Speed-controllable impurity removal type exhaust pipe framework for hovercraft cabin
By introducing a combination of wind speed detection mechanism and high-pressure nozzle into the exhaust duct of the hovercraft nacelle, the self-cleaning function of the exhaust duct is realized, solving the problem of reducing ventilation performance caused by dust accumulation, and improving engine efficiency and equipment life.
Patent Information
- Application Number
- CN202421623365.5
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-07-10
- Publication Date
- 2025-04-11
- Estimated Expiration
- 2034-07-10
AI Technical Summary
The exhaust ducts of existing hovercraft cabins are prone to accumulate dust and impurities during operation, resulting in a reduction in ventilation performance and affecting engine efficiency.
A controlled speed removal exhaust duct architecture is designed, including the exhaust duct main body, docking pipe body, wind speed detection mechanism, fan blade assembly and high-pressure nozzle. The exhaust rate is monitored in real time through the wind speed detection mechanism, and the opening and closing frequency of the high-pressure nozzle is adjusted to realize the self-cleaning function.
It effectively improves the overall functional practicality and adaptability of the exhaust duct, significantly improves ventilation performance and engine efficiency, and extends the service life of the equipment.
Smart Images

Figure CN222742907U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of hovercraft equipment, and in particular to a controllable speed-removing impurity exhaust duct structure for a hovercraft engine room. Background Art
[0002] A hovercraft is a modern water vehicle that uses an air cushion and fan technology for suspension and propulsion. It is widely used in water rescue, military patrols, tourism and other related fields.
[0003] At present, hovercraft are usually equipped with air propellers and engines that can provide power, and the ventilation volume of the engine compartment is an important indicator for evaluating the quality of a compartment design. If the ventilation performance of the compartment is poor, the heat generated by the engine cannot be quickly discharged, and the temperature inside the compartment rises sharply, which in turn causes the engine to automatically shut down due to excessive temperature, affecting the normal operation of the hovercraft; at the same time, the excessively high temperature inside the compartment will also increase the risk factor of the circuit, electrical components and oil supply pipelines, affecting the safety of the hull operation.
[0004] The existing hovercraft cabin ventilation device includes a cabin cover with an engine installed inside, and an exhaust duct installed on the cabin cover for ventilation. The traditional exhaust duct structure usually only relies on the exhaust channel to correspond to the air inlet of the cabin cover for ventilation, and no special dust removal and cleaning structure design is set. During the operation of the exhaust fan blades, dust and other particles in the air are easy to gradually accumulate along the air guide path to the fan blades. When the dust and impurities reach a certain level, the ventilation performance will be reduced, thereby affecting the engine efficiency. Utility Model Content
[0005] To this end, the utility model provides a controllable speed impurity removal exhaust duct structure for the hovercraft cabin, so as to solve the technical problem that the exhaust duct for the hovercraft cabin ventilation function in the prior art is prone to accumulate dust and impurities on its exhaust fan blades during operation, resulting in reduced engine ventilation performance efficiency.
[0006] In order to achieve the above purpose, the utility model provides the following technical solutions:
[0007] A controllable speed impurity removal exhaust duct structure for a hovercraft engine room, comprising:
[0008] Exhaust duct body;
[0009] A butt joint body is detachably fixedly assembled and connected to one end of the exhaust pipe body;
[0010] A wind speed detection mechanism, fixedly assembled and arranged on the inner side wall of the butt-jointed pipe body;
[0011] A fan blade assembly is fixedly mounted on the inner wall of the exhaust duct body;
[0012] The high-pressure nozzle is fixedly assembled on the inner wall of the exhaust pipe body, and the high-pressure nozzle corresponds to the blade position of the fan blade assembly.
[0013] On the basis of the above technical solution, the utility model is further described as follows:
[0014] As a further solution of the utility model, it also includes: a flange assembly;
[0015] One end of the exhaust pipe body away from the air inlet is connected and assembled with one end of the butt joint pipe body through the flange assembly.
[0016] As a further solution of the utility model, the flange assembly includes a flange body, a sealing gasket and bolt fasteners;
[0017] The flange bodies are provided in two groups, and the two groups of flange bodies are respectively fixedly connected to the exhaust pipe body and the opposite ends of the butt joint body in a one-to-one correspondence, and the two groups of flange bodies are fixedly assembled and connected by the bolt fasteners;
[0018] The sealing gasket layer is also arranged between the circumferential side portions of the two groups of flange bodies.
[0019] As a further solution of the utility model, an air outlet is formed at one end of the butt joint pipe body away from the exhaust duct main body, and a baffle is fixedly provided on the butt joint pipe body corresponding to the air outlet.
[0020] As a further solution of the utility model, a sound-absorbing layer is fixedly attached to the interior of the butt-joint pipe body.
[0021] As a further solution of the utility model, it also includes:
[0022] A positioning bracket, fixedly mounted on the inner wall of the exhaust duct body;
[0023] The fan blade assembly is fixedly mounted on the positioning bracket.
[0024] As a further solution of the utility model, the high-pressure nozzles are provided in several groups, and the several groups of high-pressure nozzles are respectively and spaced apart and fixedly assembled on the inner wall of the exhaust duct body, and the several groups of high-pressure nozzles correspond to the blade positions of the fan blade assembly.
[0025] As a further solution of the utility model, the high-pressure nozzle is configured as a high-pressure water nozzle;
[0026] The high-pressure water nozzle is connected to a water pump via a pipeline, and the water pump is placed inside a water tank or inside the water body where the hull is located.
[0027] As a further solution of the utility model, the high-pressure nozzle is configured as a high-pressure gas nozzle;
[0028] The high-pressure air nozzle is connected to an air pump via a pipeline.
[0029] As a further solution of the utility model, it also includes:
[0030] An electric control structure, including a mobile power source and a control module connected by an electric circuit;
[0031] The control output end of the control module is connected to the input end of the relay through a circuit, and the output end of the relay is respectively connected to the fan blade assembly and the water pump / air pump through a circuit; the wind speed detection mechanism is connected to the control input end of the control module through a circuit.
[0032] The utility model has the following beneficial effects:
[0033] This architecture can effectively correspond to the exhaust duct body, the docking pipe body, the fan blade assembly and the baffle to form a self-cleaning function through the high-pressure nozzle. At the same time, it can effectively monitor the exhaust rate in real time with the help of the wind speed detection mechanism. Then, the monitored exhaust rate can be used as the corresponding conversion parameter of the dust accumulation amount to more clearly define the opening and closing frequency of the high-pressure nozzle, which effectively improves the overall functional practicality and adaptability of the architecture. BRIEF DESCRIPTION OF THE DRAWINGS
[0034] In order to more clearly illustrate the implementation methods of the utility model or the technical solutions in the prior art, the drawings required for the implementation methods or the description of the prior art will be briefly introduced below. The structures, proportions, sizes, etc. illustrated in this specification are only used to match the contents disclosed in the specification for people familiar with this technology to understand and read. Any structural modification, change in proportional relationship or adjustment of size should still fall within the scope of the technical contents disclosed in the utility model without affecting the effects and purposes that can be achieved by the utility model.
[0035] Figure 1 The speed-controllable impurity-removing exhaust duct structure for the hovercraft cabin provided in Example 1 of the utility model corresponds to the overall axonometric structural schematic diagram of one side of the air inlet.
[0036] Figure 2 The speed-controllable impurity-removing exhaust duct structure for the hovercraft cabin provided in Example 1 of the utility model corresponds to the overall axonometric structural schematic diagram of one side of the air outlet.
[0037] Figure 3The utility model provides an overall axonometric structural diagram of a controllable speed impurity removal exhaust duct structure for a hovercraft cabin according to an embodiment 2 of the present invention.
[0038] In the accompanying drawings, the components represented by the reference numerals are listed as follows:
[0039] 1. Exhaust duct body;
[0040] 2. Flange assembly; 201. Flange body; 202. Sealing gasket; 203. Bolt fasteners;
[0041] 3. Butt joint body; 4. Dust cover; 5. Air outlet; 6. Grid baffle; 7. Wind speed detection mechanism; 8. Fan blade assembly; 9. Positioning bracket; 10. High-pressure nozzle. DETAILED DESCRIPTION
[0042] The following is a specific embodiment of the present invention. People familiar with the technology can easily understand the other advantages and functions of the present invention from the contents disclosed in this specification. Obviously, the described embodiment is a part of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.
[0043] The terms such as "upper", "lower", "left", "right", and "middle" used in this specification are only for the convenience of description and are not intended to limit the scope of the present invention. Changes or adjustments to their relative relationships shall be deemed to be within the scope of the present invention without substantially changing the technical content.
[0044] Example 1
[0045] like Figure 1 to Figure 2 As shown, the embodiment of the utility model provides a controllable speed impurity removal exhaust duct structure for the engine room of an air cushion vehicle, including an exhaust duct body 1, a flange assembly 2, a butt joint body 3, an air outlet 5, a baffle plate 6, a wind speed detection mechanism 7, a fan blade assembly 8, a positioning support frame 9 and a high-pressure nozzle 10, so as to effectively correspond to the exhaust duct body 1, the butt joint body 3, the fan blade assembly 8 and the baffle plate 6 through the high-pressure nozzle 10 to form a self-cleaning function, and at the same time, the wind speed detection mechanism 7 can be used to effectively monitor the exhaust speed in real time, and then the monitored exhaust speed can be used as the corresponding conversion parameter of the dust accumulation amount, so as to more clearly define the opening and closing frequency of the high-pressure nozzle 10, thereby improving the overall functional practicality. The specific settings are as follows:
[0046] Please refer to Figure 1 to Figure 2The end of the exhaust duct body 1 away from its air inlet is fixedly assembled and connected with one end of the docking pipe body 3 through the flange assembly 2. The docking pipe body 3 is formed with an air outlet 5 at the end away from the exhaust duct body 1, and the docking pipe body 3 is fixedly provided with a baffle plate 6 corresponding to the air outlet 5, so that the baffle plate 6 can correspond to the air outlet 5 to effectively ensure the established ventilation volume, and can also play a certain debris blocking function with the help of the baffle plate 6. At the same time, based on the detachable setting between the exhaust duct body 1 and the docking pipe body 3, the docking pipe body 3 and its corresponding baffle plate 6 can be effectively disassembled and cleaned, thereby significantly improving the cleaning effect.
[0047] Specifically, the flange assembly 2 includes a flange body 201, a sealing gasket layer 202 and bolt fasteners 203; wherein, the flange body 201 is provided in two groups, and the two groups of flange bodies 201 are respectively fixedly connected to the exhaust duct body 1 and the opposite end of the docking pipe body 3, and the two groups of flange bodies 201 are fixedly assembled and connected by the bolt fasteners 203.
[0048] As a preferred solution of this embodiment, the sealing gasket layer 202 is also positioned between the circumferential side portions of the two groups of the flange bodies 201 to significantly improve the sealing performance of the entire air duct.
[0049] As another preferred solution of this embodiment, a sound-absorbing layer is fixedly attached to the interior of the butt-joint pipe body 3 , so as to utilize the sound-absorbing layer to effectively reduce the noise spillover corresponding to the position of the air outlet 5 .
[0050] Please continue to refer to Figure 1 to Figure 2 The positioning bracket 9 is fixedly assembled on the inner wall of the exhaust duct body 1, and the fan blade assembly 8 is fixedly assembled on the positioning bracket 9 to complete the predetermined exhaust driving function through the fan blade assembly 8; the inner wall of the butt joint body 3 is fixedly assembled with at least one group of the wind speed detection mechanism 7, which is used to use the wind speed detection mechanism 7 to monitor the exhaust rate at the position of the air outlet 5 in real time, and then the monitored exhaust rate can be used as the corresponding conversion parameter of the dust accumulation amount, so as to more clearly and efficiently determine the opening and closing frequency of the high-pressure nozzle 10, and at the same time, it can effectively help users understand the operating status of the exhaust system based on the monitored exhaust rate, and flexibly adjust the exhaust volume of the air outlet 5 based on the fan blade assembly 8, and then accurately adjust the exhaust volume to avoid excessive operation of the fan blade assembly 8, thereby extending the service life of the equipment, reducing the maintenance and replacement costs, and improving the overall functional adaptability and practicality.
[0051] The wind speed detection mechanism 7 can adopt but is not limited to a small ultrasonic wind speed and direction sensor. This product has no startup wind speed limit, works at zero wind speed, has no angle limit, and is 360° all-round.
[0052] Please continue to refer to Figure 1 The high-pressure nozzles 10 are provided in a plurality of groups, and the plurality of groups of the high-pressure nozzles 10 are fixedly assembled at intervals on the inner wall of the exhaust duct body 1, and the plurality of groups of the high-pressure nozzles 10 correspond to the blade positions of the fan blade assembly 8, so as to form a self-cleaning function by effectively corresponding to the blade direction position of the fan blade assembly 8 and the baffle plate 6 through the high-pressure nozzles 10.
[0053] Specifically, the high-pressure nozzle 10 is configured as a high-pressure water nozzle and / or a high-pressure air nozzle; wherein the high-pressure water nozzle is connected to a water pump via a pipeline, and the water pump is placed inside a water tank or inside the water body where the hull is located; the high-pressure air nozzle is connected to an air pump via a pipeline; so as to realize the air / water spray cleaning function.
[0054] The controllable speed impurity removal exhaust duct structure for the hovercraft engine room also includes an electric control structure;
[0055] The electric control structure includes a mobile power supply and a control module connected by a circuit. The mobile power supply can be, but is not limited to, a lithium battery. The control module can be, but is not limited to, a single-chip control board of model AT80C51 and a microcontroller of model STM32. The control output end of the control module is connected to the input end of a relay through a circuit. The output end of the relay is respectively connected to the fan blade assembly 8 and the water pump / air pump through a circuit. The wind speed detection mechanism 7 is connected to the control input end of the control module through a circuit, so as to realize the automatic control of the wind speed detection mechanism 7, the fan blade assembly 8 and the water pump / air pump. At the same time, when the water pump / air pump starts to spray and clean, the blades of the fan blade assembly 8 can be controlled to rotate at a specific speed to effectively improve the spray and clean efficiency. In addition, when the noise is too loud, the rotation speed of the blades of the fan blade assembly 8 can be adjusted to control the noise.
[0056] Example 2
[0057] In Example 2, the same symbols are given to the same structures as in Example 1, and the same descriptions are omitted. Example 2 is improved on the basis of Example 1, please refer to Figure 3 ,
[0058] The end of the butt joint pipe body 3 corresponding to the air outlet 5 is also threadedly assembled with a dust cover 4, so that the dust cover 4 can effectively realize the installation when it is stationary to reduce the entry of dust into the interior of the pipe body.
[0059] Although the utility model has been described in detail above with general descriptions and specific embodiments, it is obvious to those skilled in the art that some modifications or improvements can be made to the utility model. Therefore, these modifications or improvements made without departing from the spirit of the utility model are within the scope of protection claimed by the utility model.
Claims
1. A controllable speed impurity removal exhaust duct structure for a hovercraft engine room, characterized in that: include: Exhaust duct body; A butt joint body is detachably fixedly assembled and connected to one end of the exhaust pipe body; A wind speed detection mechanism, fixedly assembled and arranged on the inner side wall of the butt-jointed pipe body; A fan blade assembly is fixedly mounted on the inner wall of the exhaust duct body; The high-pressure nozzle is fixedly assembled on the inner wall of the exhaust pipe body, and the high-pressure nozzle corresponds to the blade position of the fan blade assembly.
2. The controllable speed impurity removal exhaust duct structure for the engine room of the hovercraft according to claim 1, characterized in that: Also includes: Flange assembly; One end of the exhaust pipe body away from the air inlet is connected and assembled with one end of the butt joint pipe body through the flange assembly.
3. The controllable speed impurity removal exhaust duct structure for the engine room of the hovercraft according to claim 2, characterized in that: The flange assembly includes a flange body, a sealing gasket and bolt fasteners; The flange bodies are provided in two groups, and the two groups of flange bodies are respectively fixedly connected to the exhaust pipe body and the opposite ends of the butt joint body in a one-to-one correspondence, and the two groups of flange bodies are fixedly assembled and connected by the bolt fasteners; The sealing gasket layer is also arranged between the circumferential side portions of the two groups of flange bodies.
4. The controllable speed impurity removal exhaust duct structure for the engine room of the hovercraft according to claim 2, characterized in that: An air outlet is formed at one end of the butt joint pipe body away from the exhaust pipe main body, and a baffle is fixedly provided on the butt joint pipe body corresponding to the air outlet.
5. The controllable speed impurity removal exhaust duct structure for the engine room of the hovercraft according to claim 1, characterized in that: A sound-absorbing layer is fixedly attached to the interior of the butt-joint pipe body.
6. The controllable speed impurity removal exhaust duct structure for the engine room of the hovercraft according to claim 1, characterized in that: Also includes: A positioning bracket, fixedly mounted on the inner wall of the exhaust duct body; The fan blade assembly is fixedly mounted on the positioning bracket.
7. The controllable speed impurity removal exhaust duct structure for the engine room of the hovercraft according to claim 1, characterized in that: The high-pressure nozzles are provided in a plurality of groups, and the plurality of groups of the high-pressure nozzles are fixedly assembled on the inner wall of the exhaust duct body at intervals, and the plurality of groups of the high-pressure nozzles correspond to the blade positions of the fan blade assembly.
8. The controllable speed impurity removal exhaust duct structure for the engine room of a hovercraft according to claim 1 or 7, characterized in that: The high-pressure nozzle is configured as a high-pressure water nozzle; The high-pressure water nozzle is connected to a water pump via a pipeline, and the water pump is placed inside a water tank or inside the water body where the hull is located.
9. The controllable speed impurity removal exhaust duct structure for the engine room of the hovercraft according to claim 8, characterized in that: The high-pressure nozzle is configured as a high-pressure gas nozzle; The high-pressure air nozzle is connected to an air pump via a pipeline.
10. The controllable speed impurity removal exhaust duct structure for the engine room of the hovercraft according to claim 9, characterized in that: Also includes: An electric control structure, including a mobile power source and a control module connected by an electric circuit; The control output end of the control module is connected to the input end of the relay through a circuit. The output ends are respectively connected to the fan blade assembly and the water pump / air pump through circuits; The wind speed detection mechanism is connected to the control input end of the control module through a circuit.