groove, the separating piece is arranged in the impact groove, and the separating piece can move along the direction of the impact groove after receiving an impact signal and impact on the impact plate so as to realize the separation of the impact plate and the connecting seat.
As a further improvement of the invention, the connecting piece comprises a connecting seat connected with the umbrella cabin base, an impact groove is formed in the connecting seat, the separating piece is arranged in the impact groove, one end of the separating piece extends out of a notch of the impact groove and is detachably connected with the bearing piece and can move towards a direction departing from the bearing piece after receiving an impact signal, so that the separating piece and the bearing piece are separated
As a further improvement of the present invention, the separating element includes an impact assembly disposed along the direction of the impact slot, a power assembly is disposed circumferentially on the impact assembly, and the power assembly is electrically connected to the impact sensing device and is configured to receive an impact signal from the impact sensing device and push the impact assembly to move in a direction away from the bearing element.
As a further improvement of the invention, the impact assembly comprises an impact column and an impact circular table arranged along the radial direction of the impact column, and the impact circular table is used for bearing the impact force of the power assembly so as to drive the impact column to move.
As a further improvement of the invention, the power component is an electric control gunpowder.
As a further improvement of the present invention, the impact sensing device includes an inductor connected to an outer surface of the bearing member and a power controller disposed in the bearing member, the power controller is electrically connected to the power assembly, and the power controller is configured to receive impact sensing of the inductor and control start and stop of the power assembly.
As a further improvement of the invention, the connecting seat is connected with the impact plate through a screw structure.
As a further improvement of the invention, the carrier is one of a transport, a survey, a repair or a torpedo.
As a further improvement of the invention, the method comprises the following steps:
the umbrella body is used for the deceleration landing of the carrier, and the bottom of the umbrella body is provided with an umbrella cabin base connected with the outer part;
the carrier is placed in the carrier, the carrier is arranged in the carrier in an openable and closable manner, and a connecting piece is arranged at an opening of the carrier;
the bottom of the bearing piece is also provided with an impact sensing device which is used for sensing external impact on the bearing piece and transmitting an impact signal to the connecting piece;
the connecting piece is provided with a separating piece corresponding to the impact sensing device, the separating piece is electrically connected with the impact sensing device and used for receiving an impact signal and realizing the opening and closing of the bearing piece so as to discharge the carrier in the bearing from the opening and closing position.
The above-described improved technical features may be combined with each other as long as they do not conflict with each other.
Generally, compared with the prior art, the above technical solution conceived by the present invention has the following beneficial effects:
(1) according to the separable parachute system, the connecting piece is arranged between the parachute body and the bearing piece, the impact induction is transmitted through the impact induction device on the bearing piece, and the separation between the connecting piece and the parachute body or the bearing piece is realized through the impact induction, so that when the bearing piece falls to the ground or the water surface, the separation between the parachute body and the bearing piece is realized through instant impact force, the carrier on the bearing piece can freely move after falling, and the separable parachute system is not limited by the resistance of falling.
(2) According to the separable parachute system, after external impact is sensed, the impact signal is transmitted to the power assembly through the impact sensing device, the power assembly is controlled to push the impact assembly to move, the impact plate is impacted through the impact assembly, the impact plate is separated from the connecting seat, the separation of the parachute body and the bearing piece is further achieved, the structure of the whole connecting piece is simple, the motion mode of the impact assembly and the power assembly is simple, the stable separation of the parachute body and the bearing piece can be guaranteed, and the separable parachute system can adapt to various complex environments.
(3) According to the separable parachute system, after external impact is sensed, the impact signal is transmitted to the power assembly through the impact sensing device, the power assembly is controlled to push the impact assembly to move, the separation from the bearing piece is achieved through the movement of the impact assembly, and then the separation of the parachute body and the bearing piece is achieved.
(4) According to the separable parachute system, after external impact is sensed, the impact signal is transmitted to the connecting piece, and the opening and closing of the opening of the bearing piece are realized through the connecting piece, so that the carrier in the bearing piece is separated from the parachute system, and the subsequent transportation and autonomous work of the carrier are facilitated.
(5) The separable parachute system has a simple integral structure, the connection mode and the separation mode between the parachute body and the bearing piece are simple and reliable, and the bearing piece and the parachute body can be quickly separated at the moment when the bearing piece is impacted externally.
Drawings
FIG. 1 is a schematic view showing the overall construction of a separable parachute system in accordance with an embodiment of the present invention;
FIG. 2 is a schematic view of an embodiment of the present invention with the umbrella body separated from the carrier;
FIG. 3 is a schematic view of a connector structure according to an embodiment of the present invention;
FIG. 4 is a schematic view of the connection member separated from the carrier member according to one embodiment of the present invention;
FIG. 5 is a schematic view of a connector structure according to one embodiment of the present invention;
FIG. 6 is a schematic view of the connection piece being separated from the base of the canopy in one embodiment of the present invention;
fig. 7 is a schematic view of a separator according to an embodiment of the present invention.
In all the figures, the same reference numerals denote the same features, in particular:
1. an umbrella body; 2. an umbrella cabin base; 3. a carrier; 4. a connecting member; 5. an impact sensing device; 6. a separating member;
401. a connecting seat; 402. an impact plate; 403. an impact groove;
601. an impact column; 602. impacting the circular truncated cone; 603. and a power assembly.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention is described in further detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention. In addition, the technical features involved in the embodiments of the present invention described below may be combined with each other as long as they do not conflict with each other.
In the description of the present invention, it is to be understood that the terms "central," "longitudinal," "lateral," "length," "width," "thickness," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," "clockwise," "counterclockwise," "axial," "radial," "circumferential," and the like are used in the orientations and positional relationships indicated in the drawings for convenience in describing the invention and to simplify the description, and are not intended to indicate or imply that the referenced devices or elements must have a particular orientation, be constructed and operated in a particular orientation, and are therefore not to be considered limiting of the invention.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one such feature. In the description of the present invention, "a plurality" means at least two, e.g., two, three, etc., unless specifically limited otherwise.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," "secured," and the like are to be construed broadly and can, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; they may be directly connected or indirectly connected through intervening media, or they may be connected internally or in any other suitable relationship, unless expressly stated otherwise. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.
In the present invention, unless otherwise expressly stated or limited, the first feature "on" or "under" the second feature may be directly contacting the first and second features or indirectly contacting the first and second features through an intermediate. Also, a first feature "on," "over," and "above" a second feature may be directly or diagonally above the second feature, or may simply indicate that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature may be directly under or obliquely under the first feature, or may simply mean that the first feature is at a lesser elevation than the second feature.
Example (b):
the separable parachute system in the preferred embodiment of the present invention, as shown in fig. 1 to 7, comprises a parachute body 1 for carrier deceleration landing, and a parachute bay base 2 is provided at the bottom of the parachute body 1; the umbrella cabin base 3 is used for bearing or placing the carrier, a connecting piece 4 is used for connecting the umbrella cabin base 2 with the carrier 3, the connecting piece 4 is used for connecting the umbrella cabin base 2 with the carrier 3, separation between the umbrella cabin base 2 and the carrier 3 can be realized, an impact sensing device 5 is further arranged at the bottom of the carrier 3 and used for sensing external impact applied to the carrier 3 and transmitting an impact signal to the connecting piece 4, a separating piece 6 is further arranged on the connecting piece 4 corresponding to the impact sensing device 5, the separating piece 6 is electrically connected with the impact sensing device 5 and used for receiving the impact signal and realizing separation between the connecting piece 4 and the carrier 3 or the umbrella cabin base 2.
According to the invention, the connecting piece 4 structure is arranged between the umbrella body 1 and the bearing piece 3, and the impact sensing device 5 linked with the connecting piece 4 is arranged on the bearing piece 3, so that when the bearing piece 3 is impacted, an impact signal is fed back to the connecting piece 4, and the separation from the bearing piece 3 or the umbrella cabin base 2 is realized through the connecting piece 4. The whole separable parachute system is simple in structure, the separation mode between the parachute body 1 and the bearing part 3 is simple and clear, the parachute can respond at the first time and complete separation, remote control is not needed, various complex environments can be adapted, and the problem that remote control is inconvenient and the like under severe weather or no-signal environments is avoided.
As shown in fig. 1 and 2, in the application of the present invention, the umbrella chamber base 2 is used for not only reliably connecting the umbrella body 1 and the bearing member 3 and ensuring the deceleration of the bearing member 3 in high altitude, but also placing the umbrella body 1, and a space for accommodating the umbrella body 1 in a stacked state is reserved on the upper portion of the umbrella chamber base 2, so as to facilitate the carrying and recovery of the umbrella body 1. The top of the umbrella body 1 is also provided with a traction wire head for opening the umbrella body 1. The carrier in this application mainly refers to the intelligent machine carrier that possesses certain storage function, explores function, maintenance function, can carry out corresponding goods and materials transportation, ground exploration or ground maintenance etc. when going into water or descending ground, and in actual conditions, the carrier also can realize multiple functions such as goods and materials transportation, exploration or maintenance simultaneously. Of course, the functions that other robot carriers or fixed-point throwing bodies such as torpedoes and the like can complete can be completed through the carrier in the application.
As a preferred embodiment of the present invention, as shown in fig. 5 and 6, the connecting member 4 is mainly used for connecting with the umbrella chamber base 2, and comprises a connecting seat 401 and an impact plate 402, wherein the connecting seat 401 is connected with the bearing member 3, the impact plate 402 is connected with the umbrella chamber base 2, and the impact plate 402 is detachably connected with the connecting seat 401; an impact groove 403 is further formed on the connecting socket 401, the separating member 6 is disposed in the impact groove 403, and the separating member 6 can move along the opening direction of the impact groove 403 and impact on the impact plate 402 after receiving an impact signal, so as to separate the impact plate 402 from the connecting socket 401. Impact plate 402 and connecting seat 401 adopt detachable mode to be connected between, and when separator 6 in the impact groove 403 on connecting seat 401 impacted impact plate 402, impact plate 402 and connecting seat 401 separated from each other, and then realized the separation of umbrella cabin base 2 and carrier 3.
Preferably, the connection mode between the impact plate 402 and the connection seat 401 is not unique, a screw structure, a mortise and tenon structure, a thread fit structure and the like can be adopted between the impact plate 402 and the connection seat 401, the detachable structure is only used for ensuring the reliable connection between the impact plate 402 and the connection seat 401 in the descending process, and the impact of the separating piece 6 can be reliably separated, namely, the structure which has certain firmness but is not completely fixedly connected can be adopted.
Further, as an alternative embodiment of the present invention, as shown in fig. 3 and 4, the connecting member 4 includes a connecting seat 401 connected to the umbrella chamber base 2, the connecting seat 401 has an impact groove 403, the separating member 6 is disposed in the impact groove 403, and one end of the separating member 6 extends out of the notch of the impact groove 403 and is detachably connected to the supporting member 3, and can move away from the supporting member 3 after receiving an impact signal, so as to separate the separating member 6 from the supporting member 3. The detachable connection between the separating piece 6 and the bearing piece 3, when the separating piece 6 moves in the direction departing from the bearing piece 3 in the impact groove 403, the end of the bearing piece 3 is abutted against the notch of the impact groove 403, the separating piece 6 continues to move, the separating piece 6 and the bearing piece 3 are separated, and the separation of the bearing piece 3 and the umbrella cabin base 2 is realized.
Further, as a preferred embodiment of the present invention, the separating element 6 specifically includes an impact assembly disposed along the opening direction of the impact slot 403, the impact assembly is circumferentially provided with a power assembly 603, and the power assembly 603 is electrically connected to the impact sensing device 5, and is configured to receive an impact signal from the impact sensing device 5 and push the impact assembly to move in a direction away from the bearing element 3. Preferably, the impact assembly comprises an impact column 601 and an impact round table 602 arranged along the radial direction of the impact column 601, wherein the impact round table 602 is used for bearing the impact force of the power assembly 603 so as to drive the impact column 601 to move. When the outside of the bearing piece 3 is impacted, the impact sensing device 5 sends an impact signal to the power assembly 603, the power assembly 603 starts and axially transmits power along the impact groove 403, the power assembly 603 abuts against the impact circular truncated cone 602 and drives the impact assembly to move, the impact column 601 impacts the impact plate 402 to separate the impact plate 402 from the connecting seat 401, or the impact column 601 moves towards the direction departing from the bearing piece 3, the part of the impact column 601, which extends out of the impact groove 403, is received in the impact groove 403, the impact column 601 is separated from the bearing piece 3, and the bearing piece 3 is separated from the separating piece 6, as shown in fig. 7.
Further, as a preferred embodiment of the present invention, the power assembly 603 in the present application may be an electrically controlled telescopic structure, such as an electrically controlled motor or an air cylinder, or may also be an initiation structure such as an electrically controlled gunpowder, and the electrically controlled gunpowder may be started at the moment when the bearing member 3 is impacted, and has a large pushing force, so as to realize separation from the bearing member 3 or the umbrella cabin base 2 instantly, and ensure stable operation of the bearing member after falling to the ground. The carrier 3 in this application can set up with the carrier is integrative, and the carrier 3 itself is a part of carrier promptly, also can set up carrier 3 and carrier components of a whole that can function independently, and the carrier is placed on carrier 3 promptly, can change according to actual operational environment demand etc..
Further, as a preferred embodiment of the present invention, the impact sensing device 5 includes a sensor connected to an outer surface of the supporting member 3 and a power controller disposed in the supporting member 3, and the power controller is electrically connected to the power assembly 603 and is configured to receive an impact sensing of the sensor and control the start and stop of the power assembly 603. In order to ensure that the connecting piece 4 is separated from the bearing piece 3 or the umbrella cabin base 2 after the bearing piece 3 is impacted, the inductor structure of the impact induction device 5 needs to be connected with the outer surface of the bearing piece 3, the induction range of the inductor is preferably arranged at the bottom of the bearing piece 3 or around the bottom of the bearing piece 3, so that the bottom or the peripheral edge of the bearing piece 3 can immediately transmit an impact signal to the power controller when falling to the ground or falling into water, and then the power controller drives the power assembly 603 to move, so that the separation of the connecting piece 4 from the bearing piece 3 or the umbrella cabin base 2 is realized.
Further, as an optional embodiment of the present invention, the carrier 3 in the present application is openable, the carrier is accommodated inside the carrier 3, and a connecting member 4 is disposed at an opening and closing position of the carrier 3; the connecting piece 4 is also provided with a separating piece 6 corresponding to the impact sensing device 5, the structure of the separating piece 6 is the same as that of the embodiment, the difference is that the separating piece 6 is used for detachably connecting two sides of the opening of the bearing piece 3, when the bearing piece 3 falls to the ground or falls into water, the impact sensing device 5 transmits an impact signal to the connecting piece 4, the separating piece 6 on the connecting piece 4 is started, the bearing piece 3 is unfolded from the opening to two sides, and a carrier positioned in the bearing piece 3 can be smoothly discharged from the opening.
Separable parachute system in this application, through set up connecting piece 4 between parachute cabin base 2 and carrier 3, and through the 4 functions of impact control connecting piece that carrier 3 received, realize connecting piece 4 and parachute cabin base 2 or the separation that carries carrier 3, ensure to carry carrier 3 and fall to the ground or fall into water the back, connecting piece 4 can start the very first time, ensure to carry the carrier on 3 and can break away from with 1 part of the umbrella body rapidly, guarantee the follow-up work rate of carrier.
It will be understood by those skilled in the art that the foregoing is only a preferred embodiment of the present invention, and is not intended to limit the invention, and that any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the scope of the present invention.
Claims (10)
1. A separable parachute system, comprising:
the parachute body is used for decelerating and landing of the carrier, and a parachute cabin base is arranged at the bottom of the parachute body;
the bearing part is used for bearing or placing the carrier;
the connecting piece is arranged between the umbrella cabin base and the bearing piece and is used for connecting the umbrella cabin base and the bearing piece;
the bottom of the bearing piece is also provided with an impact sensing device which is used for sensing external impact on the bearing piece and transmitting an impact signal to the connecting piece;
the connecting piece is provided with a separating piece corresponding to the impact sensing device, and the separating piece is electrically connected with the impact sensing device and used for receiving an impact signal and driving the connecting piece to be separated from the bearing piece or the umbrella cabin base.
2. A detachable parachute system according to claim 1,
the connecting piece comprises a connecting seat connected with the bearing piece and an impact plate connected with the umbrella cabin base, and the impact plate is detachably connected with the connecting seat;
the connecting seat is provided with an impact groove, the separating piece is arranged in the impact groove, the notch of the impact groove is aligned with the impact plate, and the separating piece can move along the direction of the impact groove after receiving an impact signal and impact on the impact plate so as to realize the separation of the impact plate and the connecting seat.
3. The separable parachute system of claim 1, wherein the connecting member comprises a connecting seat connected to the parachute bay base, the connecting seat is provided with an impact groove, the separating member is disposed in the impact groove, one end of the separating member extends out of a notch of the impact groove and is detachably connected to the bearing member, and the separating member can move in a direction away from the direction of the bearing member after receiving an impact signal, so that the separating member is separated from the bearing member.
4. A separable parachute system according to claim 2 or 3, wherein the separating member includes an impact member disposed along the direction of opening the impact groove, and a power member is disposed circumferentially on the impact member and electrically connected to the impact sensing device, for receiving an impact signal from the impact sensing device and driving the impact member to move in a direction away from the carrier.
5. The detachable parachute system of claim 4, wherein the impact assembly comprises an impact post and an impact truncated cone disposed radially along the impact post, the impact truncated cone configured to receive an impact force of the power assembly to move the impact post.
6. A detachable parachute system according to claim 4, wherein the power unit is an electrically controlled powder.
7. The detachable parachute system of claim 4, wherein the impact sensing device comprises a sensor coupled to an outer surface of the carrier and a power controller disposed within the carrier, the power controller being electrically coupled to the power assembly, the power controller being configured to receive an impact from the sensor and control the power assembly to start or stop.
8. A detachable parachute system according to claim 2, wherein the connection base and the impact plate are connected by a screw structure.
9. A detachable parachute system according to claim 1, wherein the carrier is one of a transport, a survey, a maintenance or a torpedo.
10. A separable parachute system, comprising:
the umbrella body is used for the deceleration landing of the carrier, and the bottom of the umbrella body is provided with an umbrella cabin base connected with the outer part;
the carrier is placed in the carrier, the carrier is arranged in the carrier in an openable and closable manner, and a connecting piece is arranged at an opening and closing position of the carrier;
the bottom of the bearing piece is also provided with an impact sensing device which is used for sensing external impact on the bearing piece and transmitting an impact signal to the connecting piece;
the connecting piece is provided with a separating piece corresponding to the impact sensing device, the separating piece is electrically connected with the impact sensing device and used for receiving an impact signal and realizing the opening and closing of the bearing piece so as to discharge the carrier in the bearing from the opening and closing position.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111162404.7A CN113665820A (en) | 2021-09-30 | 2021-09-30 | Separable parachute system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111162404.7A CN113665820A (en) | 2021-09-30 | 2021-09-30 | Separable parachute system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN113665820A true CN113665820A (en) | 2021-11-19 |
Family
ID=78550510
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202111162404.7A Pending CN113665820A (en) | 2021-09-30 | 2021-09-30 | Separable parachute system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN113665820A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117699015A (en) * | 2023-12-14 | 2024-03-15 | 崂山国家实验室 | Umbrella releasing device and control method thereof |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB588507A (en) * | 1945-02-26 | 1947-05-27 | Daniel Waumsley Cooper | Improvements in or relating to automatic release-links for parachute-borne loads |
| GB603431A (en) * | 1944-10-26 | 1948-06-16 | Leonard Arthur Pollard | Impact release gear |
| DE3308177A1 (en) * | 1983-03-08 | 1984-09-20 | Autoflug Gmbh, 2084 Rellingen | ARRANGEMENT FOR DISCONNECTING A LOAD FROM A HARNESS |
| JP2004099001A (en) * | 2002-09-11 | 2004-04-02 | Kanto Koku Keiki Kk | Signal processing method for aerial delivery device |
| CN104943865A (en) * | 2015-07-12 | 2015-09-30 | 北京理工大学 | Automatic separation mechanism for full-mechanical miniature throwing robot and parachute |
| CN109747806A (en) * | 2018-12-10 | 2019-05-14 | 储锋 | A kind of airplane catapult system |
| CN210364381U (en) * | 2019-07-02 | 2020-04-21 | 詹恭强 | Security protection unmanned aerial vehicle |
| CN113428368A (en) * | 2021-06-28 | 2021-09-24 | 广东汇天航空航天科技有限公司 | Parachute device and flight device |
| CN215851907U (en) * | 2021-09-30 | 2022-02-18 | 襄阳宏伟航空器有限责任公司 | Separable parachute system |
-
2021
- 2021-09-30 CN CN202111162404.7A patent/CN113665820A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB603431A (en) * | 1944-10-26 | 1948-06-16 | Leonard Arthur Pollard | Impact release gear |
| GB588507A (en) * | 1945-02-26 | 1947-05-27 | Daniel Waumsley Cooper | Improvements in or relating to automatic release-links for parachute-borne loads |
| DE3308177A1 (en) * | 1983-03-08 | 1984-09-20 | Autoflug Gmbh, 2084 Rellingen | ARRANGEMENT FOR DISCONNECTING A LOAD FROM A HARNESS |
| JP2004099001A (en) * | 2002-09-11 | 2004-04-02 | Kanto Koku Keiki Kk | Signal processing method for aerial delivery device |
| CN104943865A (en) * | 2015-07-12 | 2015-09-30 | 北京理工大学 | Automatic separation mechanism for full-mechanical miniature throwing robot and parachute |
| CN109747806A (en) * | 2018-12-10 | 2019-05-14 | 储锋 | A kind of airplane catapult system |
| CN210364381U (en) * | 2019-07-02 | 2020-04-21 | 詹恭强 | Security protection unmanned aerial vehicle |
| CN113428368A (en) * | 2021-06-28 | 2021-09-24 | 广东汇天航空航天科技有限公司 | Parachute device and flight device |
| CN215851907U (en) * | 2021-09-30 | 2022-02-18 | 襄阳宏伟航空器有限责任公司 | Separable parachute system |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117699015A (en) * | 2023-12-14 | 2024-03-15 | 崂山国家实验室 | Umbrella releasing device and control method thereof |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| RU2756702C2 (en) | Cargo delivery system and method | |
| JP7386822B2 (en) | Air launch and/or recovery for unmanned aerial vehicles and related systems and methods | |
| CN110709322B (en) | Flying body and method for controlling flying body | |
| KR102067358B1 (en) | Drone attachable mission apparatus and system thereof | |
| KR101720028B1 (en) | Wireless power charging apparatus for unmanned aerial vehicle | |
| KR101792555B1 (en) | Unmanned drones automatic charging and containment system | |
| US7946530B1 (en) | Modular adaptive configured helicopter | |
| CN215851907U (en) | Separable parachute system | |
| JP2018513056A (en) | Aerial delivery assembly | |
| KR20200013352A (en) | The active guided docking station and a combined vehicle for automatically landing the drones at the docking station | |
| CN113665820A (en) | Separable parachute system | |
| US10894593B2 (en) | UAV with frangible airframe structures | |
| CN102910288A (en) | Multifunctional unmanned aerial vehicle provided with flexible stamping parafoil | |
| KR102263343B1 (en) | Drone attachable mission apparatus using moving pin and system thereof | |
| CN113184225B (en) | Fixed-point recovery system and method for ballistic reentry satellite re-entry capsule | |
| KR20160063917A (en) | Unmanned-flight reconnaissance system | |
| EP2738093B1 (en) | Method of landing of a surveillance unmanned aerial vehicle and and a surveillance unmanned aerial vehicle | |
| KR102643162B1 (en) | Intelligent drone charging station using a one-handed drone | |
| US20170144759A1 (en) | Plug-and-play multifunctional attachment of remote control rotorcraft | |
| CN220391518U (en) | Automatic loading and unloading unmanned aerial vehicle | |
| CN111994309B (en) | Auxiliary recovery system for carrier rocket recovery | |
| CN216030845U (en) | Intelligent detection type robot dog | |
| CN212148450U (en) | Unmanned aerial vehicle recovery system | |
| KR101220990B1 (en) | Power supply system of electric aircraft using rotating power supply line | |
| CN108082410A (en) | Small drone airplane parking area waterborne |
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 |