CN112484576A - Fighting equipment - Google Patents
Fighting equipment Download PDFInfo
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- CN112484576A CN112484576A CN202011416053.3A CN202011416053A CN112484576A CN 112484576 A CN112484576 A CN 112484576A CN 202011416053 A CN202011416053 A CN 202011416053A CN 112484576 A CN112484576 A CN 112484576A
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- machine body
- air
- motor
- air bags
- drill bit
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H13/00—Means of attack or defence not otherwise provided for
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- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- General Engineering & Computer Science (AREA)
- Earth Drilling (AREA)
Abstract
The invention discloses a fighting device, which comprises a machine body mechanism, an adsorption mechanism, a drilling mechanism, a power driving mechanism and an explosive package, wherein the power driving mechanism comprises a driving motor, a mounting seat and a propeller, the power driving mechanism is positioned in the machine body mechanism, and the mounting seat is connected with the machine body mechanism; the driving motor is arranged on the mounting seat, the propeller is connected with the driving motor, and the liquid in the machine body mechanism flows backwards from the front of the machine body mechanism; the adsorption mechanism is arranged in front of the machine body mechanism, and the drilling mechanism is arranged in the adsorption mechanism; the explosive bag is arranged on the machine body mechanism. The invention has simple structure, low manufacturing cost and flexible and convenient use.
Description
Technical Field
The invention relates to the technical field of weaponry, in particular to a combat device.
Background
Peace is a foundation stone for world development, and effective and proper defense conditions are imperative for ensuring the safety of Chinese territory and air-raid neck. However, the existing weaponry is expensive, the technological innovation cost is extremely high, and firstly, a large number of technological talents are needed to bury and dry, and expensive test equipment is required to be matched. The second is a long weapon development cycle, which is enough to push the price of the weapon equipment up to the point of letting the people to smoke the tongue. Third, the price of the weapon equipment is still high and other non-technical reasons exist, which are mainly shown in monopoly of technology by individual countries and companies, the number of countries which can independently manufacture advanced main warfare weapons such as advanced fighters, warships, tanks, ballistic missiles and the like is not more than 5, and the number of countries which can manufacture secondary weapons such as radars, gun barrels, torpedoes and the like and spare parts is not more than 10. Moreover, this situation is exacerbated by the very nature of capital profit-making, which even by extraordinary means artificially creates a stressful situation, inducing regional conflicts and thereby increasing the sales price and sales volume of weaponry. Therefore, the existing weaponry is expensive, which is a technical problem to be solved urgently.
Disclosure of Invention
The invention aims to overcome the defects of the prior art and provides the fighting equipment which is simple in structure, low in manufacturing cost and flexible and convenient to use.
In order to achieve the purpose, the invention provides a fighting device which comprises a machine body mechanism, an adsorption mechanism, a drilling mechanism, a power driving mechanism and an explosive package, wherein the power driving mechanism comprises a driving motor, a mounting seat and a propeller, the power driving mechanism is positioned in the machine body mechanism, and the mounting seat is connected with the machine body mechanism; the driving motor is arranged on the mounting seat, the propeller is connected with the driving motor, and the liquid in the machine body mechanism flows backwards from the front of the machine body mechanism; the adsorption mechanism is arranged in front of the machine body mechanism, and the drilling mechanism is arranged in the adsorption mechanism; the explosive bag is arranged on the machine body mechanism.
Furthermore, the combat equipment also comprises a posture adjusting mechanism, wherein the posture adjusting mechanism comprises a front air bag, a middle air bag, a front air pump, a rear air pump and a rear air bag; the fuselage comprises a front fuselage and a rear fuselage;
the adsorption mechanism is connected with one ends of the front air bags, the other ends of the front air bags are connected with one end of the front machine body, the other end of the front machine body is connected with one ends of the middle air bags, the other ends of the middle air bags are connected with one end of the rear machine body, and the other end of the rear machine body is connected with the rear air bags; the front air bag, the middle air bag and the rear air bag are the same in number and opposite in position in sequence;
the power driving mechanisms are arranged in the front machine body and the rear machine body; the number of the front air pumps is multiple and is the same as that of the front air bags and the middle air bags, the front air pumps are arranged on the front machine body, and two first air vents of the front air pumps are respectively connected with the front air bags and the middle air bags;
the number of the rear air pumps is multiple and is the same as that of the middle air bags and the rear air bags, the rear air pumps are arranged on the rear machine body, and two second air ports of the rear air pumps are respectively connected with the middle air bags and the rear air bags; in an initial state, the front airbag, the middle airbag and the rear airbag are filled with air.
Furthermore, the adsorption mechanism comprises a flexible sucker, a valve plate, a connecting rod, a valve seat, an electromagnet and a mounting rack, one end of the valve seat is connected with one end of the front airbags, and the other end of the valve seat is connected with the flexible sucker; the other end of the valve seat is provided with the mounting frame, the electromagnet is mounted on the mounting frame, and the electromagnet is positioned in the flexible sucker;
the valve seat is provided with a water inlet communicated with the interior of the machine body mechanism, the valve plate is movably arranged in the valve seat and used for closing/opening the water inlet, the valve plate is connected with the connecting rod, and the connecting rod is arranged in the flexible sucker; the flexible sucker can stretch out and draw back, and the connecting rod and the valve plate move relative to the valve seat along with the stretching of the flexible sucker so as to open/close the water inlet hole.
Further, the drilling mechanism comprises a motor, a drill bit, a spring and a clamping jaw, the motor is mounted on the mounting frame, an output shaft of the motor is movably matched and connected with a handle part of the drill bit, the handle part of the drill bit is of a hollow structure, and the spring is arranged in the handle part of the drill bit; two ends of the spring are respectively connected with an output shaft of the motor and the drill bit; the outer surface of the handle part of the drill bit is provided with a jaw groove, and one end of the jaw is elastically and rotatably connected with one end, close to the drill bit, of the jaw groove; the jaws are flared relative to the shank of the drill bit.
Further, the motor is a double-head output motor, an output shaft of the double-head output motor is movably matched and connected with the handle part of the drill bit, and another output shaft of the double-head output motor is connected with the propeller.
Furthermore, the explosive bags are arranged on the front machine body and the rear machine body.
The combat equipment is submerged in water, the combat equipment is driven to move in the water through the power driving mechanism, and in an initial state, the front air bag, the middle air bag and the rear air bag are filled with air, wherein the folded parts are in a folded and contracted state. The front air pump is used for inflating the air in the front air bag into the middle air bag, so that the air amount in the middle air bags is different, and the middle air bags are bent; air in the gasbag is inflated to the back gasbag in with the centre through back air pump to make the air capacity in a plurality of back gasbags different, a plurality of back gasbags take place the bending, so in order to realize the change of operation equipment gesture, make operation equipment can follow not equidirectional motion, the flexibility ratio is high.
When the combat equipment is close to the enemy ship body, the combat equipment is effectively adsorbed on the enemy ship body through the adsorption mechanism, and after adsorption, the enemy ship body is drilled and damaged through the drilling mechanism. Meanwhile, in the working process of the drilling mechanism and the adsorption mechanism, the front air pump and the rear air pump act to completely inflate the air in the front air bag and the middle air bag into the rear air bag, so that the fold parts are outwards unfolded, the area of the blocking mechanism is greatly increased, the blocking mechanism can provide great resistance when an enemy ship body runs, the enemy ship body is difficult to run, and therefore when a plurality of combat equipment simultaneously attacks the enemy ship body, the enemy ship body can not run quickly, and the damage degree of the enemy ship body is greatly increased.
The invention has simple integral structure, effectively reduces the manufacturing cost, and simultaneously adopts low-price combat equipment to attack the expensive hull of the enemy, so that the enemy economy is greatly damaged.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts.
Fig. 1 is a perspective view of the present invention.
Fig. 2 is a perspective view of fig. 1 cut away.
Fig. 3 is a perspective view of the suction mechanism and the drilling mechanism of fig. 1.
Fig. 4 is a partial perspective view of fig. 3.
Fig. 5 is a perspective view of fig. 3 cut away.
FIG. 6 is a perspective view of a plurality of rear airbags of the present invention.
Detailed Description
The following detailed description of the present invention is given for the purpose of better understanding technical solutions of the present invention by those skilled in the art, and the present description is only exemplary and explanatory and should not be construed as limiting the scope of the present invention in any way.
It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, it need not be further defined and explained in subsequent figures.
It is to be understood that the terms "center," "upper," "lower," "left," "right," "vertical," "horizontal," "inner," "outer," and the like are used in a generic and descriptive sense only and not for purposes of limitation, the terms "center," "upper," "lower," "left," "right," "vertical," "horizontal," "inner," "outer," and the like are used in the generic and descriptive sense only and not for purposes of limitation, as the term is used in the generic and descriptive sense, and not for purposes of limitation, unless otherwise specified or implied, and the specific reference to a device or element is intended to be a reference to a particular element, structure, or component. Furthermore, the terms "first," "second," "third," and the like are used solely to distinguish one from another and are not to be construed as indicating or implying relative importance.
Furthermore, the terms "horizontal", "vertical", "overhang" and the like do not imply that the components are required to be absolutely horizontal or overhang, but may be slightly inclined. For example, "horizontal" merely means that the direction is more horizontal than "vertical" and does not mean that the structure must be perfectly horizontal, but may be slightly inclined.
In the description of the present invention, it should also be noted that, unless otherwise explicitly specified or limited, the terms "disposed," "mounted," "connected," and "connected" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
As shown in fig. 1 to 6, the present embodiment provides a combat equipment, which includes a body mechanism 1, an adsorption mechanism 4, a drilling mechanism 5, a power driving mechanism 2, and an explosive charge 6, wherein the power driving mechanism 2 includes a driving motor 21, a mounting seat 20, and a propeller 22, the power driving mechanism 2 is located inside the body mechanism 1, and the mounting seat 20 is connected to the body mechanism 1; the driving motor 21 is mounted on the mounting base 20, the propeller 22 is connected with the driving motor 21, and the liquid in the machine body mechanism 1 flows backwards from the front of the machine body mechanism 1; the adsorption mechanism 4 is installed in front of the machine body mechanism 1, and the drilling mechanism 5 is installed in the adsorption mechanism 4; the explosive bag 6 is arranged on the machine body mechanism 1.
In the use of the present embodiment, the combat equipment is submerged in water, and the power drive mechanism 2 drives the combat equipment to move in the water, specifically, the drive motor 21 drives the propeller 22 to move, so that water flows in from the front inside the body mechanism 1 and is discharged from the rear. When the combat equipment is close to the enemy ship body, the combat equipment is effectively adsorbed on the enemy ship body through the adsorption mechanism 4, and after adsorption, the enemy ship body is drilled and destroyed through the drilling mechanism 5. When the combat equipment is attached to the enemy hull, the explosive charge 6 is activated to destroy the enemy hull, so that the enemy hull is completely destroyed.
Further preferably, the combat equipment of the present embodiment further comprises a posture adjusting mechanism, wherein the posture adjusting mechanism comprises a front air bag 30, a middle air bag 31, a front air pump 33, a rear air pump 34 and a rear air bag 32; the machine body mechanism 1 comprises a front machine body 10 and a rear machine body 11,
the adsorption mechanism 4 is connected with one end of the plurality of front airbags 30, the other end of the plurality of front airbags 30 is connected with one end of the front body 10, the other end of the front body 10 is connected with one end of the plurality of middle airbags 31, the other end of the plurality of middle airbags 31 is connected with one end of the rear body 11, and the other end of the rear body 11 is connected with the plurality of rear airbags 32; the front air bags 30, the middle air bags 31 and the rear air bags 32 are the same in number and opposite in position in sequence;
the power driving mechanism 2 is arranged in the front machine body 10 and the rear machine body 11; the number of the front air pumps 33 is multiple and is the same as that of the front air bags 30 and the middle air bags 31, the front air pumps 33 are installed on the front fuselage 10, and two first air vents of the front air pumps 33 are respectively connected with the front air bags 30 and the middle air bags 31;
the number of the rear air pumps 34 is multiple and is the same as that of the middle air bags 31 and the rear air bags 32, the rear air pumps 34 are installed on the rear machine body 11, and two second air vents of the rear air pumps 34 are respectively connected with the middle air bags 31 and the rear air bags 32; in the initial state, the front airbag 30, the intermediate airbag 31, and the rear airbag 32 are filled with air.
In the initial state of the present embodiment, the front airbag 30, the intermediate airbag 31, and the rear airbag 32 are filled with air. The air in the front airbag 30 is re-inflated into the middle airbag 31 by the front air pump 33 so that the air amount in the plurality of middle airbags 31 is different and the plurality of middle airbags 31 are curved, and correspondingly, the air in the middle airbag 31 is re-inflated into the front airbag 30 by the front air pump 33 so that the air amount in the plurality of front airbags 30 is different and the plurality of front airbags 30 are curved; air in the gasbag 31 is changeed to the back gasbag 32 in with middle through back air pump 34 to make the air volume in a plurality of back gasbags 32 different, a plurality of back gasbags 32 take place to buckle, so in order to realize the change of combat equipment gesture, make combat equipment can follow not equidirectional motion, the flexibility ratio is high.
In this embodiment, it is preferable that the number of the driving motors 21 and the propellers 22 in the front body 10 and the rear body 11 is two, and the two driving motors 21 are installed on both sides of the mounting base 20 to increase the driving force of the power driving mechanism 2.
Further preferably, the suction mechanism 4 includes a flexible suction cup 40, a valve plate 42, a connecting rod 43, a valve seat 41, an electromagnet 44, and a mounting bracket 45, wherein one end of the valve seat 41 is connected to one end of the front airbags 30, and the other end of the valve seat 41 is connected to the flexible suction cup 40; the other end of the valve seat 41 is provided with the mounting rack 45, the electromagnet 44 is mounted on the mounting rack 45, and the electromagnet 44 is positioned in the flexible sucker 40; the valve seat 41 is provided with a water inlet 410 hole communicated with the interior of the machine body mechanism 1, the valve plate 42 is movably arranged in the valve seat 41 and is used for closing/opening the water inlet 410, the valve plate 42 is connected with the connecting rod 43, and the connecting rod 43 is arranged in the flexible sucker 40; the flexible suction cup 40 can be extended and contracted, and the connecting rod 43 and the valve plate 42 move relative to the valve seat 41 as the flexible suction cup 40 is extended and contracted to open/close the water inlet hole 410. Wherein the valve seat 41 is provided with a moving groove 411 matched with the valve plate 42.
In the embodiment, when the combat equipment is not in contact with the enemy ship, the flexible suction cup 40 is in a natural state, the water inlet hole 410 is in an open state, the power driving mechanism 2 works, and water enters from the central hole 410 of the flexible suction cup 40 and is discharged through the valve seat 41, the front air bag 30, the front body 10, the middle air bag 31, the rear body 11 and the rear air bag 32. When the power driving mechanism 2 is driven to the state that the adsorption mechanism 4 is in contact with the surface of the enemy ship, as the combat equipment continues to move towards the enemy ship, the flexible suction cups 40 are compressed, and as the flexible suction cups 40 are compressed, the connecting rods 43 and the valve plates 42 move relative to the valve seats 41 to close the water inlet holes 410, at this time, water can only flow in from the central holes of the flexible suction cups 40, so that the flexible suction cups 40 can be adsorbed on the enemy ship. Meanwhile, along with the compression of the flexible sucker 40, the electromagnet 44 can expose out of the surface of the flexible sucker 40, and the electromagnet 44 adsorbs the enemy ship body, so that the enemy ship body can be effectively adsorbed on the enemy ship body under the double adsorption action of the flexible sucker 40 and the electromagnet 44. In the present embodiment, the valve seat 41 is preferably provided with a plurality of water inlet holes 410, and a plurality of water inlet holes are provided corresponding to the number of the valve plates 42 and the connecting rods 43.
The embodiment further preferably includes that the drilling mechanism 5 includes a motor 50, a drill bit 51, a spring 53, and a latch 52, the motor 50 is mounted on the mounting frame 45, an output shaft of the motor 50 is movably connected with a handle of the drill bit 51 in a matching manner, the handle of the drill bit 51 is hollow, and the spring 53 is disposed in the handle of the drill bit 51; two ends of the spring 53 are respectively connected with the output shaft of the motor 50 and the drill bit 51; the outer surface of the handle of the drill bit 51 is provided with a jaw groove 510, and one end of the jaw 52 is elastically and rotatably connected with one end of the jaw groove 510 close to the drill bit 51; the jaws 52 are flared relative to the shank of the drill bit 51.
This embodiment is when adsorption apparatus 4 adsorbs on the enemy hull, and flexible suction cup 40 can be compressed, and along with the compression of flexible suction cup 40, drill bit 51 can expose flexible suction cup 40's surface, and motor 50 starts to drive drill bit 51 and rotates this moment to drill bit 51 is gone into to the enemy hull, and after drill bit 51 went into the enemy hull, jack catch 52 card was on the enemy hull, makes the equipment of fighting effectively fix on the enemy hull. In the embodiment, the output shaft of the motor 50 is elastically connected with the drill 51 through the spring 53 to play a role of floating drilling, so that the drill 51 is prevented from being broken when drilling due to rigid connection. In particular, the output shaft of the motor 50 is inserted into the handle of the drill 51, wherein the output shaft of the motor 50 and the handle of the drill 51 are provided with a limiting part, so that the output shaft of the motor 50 can only be limited in the handle of the drill 51.
In this embodiment, the motor 50 is preferably a double-head output motor, one output shaft of the double-head output motor is movably connected with the handle of the drill 51 in a matching manner, and the other output shaft of the double-head output motor is connected with the propeller 22.
In this embodiment, preferably, the explosive packs 6 are mounted on both the front body 10 and the rear body 11.
This embodiment of course also includes a power supply for supplying power to the drive motor 21, the motor 50, the electromagnet 44, and the like, and a switch for controlling energization of the power supply; the ignition device for igniting the explosive package 6 is also included, which is conventional in the art, and is not essential to the present embodiment, and thus will not be described in detail.
It should be noted that, in this document, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
The foregoing shows and describes the general principles, essential features, and advantages of the invention. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, which are given by way of illustration of the principles of the present invention, and that various changes and modifications may be made without departing from the spirit and scope of the invention as defined by the appended claims. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (6)
1. The combat equipment is characterized by comprising a machine body mechanism, an adsorption mechanism, a drilling mechanism, a power driving mechanism and an explosive package, wherein the power driving mechanism comprises a driving motor, a mounting seat and a propeller, the power driving mechanism is positioned in the machine body mechanism, and the mounting seat is connected with the machine body mechanism; the driving motor is arranged on the mounting seat, the propeller is connected with the driving motor, and the liquid in the machine body mechanism flows backwards from the front of the machine body mechanism; the adsorption mechanism is arranged in front of the machine body mechanism, and the drilling mechanism is arranged in the adsorption mechanism; the explosive bag is arranged on the machine body mechanism.
2. The combat equipment of claim 1, further comprising a posture adjustment mechanism comprising a front air bag, a middle air bag, a front air pump, a rear air bag; the fuselage comprises a front fuselage and a rear fuselage;
the adsorption mechanism is connected with one ends of the front air bags, the other ends of the front air bags are connected with one end of the front machine body, the other end of the front machine body is connected with one ends of the middle air bags, the other ends of the middle air bags are connected with one end of the rear machine body, and the other end of the rear machine body is connected with the rear air bags; the front air bag, the middle air bag and the rear air bag are the same in number and opposite in position in sequence;
the power driving mechanisms are arranged in the front machine body and the rear machine body; the number of the front air pumps is multiple and is the same as that of the front air bags and the middle air bags, the front air pumps are arranged on the front machine body, and two first air vents of the front air pumps are respectively connected with the front air bags and the middle air bags;
the number of the rear air pumps is multiple and is the same as that of the middle air bags and the rear air bags, the rear air pumps are arranged on the rear machine body, and two second air ports of the rear air pumps are respectively connected with the middle air bags and the rear air bags; in an initial state, the front airbag, the middle airbag and the rear airbag are filled with air.
3. The combat equipment of claim 2, wherein the suction mechanism comprises a flexible sucker, a valve plate, a connecting rod, a valve seat, an electromagnet and a mounting frame, one end of the valve seat is connected with one ends of the front airbags, and the other end of the valve seat is connected with the flexible sucker; the other end of the valve seat is provided with the mounting frame, the electromagnet is mounted on the mounting frame, and the electromagnet is positioned in the flexible sucker;
the valve seat is provided with a water inlet communicated with the interior of the machine body mechanism, the valve plate is movably arranged in the valve seat and used for closing/opening the water inlet, the valve plate is connected with the connecting rod, and the connecting rod is arranged in the flexible sucker; the flexible sucker can stretch out and draw back, and the connecting rod and the valve plate move relative to the valve seat along with the stretching of the flexible sucker so as to open/close the water inlet hole.
4. The combat equipment of claim 3, wherein the drilling mechanism comprises a motor, a drill bit, a spring and a claw, the motor is mounted on the mounting frame, an output shaft of the motor is movably matched and connected with a handle part of the drill bit, the handle part of the drill bit is of a hollow structure, and the spring is arranged in the handle part of the drill bit; two ends of the spring are respectively connected with an output shaft of the motor and the drill bit; the outer surface of the handle part of the drill bit is provided with a jaw groove, and one end of the jaw is elastically and rotatably connected with one end, close to the drill bit, of the jaw groove; the jaws are flared relative to the shank of the drill bit.
5. The combat equipment of claim 4, wherein the motor is a double-ended output motor, one output shaft of the double-ended output motor being movably coupled to the handle portion of the drill head, the other output shaft of the double-ended output motor being coupled to the propeller.
6. A combat equipment according to claim 2 wherein said explosives are mounted on both said front and rear bodies.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN202011416053.3A CN112484576A (en) | 2020-12-07 | 2020-12-07 | Fighting equipment |
Applications Claiming Priority (1)
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CN202011416053.3A CN112484576A (en) | 2020-12-07 | 2020-12-07 | Fighting equipment |
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CN112484576A true CN112484576A (en) | 2021-03-12 |
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CN202011416053.3A Withdrawn CN112484576A (en) | 2020-12-07 | 2020-12-07 | Fighting equipment |
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Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA2278111A1 (en) * | 1999-07-21 | 2001-01-21 | Michael Cyril Bowditch Stacey | Hull penetration system |
CN103112568A (en) * | 2012-12-21 | 2013-05-22 | 浙江建林电子电气有限公司 | Flexible aggressive mechanical octopus |
KR20150009081A (en) * | 2013-07-15 | 2015-01-26 | 대우조선해양 주식회사 | Apparatus for attacking propeller of enemy |
CN105730541A (en) * | 2016-03-17 | 2016-07-06 | 上海交通大学 | Pneumatic multi-bag type soft wall-climbing robot and control method thereof |
CN106184663A (en) * | 2016-07-20 | 2016-12-07 | 张学衡 | A kind of submarine patrol BFR |
CN106378764A (en) * | 2016-10-12 | 2017-02-08 | 盐城工学院 | Driving device and mobile robot |
CN206939005U (en) * | 2017-05-24 | 2018-01-30 | 大鹏高科(武汉)智能装备有限公司 | A kind of unmanned boat of auxiliary catch enemy ship |
CN108100191A (en) * | 2017-12-21 | 2018-06-01 | 大连厚德坤泰管理咨询有限公司 | Full attitude motion underwater robot |
CN109795647A (en) * | 2019-01-29 | 2019-05-24 | 山东大学 | Electromagnetic adsorption-thrust by airscrew underwater cleaning robot |
CN210581826U (en) * | 2019-08-20 | 2020-05-22 | 深圳市呵康科技有限公司 | Air mattress |
-
2020
- 2020-12-07 CN CN202011416053.3A patent/CN112484576A/en not_active Withdrawn
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA2278111A1 (en) * | 1999-07-21 | 2001-01-21 | Michael Cyril Bowditch Stacey | Hull penetration system |
CN103112568A (en) * | 2012-12-21 | 2013-05-22 | 浙江建林电子电气有限公司 | Flexible aggressive mechanical octopus |
KR20150009081A (en) * | 2013-07-15 | 2015-01-26 | 대우조선해양 주식회사 | Apparatus for attacking propeller of enemy |
CN105730541A (en) * | 2016-03-17 | 2016-07-06 | 上海交通大学 | Pneumatic multi-bag type soft wall-climbing robot and control method thereof |
CN106184663A (en) * | 2016-07-20 | 2016-12-07 | 张学衡 | A kind of submarine patrol BFR |
CN106378764A (en) * | 2016-10-12 | 2017-02-08 | 盐城工学院 | Driving device and mobile robot |
CN206939005U (en) * | 2017-05-24 | 2018-01-30 | 大鹏高科(武汉)智能装备有限公司 | A kind of unmanned boat of auxiliary catch enemy ship |
CN108100191A (en) * | 2017-12-21 | 2018-06-01 | 大连厚德坤泰管理咨询有限公司 | Full attitude motion underwater robot |
CN109795647A (en) * | 2019-01-29 | 2019-05-24 | 山东大学 | Electromagnetic adsorption-thrust by airscrew underwater cleaning robot |
CN210581826U (en) * | 2019-08-20 | 2020-05-22 | 深圳市呵康科技有限公司 | Air mattress |
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