CN113428368B - Parachute device and flight device - Google Patents
Parachute device and flight device Download PDFInfo
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- CN113428368B CN113428368B CN202110719403.1A CN202110719403A CN113428368B CN 113428368 B CN113428368 B CN 113428368B CN 202110719403 A CN202110719403 A CN 202110719403A CN 113428368 B CN113428368 B CN 113428368B
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- 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
- B64D17/80—Parachutes in association with aircraft, e.g. for braking thereof
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- 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
- B64D17/24—Rigging lines
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- 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
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- 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
- B64D17/62—Deployment
- B64D17/64—Deployment by extractor parachute
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- 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
- B64D17/62—Deployment
- B64D17/72—Deployment by explosive or inflatable means
- B64D17/725—Deployment by explosive or inflatable means by explosive means
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Abstract
The application discloses parachute device and flight device, the parachute device is applied to the flight device, the parachute device includes the parachute cabin, the parachute package, parachute throwing mechanism and controller, the parachute cabin includes parachute cabin main part and block, the parachute cabin main part is equipped with the umbrella mouth, the umbrella mouth is located to the block lid, parachute throwing mechanism is including connecting first parachute throwing ware and the second parachute throwing ware in the parachute cabin main part, first parachute throwing ware and second parachute throwing ware are used for acting on the separating force to the both sides of block respectively, controller and parachute throwing mechanism communication connection, the controller is configured to control parachute throwing mechanism in response to the parachute opening instruction and orders about the direction that the block was ordered about the umbrella mouth and break away from the umbrella mouth. The controller controls the first parachute throwing device and the second parachute throwing device to be opened in response to the parachute opening instruction, so that the two sides of the cover cap are acted by separating force, the cover cap is separated from the parachute outlet to pull out the parachute package quickly, the parachute of the parachute package is opened, when one of the parachute package is broken down, the parachute of the parachute package can still be opened, and safety is improved.
Description
Technical Field
The application relates to the technical field of flight and landing equipment, in particular to a parachute device and a flight device.
Background
The parachute device is widely applied to the parachute of flight devices, carries on the parachute device on the aircraft usually, is equipped with the parachute thrower in its parachute bay, and the parachute thrower pulls out the parachute in the parachute bay from the parachute bay after the circular telegram is detonated to realize the parachute-opening of parachute, because the aircraft device when taking place the accident, if when breaking down, the parachute thrower can't guarantee that the parachute can in time parachute-opening, reduced the security.
Disclosure of Invention
The application provides a parachute device and a flight device.
In a first aspect, an embodiment of the present application provides a parachute device, which is applied to a flight device, and includes a parachute bay, a parachute bag, a parachute throwing mechanism and a controller, wherein the parachute bay includes a parachute bay main body and a cap, the parachute bay main body is provided with a parachute outlet, the cap is arranged at the parachute outlet, and the parachute bag is accommodated in the parachute bay main body; the one end of parachute package is connected with the block through first parachute line, the other end passes through the second parachute line and is connected with the parachute cabin main part, parachute throwing mechanism is including connecting in the first parachute throwing ware and the second parachute throwing ware of parachute cabin main part, first parachute throwing ware and second parachute throwing ware are used for acting on the separating power to the both sides of block respectively, controller and parachute throwing mechanism communication connection, the controller is configured to control parachute throwing mechanism in response to the parachute opening instruction and orders about the block and break away from the parachute outlet towards the direction of keeping away from the parachute outlet, in order to pull out the parachute package in the parachute cabin main part.
In a second aspect, an embodiment of the present application provides a flying device, and the flying device is equipped with the parachute device.
The application provides a parachute device and flight device, the controller of parachute device is opening in response to the parachute opening instruction and control first parachute launcher and second parachute launcher for the both sides of block receive the effect of separating force, and the block breaks away from and pulls out the parachute package fast from the umbrella mouth, realizes the parachute-opening of parachute package, and when one of them broke down, parachute opening of parachute package still can be accomplished to parachute-throwing mechanism, has improved the security.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present application, the drawings required to be used in the description of the embodiments are briefly introduced below, and it is obvious that the drawings in the description below are only some embodiments of the present application, and it is obvious for those skilled in the art to obtain other drawings based on these drawings without creative efforts.
Fig. 1 shows a schematic structural diagram of a flying device provided by an embodiment of the present application.
Fig. 2 shows a schematic structural diagram of the parachute device provided by the embodiment of the application.
Figure 3 shows a schematic view of the parachute apparatus shown in figure 2 exploded when not opened.
Figure 4 shows an exploded view of the parachute assembly of figure 3 after opening.
Fig. 5 shows a plan view of the parachute bay body, the first parachute launcher and the second parachute launcher in the parachute apparatus shown in fig. 4 in an assembled state.
Figure 6 shows a schematic cross-sectional view of the parachute apparatus shown in figure 3.
Detailed Description
Reference will now be made in detail to embodiments of the present application, examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to the same or similar elements or elements having the same or similar functions throughout. The embodiments described below with reference to the accompanying drawings are exemplary only for explaining the present application and are not to be construed as limiting the present application.
The following disclosure provides many different embodiments or examples for implementing different features of the application. To simplify the disclosure of the present application, specific example components and arrangements are described below. Of course, they are merely examples and are not intended to limit the present application. Further, the present application may repeat reference numerals and/or reference letters in the various examples for simplicity and clarity and does not in itself dictate a relationship between the various embodiments and/or arrangements discussed.
Referring to fig. 1, an embodiment of the present application provides a flying device 200, where the flying device 200 may be a flying car, a flying backpack, an unmanned aerial vehicle, and the like, the flying device 200 is mounted with a parachute apparatus 100, and the parachute apparatus 100 may be disposed on the top of the flying device 200 for safe landing of the flying device 200. The following description will be given taking the flying device 200 as an example of a flying car:
referring to fig. 2 and 3, the parachute apparatus 100 includes a parachute bay 110, a parachute pack 120, a parachute throwing mechanism 130 and a controller 140, the parachute pack 120 is accommodated in the parachute bay 110, and the parachute throwing mechanism 130 is used for pulling the parachute pack 120 out of the parachute bay 110, so that the parachute pack 120 is opened in the sky. When the flying device 200 needs to be dropped, for example, when the flying device 200 malfunctions, the controller 140 of the parachute apparatus 100 controls the parachute throwing mechanism 130 to pull the parachute package 120 out of the parachute bay 110 in response to the parachute opening instruction, so that the parachute of the parachute package 120 is opened in the air. The parachute is a deployable aerodynamic speed reducer that is inflated and deployed with respect to the movement of air by using the principle of air resistance, and slows down the falling speed of the flying device 200 by means of the air resistance, so that the flying device 200 falls stably and safely at a low falling speed.
With continued reference to fig. 2 and 3, the umbrella chamber 110 includes a chamber body 111 and a cap 112, the chamber body 111 is provided with an umbrella outlet 1111, and the cap 112 is provided with the umbrella outlet 1111. In the present embodiment, the parachute bay main body 111 may have a hollow cylindrical structure, for example, a cylindrical structure having a circular cylindrical shape, a rectangular cylindrical shape, a rhombic cylindrical shape, or another shape, the parachute bay main body 111 is used to house the parachute pack 120, and the parachute in the parachute pack 120 disposed in the parachute bay main body 111 is in a collapsed state.
When the cap 112 receives the separating force from the parachute-throwing mechanism 130, the cap 112 can be separated from the parachute outlet 1111 in a direction away from the parachute outlet 1111 and rapidly pull out the parachute pack 120 from the parachute bay main body 111, enabling the parachute of the parachute pack 120 to be opened. The outer surface of the cap 112 is streamlined so that its resistance to air can be reduced. As an example, the outer surface of the cap 112 may be a cambered surface, such as a hemispherical surface or a conical surface, so that when the cap 112 is separated from the parachute outlet 1111 by a separating force during the parachute opening process of the parachute apparatus 100, the resistance generated between the cap 112 and the air is small, which can ensure that the cap 112 has a large separation speed, so that the cap 112 can rapidly pull the parachute pack 120 out of the parachute bay main body 111, thereby achieving the rapid parachute opening of the parachute pack 120.
In this embodiment, the parachute device 100 may further include a protection cabin 113, the parachute cabin 110 is disposed in the protection cabin 113, the cap 112 is movably covered on an outlet of the protection cabin 113 and covers the parachute outlet 1111 of the parachute cabin main body 111, and the cap 112 and the protection cabin 113 together form a part of an appearance surface of the parachute device 100. When the cap 112 is subjected to the separating force, the cap 112 is directly separated from the protection cabin 113. In this embodiment, the protection cabin 113 may be fixedly connected to the umbrella cabin main body 111, the protection cabin 113 is provided with a connection portion 1131 for connecting with the flight device 200, and the connection portion 1131 may be a connection structure such as a thread structure and a buckle. Illustratively, the protection cabin 113 may have a substantially cylindrical structure, the inner space of the protection cabin 113 may be adapted to the structure of the umbrella cabin 110, and the protection cabin 113 may be detachably connected to the umbrella cabin 110. By disposing the umbrella bay 110 in the protection bay 113, the umbrella bay body 111 and the electronic devices (e.g., a battery, a control board, etc.) disposed on the umbrella bay 110 can be protected from damage.
Referring to fig. 3 and 4, the parachute bag 120 is accommodated in the parachute bay main body 111, and one end of the parachute bag 120 is connected to the cap 112 through the first parachute cord 151 and the other end is connected to the parachute bay main body 111 through the second parachute cord 152. Specifically, in the present embodiment, the parachute pack 120 includes a guide parachute 121 and a main parachute 122, the main parachute 122 is connected to the parachute bay body 111 by a second parachute cord 152, the guide parachute 121 is connected to the top of the main parachute 122 by a first parachute cord 151, and the cap 112 is connected to the top of the guide parachute 121 by a third parachute cord 153.
In the present embodiment, the number of the first umbrella strings 151, the second umbrella strings 152, and the third umbrella strings 153 is plural. Specifically, a plurality of first umbrella strings 151 are disposed at intervals along the edge of the guide umbrella 121, one end of each first umbrella string 151 is connected to the edge of the guide umbrella 121, and the other end is connected to the top of the main umbrella 122, and the plurality of first umbrella strings 151 are located in substantially the same annular region. A plurality of second umbrella strings 152 are disposed at intervals along the edge of the main umbrella 122, one end of each second umbrella string 152 is connected to the edge of the main umbrella 122, the other end is connected to the umbrella cabin body 111, and the plurality of second umbrella strings 152 are substantially located in the same annular region. Specifically, the other end of each second umbrella rope 152 may be connected to the umbrella cabin body 111 through a connection structure, and may be close to each other. When guide umbrella 121 and main umbrella 122 are in the normal open state, the outer diameter of main umbrella 122 is larger than the outer diameter of guide umbrella 121, for example, the outer diameter of main umbrella 122 is 2 times or more larger than the outer diameter of guide umbrella 121. Parachute device 100 is at the parachute-opening in-process, and cap 112 pulls out main umbrella 122 through guide umbrella 121, because the external diameter size of guide umbrella 121 is less than the external diameter size of main umbrella 122, the parachute-opening time of guide umbrella 121 is shorter, can open the umbrella fast, guide umbrella 121 provides the power of opening for main umbrella 122, and simultaneously, guide umbrella 121 can also play the effect of buffering, prevents that the initial velocity of flight device 200 when descending is too fast.
The controller 140 is communicatively connected to the parachute mechanism 130, and the controller 140 is configured to control the parachute mechanism 130 to drive the cap 112 away from the outlet 1111 in response to an parachute opening instruction to pull the parachute package 120 out of the pod body 111. The controller 140 may be mounted to the canopy body 111.
In this embodiment, the parachute apparatus 100 further includes a power module 142 and a communication module 143 coupled to the controller 140, the communication module 143 is used for communicating with the flying device 200, the power module 142 is electrically connected to the communication module 143 and the controller 140, and the power module 142 is installed on the parachute bay main body 111.
Exemplarily, the number of the power modules 142 may be two, the two power modules 142 are respectively disposed on two sides of the parachute bay main body 111 and are approximately symmetrically disposed with respect to the parachute bay main body 111, the power modules 142 may be installed between the parachute bay main body 111 and the protection bay 113, a space between the parachute bay main body 111 and the protection bay 113 may be effectively utilized, it is avoided that heat generated by the power modules 142 is concentrated to cause an over-high temperature, meanwhile, it is ensured that the two sides of the parachute apparatus 100 are uniformly stressed, and it is avoided that the opposite sides of the parachute apparatus 100 are unevenly stressed to tilt in the landing process.
Further, the controller 140 may be disposed between two power modules 142, the two power modules 142 being symmetrically disposed about the controller 140. The controller 140 may receive a control command sent by the flying device 200 through the communication module 143, and when the flying device 200 is normal, the control command of the flying device 200 may be prior to the control command of the controller 140, that is, the control command of the flying device 200 may directly control the working state of the parachute apparatus 100.
In some embodiments, the power module 142 and the controller 140 can be disposed on opposite sides of the canopy body 111, such that the power module 142 and the controller 140 can be separated from each other, thereby preventing the power module 142 and the controller 140 from concentrating heat and causing excessive temperature
Referring to fig. 4 and 5, the parachute opening mechanism 130 includes first and second parachute opening devices 131 and 132 connected to the nacelle body 111, and the first and second parachute opening devices 131 and 132 are respectively used to apply separating forces to both sides of the cap 112. The controller 140 of the parachute apparatus 100 controls the first and second parachute ejectors 131 and 132 to open in response to the parachute opening command, and when the first and second parachute ejectors 131 and 132 are opened, the first and second parachute ejectors 131 and 132 respectively apply separating forces to both sides of the cap 112, and the direction of the application of the separating forces may substantially coincide with the axial direction of the parachute outlet 111. The cap 112 is separated from the parachute outlet 1111 to rapidly pull out the parachute bag 120, so that the parachute of the parachute bag 120 is opened, and when one of the parachute bags fails, the parachute throwing mechanism 130 can still finish the parachute opening of the parachute bag 120, thereby improving the safety. The amount of separation force applied by each of the first and second umbrella ejectors 131 and 132 to the cap 112 may be substantially uniform.
Specifically, in the present embodiment, the first and second parachute ejectors 131 and 132 may be a kind of initiating explosive device, and the interiors of the ejectors are filled with gunpowder and fuze, and have piston columns. When the fuse is electrified to ignite the gunpowder, the piston column generates impact force on the separation structure of the parachute thrower under the action of explosive impact, the impact force enables the separation structure of the parachute thrower to break, the parachute thrower generates larger impact force towards the cover cap 112, the cover cap 112 generates accelerated motion under the action of impact of the parachute thrower, so that the separation force is rapidly separated from the parachute bay main body 111, the cover cap 112 pulls out the guide parachute 121, the guide parachute 121 is opened in the air, and the first-stage deceleration of the parachute device 100 is realized; the guide parachute 121 pulls out the main parachute 122, and the main parachute 122 opens in the air, thereby realizing the secondary deceleration of the parachute apparatus 100.
In some embodiments, the first and second ejectors 131 and 132 may also be automatic ejectors, which may use compressed air or hydraulic pressure as an ejection power to rapidly eject the cap 112 from the canopy body 111.
In some embodiments, as shown in fig. 5, the first and second umbrella ejectors 131 and 132 are respectively disposed at opposite sides of the umbrella outlet 1111, and the controller 140 is configured to control the first and second umbrella ejectors 131 and 132 to be opened simultaneously in response to an umbrella opening command. Illustratively, the first and second parachute ejectors 131 and 132 may be disposed outside the nacelle body 111 and may be disposed substantially symmetrically about a radial direction of the outlet 1111.
In the process of falling the parachute device 100, the controller 140 can control the first and second parachute throwers 131 and 132 to open simultaneously, so as to simultaneously act on the separating force to both sides of the cap 112, because both sides of the cap 112 simultaneously receive the separating force, both sides of the cap 112 can be separated from the parachute outlet 1111 substantially towards the direction that the cap 112 is far away from the parachute outlet 1111 simultaneously, the cap 112 can pull the guide parachute 121 open uniformly through the first parachute cord 151, ensuring the complete parachute opening of the guide parachute 121, when one of them breaks down, the parachute opening mechanism 130 can still complete the parachute opening of the parachute pack 120, and the safety is improved. Further, in some embodiments, the parachute throwing mechanism 130 can include a plurality of parachutors, which can be spaced around the exit 1111.
In some embodiments, as shown in fig. 4, the parachute apparatus 100 includes a connection mechanism 170 and a state detection sensor 160, the state detection sensor 160 is disposed on at least one of the canopy of the parachute pack 120 and the second parachute cord 152, the connection mechanism 170 is connected to the parachute bay main body 111, the connection mechanism 170 includes a parachute tray 171 and an adjustment member 172, the adjustment member 172 is connected to the parachute tray 171, the parachute tray 171 may be of a substantially disc-sheet structure, the parachute tray 171 is connected between the adjustment member 172 and the second parachute cord 152, specifically, the other end of the second parachute cord 152, which is far away from the main parachute 122, is connected to the parachute tray 171, and the controller 140 is configured to control the adjustment member 172 to tighten the second parachute cord 152 when a detection signal of the state detection sensor 160 corresponds to a preset change. When the canopy of the main umbrella 122 breathes, the adjusting assembly 172 may tighten the second umbrella string 152 to apply an inward pulling force to the outer circumference of the umbrella bag 120, and the outer circumference of the main umbrella 122 may be appropriately closed, thereby suppressing the breathing of the main umbrella 122, so that the parachute apparatus 100 may be smoothly dropped.
The 'breathing phenomenon' means that when the parachute is in a landing state, the canopy of the parachute is filled with gas, the canopy still continues to expand outwards, the surface of the canopy is tensioned, the surface tension of the canopy is increased, the outer diameter of the canopy continues to increase, the canopy rope connected with the canopy is tensioned, and therefore the tension of the canopy rope connected with the canopy is also increased; then the umbrella is contracted, the outer diameter of the umbrella is reduced, the surface of the umbrella is contracted, the surface tension is reduced, the umbrella rope connected with the umbrella is loosened, and the tension of the umbrella rope connected with the umbrella is reduced. In the whole process, the canopy is repeatedly expanded and contracted. The main reason for breathing phenomenon of the canopy is usually caused by the problem of flexible material of the canopy, and as the flexible material cannot keep the shape of the canopy unchanged like a rigid material, the canopy usually fluctuates in the periodic repeated fluctuation period, however, the breathing phenomenon can cause the "surge" or resonance phenomenon of the canopy.
In some embodiments, the condition detecting sensor 160 may include at least one of a flexibility sensor, a tension sensor 161, and a vibration sensor 162. Illustratively, the flexible sensor may comprise a piezoresistive flexible pressure sensor, a capacitive flexible pressure sensor, or a piezoelectric flexible pressure sensor, for example, which may be disposed on a surface of a canopy. When the flexible sensor deforms, the deformation quantity is different, the output voltage of the flexible sensor is also different, and the output voltage increases along with the increase of the deformation quantity, wherein the deformation can comprise multiple types, for example, the flexible sensing device can be bent or stretched, so that bending deformation or stretching deformation occurs; the flexible sensor outputs voltage signals under the action of external force, when the bending degree of the surface of the canopy or the umbrella rope is larger, the voltage signals output by the flexible sensor are larger, and when the change of the detected voltage signals accords with the preset voltage change, the canopy is determined to generate a breathing phenomenon; the tension sensor 161 may be a strain gauge type, in which a tension strain gauge and a compression strain gauge are connected together in a bridge manner, and a resistance value of the strain gauge changes when external pressure is applied, and when a bending degree of the surface of the canopy or the umbrella cord is larger, the resistance value is larger, and when a detected resistance value meets a preset resistance change, it is determined that the canopy generates a breathing phenomenon; the vibration sensor 162 may include an eddy current type vibration sensor 162, an inductive type vibration sensor 162, a capacitive type vibration sensor 162, a piezoelectric type vibration sensor 162, or a resistance strain type vibration sensor 162, when the vibration sensor 162 performs vibration measurement on the canopy, the vibration sensor can convert the vibration parameter of the canopy into an electrical parameter signal (output voltage or output current, etc.), when the vibration quantity is large, the output voltage or output current is larger, and when it is detected that the change of the output voltage corresponds to the change of the preset voltage, or the change of the output current corresponds to the change of the preset current, it is determined that the canopy generates a breathing phenomenon.
In some embodiments, as shown in fig. 4 and 6, the adjustment assembly 172 may include a drive portion 1721 and a telescoping rod 1722. The driving part 1721 is connected with the umbrella disc 171 through an expansion rod 1722, and the driving part 1721 drives the expansion rod 1722 to expand and contract. The state detecting sensor 160 may include a tension sensor 161, and the tension sensor 161 is disposed at the second parachute cord 152 or the canopy, and for example, the tension sensor 161 may be disposed at a canopy surface of the main parachute 122 for detecting a tension of the surface of the main parachute 122. When the tension sensor 161 detects that the tension value is changed according to the preset tension value, the adjusting assembly 172 may tighten the second umbrella rope 152, and the second umbrella rope 152 applies an inward pulling force to the outer circumference of the umbrella bag 120, so as to suppress the breathing phenomenon of the main umbrella 122.
Illustratively, in the process of falling, when it is detected that the tension value of the main parachute 122 is increased and then decreased, and meets the preset variation rule, the parachute device 100 determines that the canopy breathes. When the canopy breathes, the outer diameter of the canopy is continuously increased, the surface of the canopy is in a more tensioned state, the surface tension of the canopy is increased, and meanwhile, the canopy tightens the second umbrella cord 152 more, so that the tension value of the second umbrella cord 152 is also increased, when the canopy, which breathes, contracts, the surface tension value of the canopy is reduced, and at the same time, the tightened second umbrella cord 152 is released, so that the second umbrella cord 152 is tightened, and the tension value of the second umbrella cord 152 is also reduced, so that when the canopy breathes, the tension values of the canopy and the second umbrella cord 152 are substantially changed in a substantially same regular manner, and therefore, the tension sensor 161 can detect the change of the tension values of the canopy and the second umbrella cord 152, and when the detected tension value is increased to the value a and is reduced to the value b, the value a is greater than the value b, the controller 140 controls the driving part 1721 to shorten downwards, and the telescopic rod 1722 tightens the second umbrella cord 152 to apply the tension to the outer periphery of the umbrella 120, thereby inhibiting the breathing phenomenon.
In other embodiments, the adjustment assembly 172 may include a winding portion, the other end of the second umbrella cord 152, which is away from the main umbrella 122, is wound around the winding portion, and when the tension sensor 161 detects that the tension value changes according to the preset tension value, the controller 140 controls the winding portion to rotate in a forward direction to wind a portion of the length of the second umbrella cord 152, such that the second umbrella cord 152 is tightened, and the second umbrella cord 152 applies an inward pulling force to the outer circumference of the umbrella bag 120, such that the breathing phenomenon of the main umbrella 122 is suppressed.
As another example, the state detection sensor 160 further includes a vibration sensor 162, the vibration sensor 162 is disposed on the canopy of the parachute pack 120 or the second parachute harness 152, and when the vibration frequency detected by the vibration sensor 162 is changed according to a preset frequency, the controller 140 controls the driving part 1721 to drive the telescopic rod 1722 to be shortened. When the canopy is breathing, the canopy is regularly expanded outward and then contracted inward, and therefore, under the action of the airflow, the surface of the canopy generates regular vibration, and the vibration frequencies of the canopy and the second canopy cord 152 basically show approximately the same regular change, so that when the vibration sensor 162 detects that the vibration frequency of the canopy or the second canopy cord 152 conforms to the preset frequency change, it is determined that the canopy is breathing, and therefore, the controller 140 may control the driving portion 1721 to shorten the telescopic rod 1722 to inhibit the breathing phenomenon of the canopy.
In some embodiments, the state detection sensor 160 may further include an image sensor (not shown), the image sensor may be disposed outside the umbrella chamber main body 111, and a camera of the image sensor may be disposed toward the side where the umbrella outlet 1111 is located. When the parachute apparatus 100 is landed, the image sensor is used to acquire the outer circumferential profile of the main parachute 122 in real time, and the controller 140 determines the radius change of the outer circumferential profile of the main parachute 122 in real time according to the outer circumferential profile acquired by the image sensor in real time. When the canopy breathes, the canopy can be outwards expanded regularly and then contracts inwards, the radius of the peripheral outline of the canopy is increased and then reduced, and the change is regular. If the radius change of the outer circumference profile conforms to the preset radius change, it is determined that the canopy has a breathing phenomenon, and the controller 140 controls the driving part 1721 to shorten the telescopic rod 1722, so that the second umbrella cord 152 is tightened, and the second umbrella cord 152 applies an inward pulling force to the outer circumference of the umbrella pack 120 to suppress the breathing phenomenon of the canopy. The image sensor can accurately acquire the change of the peripheral contour of the canopy in real time, and determine whether the canopy is in a breathing state by measuring the change of the radius of the peripheral contour in real time, so that the adjusting component 172 can tighten the second canopy rope 152 in time, the breathing phenomenon of the canopy is effectively inhibited, and the stable landing of the flight device 200 is realized.
In some applications, as shown in fig. 4 and 6, the parachute apparatus 100 further comprises a height detection sensor 193, the connection mechanism 170 may comprise a mounting member 173 and a self-separating member 174, the parachute tray 171 is adapted to be connected to the flying device 200 carrying the parachute apparatus 100, and the second parachute line 152, the mounting member 173, the self-separating member 174 and the parachute tray 171 are sequentially connected. When the height detection sensor 193 detects that the height at which the parachute device 100 is located is less than or equal to the preset height, the preset height is a safe height at which the parachute device 100 is landed. The controller 140 is used to control the automatic release 174 to release the attachment 173 from its connection with the umbrella shaft 171. When the height detection sensor 193 detects that the flying device 200 is about to land, the controller 140 is used for controlling the automatic separating piece 174 to automatically separate the mounting piece 173 from the parachute tray 171, so that the parachute is separated from the flying device 200, the phenomenon that the flying device 200 is dragged by the parachute due to the body of the flying device 200 pulled by the parachute is effectively avoided, the flying device 200 can land stably, the flying device 200 is not easy to collide with the ground, and the landing safety is improved.
Illustratively, the automatic separating member 174 may be an explosion bolt, both ends of which are provided with screw coupling parts, and the mounting member 173 may be a mounting ring, which may be screw-coupled with one end of the explosion bolt, and the flying device 200 is coupled with the other end of the explosion bolt by a bolt. The explosion bolt 22 is an initiating explosive device, has a shape structure similar to a bolt, is filled with gunpowder and a fuse, and after the fuse is electrified and detonates the gunpowder, the weak position of the explosion bolt 22 is broken, so that the parachute pack 120 connected with the explosion bolt 22 is separated from the flight device 200. When the flying device 200 is about to land, the controller 140 may control the explosion bolt to be powered on for detonation, and the weak position of the explosion bolt 22 is disconnected, so that the mounting member 173 is separated from the umbrella disc 171, and after the flying device 200 lands, since the parachute is already separated from the flying device 200, the parachute does not generate drag force on the flying device 200, thereby effectively ensuring the safety of the flying device 200 when landing.
In addition, in some embodiments, the automatic separating element 174 may also be an electromagnetic locking mechanism, the electromagnetic locking mechanism may lock the mounting element 173 on the umbrella disc 171, and when the height of the parachute apparatus 100 is less than or equal to the preset height, the controller 140 may control the electromagnetic locking mechanism to release the locking of the mounting element 173, so as to achieve the rapid separation of the parachute from the flying device 200.
The application provides a parachute device and flight device, the controller of parachute device is opening in response to the parachute opening instruction and control first parachute launcher and second parachute launcher for the both sides of block receive the effect of separating force, and the block breaks away from and pulls out the parachute package fast from the umbrella mouth, realizes the parachute-opening of parachute package, and when one of them broke down, parachute opening of parachute package still can be accomplished to parachute-throwing mechanism, has improved the security.
Further, when the flight device breaks down in the air, for example, when the power supply device and the control device of the flight device break down, the parachute device can provide electric energy for the controller through the power supply module of the parachute device, and the controller sends out a parachute opening instruction to the parachute throwing mechanism to control the parachute package to open the parachute; when the flight device descends to the preset height, the controller can also send a control instruction to the automatic separating piece to enable the automatic separating piece to be automatically separated, so that separation between the parachute and the flight device is achieved, the flight device is prevented from being dragged by the parachute, and safety is improved.
In the description herein, references to the description of the terms "one embodiment," "certain embodiments," "an illustrative embodiment," "an example," "a specific example," or "some examples" or the like mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the present application. In this specification, schematic representations of the above terms do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
In the description of the present application, it is to be understood that the terms "length," "above," "front," "top," "inner," "outer," and the like are used in the orientations and positional relationships indicated in the drawings only for the convenience of description and simplicity of description, and do not indicate or imply that the referenced devices or elements must have a particular orientation, be constructed in a particular orientation, and be operated in a particular manner, and thus should not be construed as limiting the present application. 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, features defined as "first", "second", may explicitly or implicitly include one or more of the described features. In the description of the present application, "a plurality" means two or more unless specifically limited otherwise.
In the description of the present application, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted" and "connected" are to be interpreted broadly, e.g., as being either fixedly connected, detachably connected, or integrally connected; may be mechanically connected, may be electrically connected or may be in communication with each other; they may be directly connected or indirectly connected through intervening media, or may be connected through the use of two elements or the interaction of two elements. The specific meaning of the above terms in the present application can be understood by those of ordinary skill in the art as the case may be.
In this application, unless expressly stated or limited otherwise, the recitation of a first feature by "on" a second feature may include the recitation of the first and second features in direct contact, and may also include the recitation of the first and second features not in direct contact, but in contact with each other via additional features between them. Also, the first feature being "above" the second feature includes the first feature being directly above and obliquely above the second feature, or merely indicating that the first feature is at a higher level than the second feature.
While embodiments of the present application have been shown and described, it will be understood by those of ordinary skill in the art that: numerous changes, modifications, substitutions and alterations can be made to the embodiments without departing from the principles and spirit of the application, the scope of which is defined by the claims and their equivalents.
Claims (7)
1. A parachute apparatus, characterized in that, being applied to a flying device, the parachute apparatus comprises:
the umbrella cabin comprises an umbrella cabin body and a cover cap, wherein the umbrella cabin body is provided with an umbrella outlet, and the cover cap is covered on the umbrella outlet;
the parachute bag is accommodated in the parachute cabin main body; one end of the parachute bag is connected with the cap through a first parachute cord, and the other end of the parachute bag is connected with the parachute cabin main body through a second parachute cord;
the umbrella throwing mechanism comprises a first umbrella throwing device and a second umbrella throwing device which are connected with the umbrella cabin body, and the first umbrella throwing device and the second umbrella throwing device are respectively used for acting separating force to two sides of the cover cap;
a controller in communication connection with the parachute ejection mechanism, the controller configured to control the parachute ejection mechanism to disengage the cap from the parachute outlet in a direction away from the parachute outlet in response to an parachute opening instruction to pull the parachute package out of the parachute bay body;
the umbrella cabin is arranged in the protection cabin, the protection cabin is fixedly connected with the umbrella cabin main body, and the inner wall of the protection cabin and the outer wall of the umbrella cabin main body are arranged at intervals;
the power supply module is arranged between the outer wall of the umbrella cabin main body and the inner wall of the protection cabin and is electrically connected with the controller; the number of the power supply modules is two, and the two power supply modules are respectively arranged on two sides of the parachute cabin main body and are symmetrically arranged relative to the parachute cabin main body; the controller is arranged between the two power supply modules;
the connecting mechanism is connected to the umbrella cabin main body and comprises an umbrella disc and an adjusting assembly, and the umbrella disc is connected between the adjusting assembly and the second umbrella rope; the adjusting assembly comprises a driving part and an expansion rod, and the driving part is connected with the umbrella disc through the expansion rod; and
a state detection sensor provided to at least one of the canopy of the parachute pack and the second parachute line; the controller is configured to control the adjusting assembly to tighten the second umbrella rope when a detection signal of the state detection sensor conforms to a preset change; the state detection sensor comprises a tension sensor and a vibration sensor, the tension sensor is arranged on the second parachute rope or the canopy, and when the tension value detected by the tension sensor changes and accords with the preset tension value, the controller controls the driving part to drive the telescopic rod to shorten; the vibration sensor set up in the canopy of parachute package perhaps the second parachute cord when the vibration frequency change that the vibration sensor detected accords with and predetermines the frequency change, the controller control the drive division orders about the telescopic link shortens.
2. A parachute apparatus as claimed in claim 1, wherein the first and second spreaders are respectively disposed on opposite sides of the outlet, the controller being configured to control the first and second spreaders to be simultaneously opened in response to an opening command.
3. A parachute apparatus according to claim 1, further comprising a height detection sensor, wherein the connection mechanism further comprises an installation member and an automatic separating member, wherein the second parachute line, the installation member, the automatic separating member and the parachute tray are connected in sequence, and the parachute tray is used for being connected to a flying device on which the parachute apparatus is mounted; when the height detection sensor detects that the height at which the parachute device is located is smaller than or equal to a preset height, the controller is used for controlling the automatic separating piece to release the connection relation between the mounting piece and the umbrella disc.
4. A parachute apparatus according to claim 3, further comprising a communication module coupled to the controller for communicating with the flying device, wherein the power module is electrically connected to the communication module.
5. A parachute arrangement according to claim 1, wherein the pod is provided with a connection for connection to the flying article.
6. A parachute device according to any one of claims 1 to 5, wherein the parachute pack comprises a leading parachute and a main parachute, the main parachute is connected to the parachute bay main body through the second parachute line, the leading parachute is connected to the top of the main parachute through the first parachute line, and the cap is connected to the top of the leading parachute through a third parachute line.
7. A flying device, characterized in that the flying device is provided with the parachute apparatus as claimed in any one of claims 1 to 6.
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CN113665820A (en) * | 2021-09-30 | 2021-11-19 | 襄阳宏伟航空器有限责任公司 | Separable parachute system |
CN115367120A (en) * | 2022-08-30 | 2022-11-22 | 南京云之璟机电科技有限公司 | Traction type pneumatic launching umbrella net system and launching method thereof |
CN117284484A (en) * | 2023-11-09 | 2023-12-26 | 南京航空航天大学 | Helicopter rotor tail rotor failure protection system and helicopter |
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