CN111806703B - Cloud computing type emergency state identification platform - Google Patents
Cloud computing type emergency state identification platform Download PDFInfo
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- CN111806703B CN111806703B CN202010232895.7A CN202010232895A CN111806703B CN 111806703 B CN111806703 B CN 111806703B CN 202010232895 A CN202010232895 A CN 202010232895A CN 111806703 B CN111806703 B CN 111806703B
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- 239000002360 explosive Substances 0.000 claims abstract description 30
- 238000005474 detonation Methods 0.000 claims abstract description 10
- 238000001514 detection method Methods 0.000 claims description 22
- 230000000007 visual effect Effects 0.000 claims description 18
- 238000001816 cooling Methods 0.000 claims description 12
- 238000012544 monitoring process Methods 0.000 claims description 11
- 238000000034 method Methods 0.000 claims description 5
- 238000004891 communication Methods 0.000 claims description 4
- 208000027418 Wounds and injury Diseases 0.000 abstract description 3
- 230000006378 damage Effects 0.000 abstract description 3
- 208000014674 injury Diseases 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 6
- 239000000306 component Substances 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 230000004044 response Effects 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 241000700605 Viruses Species 0.000 description 1
- 230000003044 adaptive effect Effects 0.000 description 1
- 230000010485 coping Effects 0.000 description 1
- 239000008358 core component Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
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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
- B64D25/00—Emergency apparatus or devices, not otherwise provided for
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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
- B64D43/00—Arrangements or adaptations of instruments
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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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L67/00—Network arrangements or protocols for supporting network services or applications
- H04L67/01—Protocols
- H04L67/02—Protocols based on web technology, e.g. hypertext transfer protocol [HTTP]
- H04L67/025—Protocols based on web technology, e.g. hypertext transfer protocol [HTTP] for remote control or remote monitoring of applications
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L67/00—Network arrangements or protocols for supporting network services or applications
- H04L67/01—Protocols
- H04L67/10—Protocols in which an application is distributed across nodes in the network
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L67/00—Network arrangements or protocols for supporting network services or applications
- H04L67/01—Protocols
- H04L67/12—Protocols specially adapted for proprietary or special-purpose networking environments, e.g. medical networks, sensor networks, networks in vehicles or remote metering networks
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- Engineering & Computer Science (AREA)
- Computer Networks & Wireless Communication (AREA)
- Signal Processing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Health & Medical Sciences (AREA)
- Computing Systems (AREA)
- General Health & Medical Sciences (AREA)
- Medical Informatics (AREA)
- Alarm Systems (AREA)
Abstract
The invention relates to a cloud computing type emergency state identification platform, which comprises: the field self-destruction mechanism is arranged below the propeller of the helicopter and used for automatically exploding the propeller of the helicopter when receiving a self-destruction request instruction; the on-site self-destruction mechanism comprises an instruction receiving device, an explosive storage tank, an electronic detonation device and a gas pushing device; the electronic detonation device is connected with the instruction receiving device and used for detonating explosives in the explosive storage tank when the self-destruction request instruction is received, and the explosive storage tank is tied on the support frame of the propeller. The cloud computing type emergency state identification platform is intelligent in operation and convenient to control. The propeller can be directly fried under the condition that people are identified to escape and the flying height meets the requirement, so that the escape personnel are prevented from being sucked into the injury range of the propeller.
Description
Technical Field
The invention relates to the field of cloud computing systems, in particular to a cloud computing type emergency state identification platform.
Background
Currently, a cloud computing service is provided by a provider, and in order to guarantee information security, the provider should set a corresponding access right according to the requirement condition of a user side, so as to guarantee the secure sharing of information resources. Under an open internet environment, on one hand, a supplier needs to make setting work of access authority to strengthen reasonable sharing and application of resources; on the other hand, the encryption work needs to be done, the information security protection is strengthened from the supplier to the user, the network security construction is noticed, and the user security is effectively guaranteed. Therefore, the development of the cloud computing technology can strengthen the construction of a security technology system, and the information protection level is improved in the reasonable setting of the access authority. Meanwhile, the cloud computing has the advantages of high computing speed, timely response, distributed processing and the like.
In the prior art, how to use various advantages of cloud computing in various specific application fields, such as monitoring of critical states of helicopters and selection of emergency response modes, is one of the problems to be solved by technical personnel in the related fields.
Disclosure of Invention
In order to solve the technical problems in the related field, the invention provides a cloud computing type emergency state identification platform which can utilize a cloud computing server to perform corresponding emergency state monitoring and emergency coping mode selection on each helicopter in a flying state in a jurisdiction area, so that when the helicopter is judged to have an accident, the flying height meets the requirement and personnel jump out of the helicopter, propellers are quickly exploded to provide an opportunity for the personnel on board to escape by using a parachute.
Therefore, the invention needs to have the following three important points:
(1) when the helicopter is above a preset height and a scene that a human body escapes from the helicopter appears, a propeller of the helicopter is automatically destroyed immediately to avoid the propeller from damaging the human body;
(2) when the propellers are blown away, the gas pushing equipment is adopted to provide vertical upward thrust for the fallen propellers so as to further avoid the propellers from hurting the human body below;
(3) the state of each helicopter is detected and managed in a cloud computing server mode, so that the local hardware load of the helicopter is reduced, and meanwhile, the timeliness of emergency state response is guaranteed.
According to an aspect of the present invention, there is provided a cloud computing type emergency state recognition platform, including:
the field self-destruction mechanism is arranged below the propeller of the helicopter and used for automatically exploding the propeller of the helicopter when receiving a self-destruction request instruction;
the on-site self-destruction mechanism comprises an instruction receiving device, an explosive storage tank, an electronic detonation device and a gas pushing device;
the electronic detonation device is connected with the instruction receiving device and is used for detonating explosives in the explosive storage tank when the self-destruction request instruction is received, and the explosive storage tank is tied on a support frame of the propeller;
the gas pushing equipment is arranged at the base position of the support frame of the propeller and used for providing vertical upward thrust for the propeller falling off the support frame when receiving a self-destruction request instruction;
the instant cooling equipment is bound on a support frame of the propeller, is positioned on the explosive storage tank and is used for providing cooling operation for a tank body of the explosive storage tank when the helicopter flies;
the altitude measuring equipment is arranged in an instrument panel of the helicopter and used for judging the current real-time altitude of the helicopter based on the air pressure detection result nearby the altitude measuring equipment;
the visual detection equipment is arranged at the top end of the door body of the helicopter and used for detecting whether a human body target exists below the door body or not when the door body of the helicopter is opened;
the cloud computing server is arranged at the far end of the helicopter, is respectively connected with the height measuring equipment, the visual detection equipment and the instruction receiving equipment through a network, and is used for sending a self-destruction request instruction or sending a safety monitoring instruction when the visual detection equipment detects that a human body exists below a door body and the real-time height is greater than or equal to a preset height threshold value;
and the gas pushing equipment is also used for providing vertical upward thrust for the propeller falling off the support frame when receiving the safety monitoring instruction.
According to another aspect of the present invention, there is also provided a cloud computing type emergency state identification method, including using a cloud computing type emergency state identification platform as described above, for detecting whether each helicopter is in an emergency state based on a cloud computing server and executing corresponding decisions.
The cloud computing type emergency state identification platform is intelligent in operation and convenient to control. The propeller can be directly fried under the condition that people are identified to escape and the flying height meets the requirement, so that the escape personnel are prevented from being sucked into the injury range of the propeller.
Drawings
Embodiments of the invention will now be described with reference to the accompanying drawings, in which:
fig. 1 is a schematic diagram illustrating components of a cloud computing emergency recognition platform according to the present invention.
Fig. 2 is a block diagram illustrating a structure of a cloud-computing emergency recognition platform according to a first embodiment of the present invention.
Fig. 3 is a block diagram illustrating a structure of a cloud-computing emergency recognition platform according to a second embodiment of the present invention.
Detailed Description
Embodiments of the cloud computing type emergency state recognition platform according to the present invention will be described in detail below with reference to the accompanying drawings.
At present, because the helicopter adopts a single-engine airplane mode, the safety level of the helicopter is inferior to that of a multi-engine fixed wing airplane, once an accident occurs to the helicopter, personnel on the helicopter are difficult to escape safely in a self-contained landing bag mode, and the reason is that the huge suction force of a propeller in the operation process can quickly suck the escaped personnel into the injury range of the propeller.
In order to overcome the defects, the cloud computing type emergency state identification platform is set up, and the corresponding technical problem can be effectively solved.
Fig. 1 is a schematic diagram illustrating components of a cloud computing emergency recognition platform according to the present invention.
As shown in fig. 1, the cloud computing server serves as a core component for communication and operation, and bridges are set up for communication and computation of other components.
Fig. 2 is a block diagram illustrating a structure of a cloud-computing emergency identification platform according to a first embodiment of the present invention, where the platform includes:
the field self-destruction mechanism is arranged below the propeller of the helicopter and used for automatically exploding the propeller of the helicopter when receiving a self-destruction request instruction;
the on-site self-destruction mechanism comprises an instruction receiving device, an explosive storage tank, an electronic detonation device and a gas pushing device;
the electronic detonation device is connected with the instruction receiving device and is used for detonating explosives in the explosive storage tank when the self-destruction request instruction is received, and the explosive storage tank is tied on a support frame of the propeller;
the gas pushing equipment is arranged at the base position of the support frame of the propeller and used for providing vertical upward thrust for the propeller falling off the support frame when receiving a self-destruction request instruction;
the instant cooling equipment is bound on a support frame of the propeller, is positioned on the explosive storage tank and is used for providing cooling operation for a tank body of the explosive storage tank when the helicopter flies;
the altitude measuring equipment is arranged in an instrument panel of the helicopter and used for judging the current real-time altitude of the helicopter based on the air pressure detection result nearby the altitude measuring equipment;
the visual detection equipment is arranged at the top end of the door body of the helicopter and used for detecting whether a human body target exists below the door body or not when the door body of the helicopter is opened;
the cloud computing server is arranged at the far end of the helicopter, is respectively connected with the height measuring equipment, the visual detection equipment and the instruction receiving equipment through a network, and is used for sending a self-destruction request instruction or sending a safety monitoring instruction when the visual detection equipment detects that a human body exists below a door body and the real-time height is greater than or equal to a preset height threshold value;
and the gas pushing equipment is also used for providing vertical upward thrust for the propeller falling off the support frame when receiving the safety monitoring instruction.
Fig. 3 is a block diagram illustrating a structure of a cloud-computing emergency identification platform according to a second embodiment of the present invention, where the platform includes:
the kernel analysis equipment is used for receiving the utilization rate of the current kernel of the visual detection equipment, and the utilization rate is a percentage;
the utilization rate analysis equipment is connected with the kernel analysis equipment and is used for sending a load overfilling signal when the utilization rate exceeds the limit;
the field self-destruction mechanism is arranged below the propeller of the helicopter and used for automatically exploding the propeller of the helicopter when receiving a self-destruction request instruction;
the on-site self-destruction mechanism comprises an instruction receiving device, an explosive storage tank, an electronic detonation device and a gas pushing device;
the electronic detonation device is connected with the instruction receiving device and is used for detonating explosives in the explosive storage tank when the self-destruction request instruction is received, and the explosive storage tank is tied on a support frame of the propeller;
the gas pushing equipment is arranged at the base position of the support frame of the propeller and used for providing vertical upward thrust for the propeller falling off the support frame when receiving a self-destruction request instruction;
the instant cooling equipment is bound on a support frame of the propeller, is positioned on the explosive storage tank and is used for providing cooling operation for a tank body of the explosive storage tank when the helicopter flies;
the altitude measuring equipment is arranged in an instrument panel of the helicopter and used for judging the current real-time altitude of the helicopter based on the air pressure detection result nearby the altitude measuring equipment;
the visual detection equipment is arranged at the top end of the door body of the helicopter and used for detecting whether a human body target exists below the door body or not when the door body of the helicopter is opened;
the cloud computing server is arranged at the far end of the helicopter, is respectively connected with the height measuring equipment, the visual detection equipment and the instruction receiving equipment through a network, and is used for sending a self-destruction request instruction or sending a safety monitoring instruction when the visual detection equipment detects that a human body exists below a door body and the real-time height is greater than or equal to a preset height threshold value;
and the gas pushing equipment is also used for providing vertical upward thrust for the propeller falling off the support frame when receiving the safety monitoring instruction.
Next, a specific configuration of the cloud computing emergency recognition platform according to the present invention will be further described.
In the cloud computing type emergency state recognition platform: the instant cooling equipment is further used for stopping providing cooling operation for the tank body of the explosive storage tank when receiving a self-destruction request instruction.
In the cloud computing type emergency state recognition platform: the utilization rate analysis device is also used for sending out a load sufficiency signal when the received utilization rate is not over limit.
The cloud computing type emergency state recognition platform further comprises: and the AT89C51 singlechip is connected with the utilization rate analysis equipment and is used for entering a working mode from a sleep mode when receiving a load overfilling signal.
In the cloud computing type emergency state recognition platform: the AT89C51 single chip microcomputer is also used for bearing partial tasks of the visual detection equipment when the working mode is entered.
In the cloud computing type emergency state recognition platform: the AT89C51 single chip microcomputer is also used for refusing to undertake partial tasks of the visual detection equipment when entering the sleep mode.
The cloud computing type emergency state recognition platform further comprises: and the wireless communication interface is connected with the height measuring equipment and used for receiving the output data of the height measuring equipment and wirelessly transmitting the output data.
Meanwhile, in order to overcome the defects, the third embodiment of the invention also provides a cloud computing type emergency state identification method, which comprises the step of using the cloud computing type emergency state identification platform for detecting whether each helicopter is in an emergency state or not and executing corresponding decisions based on the cloud computing server.
In addition, cloud computing is based on advanced internet technology, and its implementation forms are numerous, and mainly completed through the following forms:
(1) software is a service. Generally, a user issues a service demand, and the cloud system provides resources, programs and the like to the user through a browser. It is worth mentioning that it does not cost any cost to use the browser application to deliver the service information, so the provider can do the maintenance work of the application program.
(2) A network service. Developers can continuously improve and develop new application products on the basis of the API, and the operation performance in a single-machine program is greatly improved.
(3) And (4) platform service. The system generally serves a development environment, assists an intermediary in upgrading and researching programs, simultaneously improves a user downloading function, enables users to download programs through the Internet, and has the characteristics of being fast and efficient.
(4) And (4) integrating the Internet. When the internet is used for sending out instructions, perhaps the same type of services are numerous, and the cloud system can be matched with the adaptive services according to the requirements of terminal users.
(5) A business service platform. The purpose of building a business service platform is to provide a platform for users and providers to communicate with each other, thereby requiring management of services and software, i.e., service matching applications.
(6) Managing the service provider. The application mode is not strange, the IT industry is frequently served, and the common service contents comprise: scanning mail viruses, monitoring application environments, etc.
In the description herein, references to the description of the term "one embodiment," "some embodiments," "an example," "a specific example," or "some examples," etc., 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 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.
Although the present invention has been described with reference to the above embodiments, it should be understood by those skilled in the art that various changes may be made and equivalents may be substituted without departing from the spirit and scope of the invention. Therefore, the protection scope of the present invention should be subject to the scope defined by the claims of the present application.
Claims (10)
1. A cloud computing emergency identification platform, the platform comprising:
the field self-destruction mechanism is arranged below the propeller of the helicopter and used for automatically exploding the propeller of the helicopter when receiving a self-destruction request instruction;
the on-site self-destruction mechanism comprises an instruction receiving device, an explosive storage tank, an electronic detonation device and a gas pushing device;
the electronic detonation device is connected with the instruction receiving device and is used for detonating explosives in the explosive storage tank when the self-destruction request instruction is received, and the explosive storage tank is tied on a support frame of the propeller;
the gas pushing equipment is arranged at the base position of the support frame of the propeller and used for providing vertical upward thrust for the propeller falling off the support frame when receiving a self-destruction request instruction;
the instant cooling equipment is bound on a support frame of the propeller, is positioned on the explosive storage tank and is used for providing cooling operation for a tank body of the explosive storage tank when the helicopter flies;
the altitude measuring device is arranged in an instrument panel of the helicopter and used for judging the current real-time altitude of the helicopter based on the air pressure detection result near the altitude measuring device;
the visual detection equipment is arranged at the top end of the door body of the helicopter and used for detecting whether a human body target exists below the door body or not when the door body of the helicopter is opened;
the cloud computing server is arranged at the far end of the helicopter, is respectively connected with the height measuring equipment, the visual detection equipment and the instruction receiving equipment through a network, and is used for sending a self-destruction request instruction or sending a safety monitoring instruction when the visual detection equipment detects that a human body exists below a door body and the real-time height is greater than or equal to a preset height threshold value;
and the gas pushing equipment is also used for providing vertical upward thrust for the propeller falling off the support frame when receiving the safety monitoring instruction.
2. A cloud computing-based emergency status recognition platform according to claim 1, wherein:
the instant cooling equipment is further used for stopping providing cooling operation for the tank body of the explosive storage tank when receiving a self-destruction request instruction.
3. A cloud-computing emergency state identification platform according to claim 2, wherein said cloud-computing emergency state identification platform further comprises:
the kernel analysis equipment is used for receiving the utilization rate of the current kernel of the visual detection equipment, and the utilization rate is a percentage.
4. A cloud-computing emergency state identification platform according to claim 3, wherein said cloud-computing emergency state identification platform further comprises:
and the utilization rate analysis equipment is connected with the kernel analysis equipment and is used for sending a load overfilling signal when the utilization rate exceeds the limit.
5. A cloud computing-based emergency status recognition platform according to claim 4, wherein:
the utilization rate analysis device is also used for sending out a load sufficiency signal when the received utilization rate is not over limit.
6. The cloud-computing emergency state recognition platform of claim 5, wherein the cloud-computing emergency state recognition platform further comprises:
and the AT89C51 singlechip is connected with the utilization rate analysis equipment and is used for entering a working mode from a sleep mode when receiving a load overfilling signal.
7. A cloud computing-based emergency status recognition platform according to claim 6, wherein:
the AT89C51 single chip microcomputer is also used for bearing partial tasks of the visual detection equipment when the working mode is entered.
8. A cloud computing-based emergency status recognition platform according to claim 7, wherein:
the AT89C51 single chip microcomputer is also used for refusing to undertake partial tasks of the visual detection equipment when entering the sleep mode.
9. The cloud-computing emergency status identification platform of claim 8, further comprising:
and the wireless communication interface is connected with the height measuring equipment and used for receiving the output data of the height measuring equipment and wirelessly transmitting the output data.
10. A cloud-computing emergency identification method, the method comprising providing a cloud-computing emergency identification platform according to any one of claims 1 to 9, for detecting whether each helicopter is in an emergency state based on a cloud computing server, and performing corresponding decision making.
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| Application Number | Priority Date | Filing Date | Title |
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| CN202010232895.7A CN111806703B (en) | 2020-03-28 | 2020-03-28 | Cloud computing type emergency state identification platform |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202010232895.7A CN111806703B (en) | 2020-03-28 | 2020-03-28 | Cloud computing type emergency state identification platform |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| US7946530B1 (en) * | 2005-06-13 | 2011-05-24 | Talmage Jr Robert N | Modular adaptive configured helicopter |
| CN101157385A (en) * | 2007-11-27 | 2008-04-09 | 谭生 | Helicopter |
| KR20110086920A (en) * | 2010-01-25 | 2011-08-02 | 정재원 | Automatic cutting blades to survive a hellicopter pilot |
| CN103538725B (en) * | 2012-07-16 | 2016-04-27 | 中国人民解放军军械工程学院 | Helicopter emergency escape system |
| CN105730702A (en) * | 2016-02-17 | 2016-07-06 | 中山浩发节能科技有限公司 | Emergency rescue device guaranteeing slow landing of aircraft when fault happens |
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