CN211863851U - Model airplane remote control aircraft capable of floating on water surface and preventing sinking - Google Patents

Model airplane remote control aircraft capable of floating on water surface and preventing sinking Download PDF

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Publication number
CN211863851U
CN211863851U CN201922423737.5U CN201922423737U CN211863851U CN 211863851 U CN211863851 U CN 211863851U CN 201922423737 U CN201922423737 U CN 201922423737U CN 211863851 U CN211863851 U CN 211863851U
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CN
China
Prior art keywords
fixedly connected
gasbag
water
storehouse
fuselage
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Expired - Fee Related
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CN201922423737.5U
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Chinese (zh)
Inventor
赵传生
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Huai'an Tiandao Technology Innovation Co ltd
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Huai'an Tiandao Technology Innovation Co ltd
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Priority to CN201922423737.5U priority Critical patent/CN211863851U/en
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Publication of CN211863851U publication Critical patent/CN211863851U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a but surface of water floats prevents sinking model aeroplane and model ship remote control aircraft, the reciprocating impact tunnel drilling machine comprises a machine body, the top fixedly connected with waterproof cover of wing device, the bottom fixedly connected with water logging sensor device of undercarriage base, the bottom fixedly connected with gasbag storehouse in gasbag storehouse, the inside swing joint in gasbag storehouse has the gasbag, the outside swing joint in gasbag storehouse has gasbag storehouse board. This but surface of water floats prevents sinking model aeroplane and model ship remote control aircraft device is provided with gas pitcher storehouse and gasbag storehouse, when remote control aircraft fell on the surface of water, water sensor device give-out order, gas pitcher storehouse begins to aerify the gasbag, meanwhile, gasbag storehouse board begins to open, the gasbag is because the inflated reason, begin to the motion outside the gasbag storehouse, at this moment, the foam pad of water sensor device bottom is because the fuselage overweight begins to sink, the gasbag has been opened, the fuselage has been avoided soaking the loss that the aquatic brought for the user, remote control aircraft's practicality has been improved greatly.

Description

Model airplane remote control aircraft capable of floating on water surface and preventing sinking
Technical Field
The utility model relates to a remote control aircraft technical field specifically is a but surface of water floats prevents sinking model aeroplane and model ship remote control aircraft.
Background
With the development of science and technology, the science and technology content of the remote control plane is greatly improved, the cost is lowered greatly than before, the number of users of the remote control plane is increased, the control mode of the remote control plane is complex, more common remote control planes with 4 channels and 6 channels are more common, manufacturers of the remote control plane are more, therefore, even if the maneuvering performances of the remote control plane are similar, various control parts on the remote control plane such as a steering engine, a tail wing, an aileron and the like are similar, the specific control method by using the remote controller still has obvious difference, and the users are difficult to adapt to different remote control planes.
The existing remote control aircraft is also more and more widely applied in folk, the technology of the remote control aircraft is mature day by day, some remote control aircraft are specially used for lakes and sea level aerial photography, but if equipment faults are met in flight, the remote control aircraft can fall into water, the water can easily enter the motor from the joint, the motor is damaged, when people arrive, the aircraft body sinks into the water and is difficult to retrieve, in addition, when the remote control aircraft lands on the water surface, the aircraft body cannot stably land due to the small support, and certain influence is brought to the use of the aircraft body of the remote control aircraft.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a but surface of water floats prevents sinking model aeroplane and model ship remote control aircraft to solve the problem that proposes among the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: a remotely controlled model airplane capable of floating on water and preventing sinking comprises a fuselage, wherein first connecting seats are fixedly connected to two sides of the middle of the fuselage, connecting arms are fixedly connected to the outer sides of the first connecting seats, second connecting seats are fixedly connected to the right sides of the connecting arms, wing devices are fixedly connected to the right sides of the second connecting seats, waterproof cases are fixedly connected to the tops of the wing devices, rotating shafts are movably connected to the tops of the waterproof cases, wings are fixedly connected to the tops of the rotating shafts, third connecting seats are fixedly connected to the tops of the wings, a fuselage undercarriage is fixedly connected to the bottom of the wing devices, an undercarriage base is fixedly connected to the bottom of the fuselage undercarriage base, a water sensor device is fixedly connected to the bottom of the undercarriage base, connecting rods are fixedly connected to the bottoms of two sides of the fuselage, and air tank bins are fixedly mounted to the bottoms, the utility model discloses an air tank, including air tank storehouse, bottom fixedly connected with gasbag storehouse, the inside swing joint in gasbag storehouse has the gasbag, the outside swing joint in gasbag storehouse has gasbag storehouse board, the preceding bottom fixedly connected with connecting plate of fuselage, the automatically controlled cloud platform of bottom fixedly connected with of connecting plate, the bottom fixedly connected with camera device of automatically controlled cloud platform.
Preferably, the outer surface of the water sensor device is fixedly connected with foam.
Preferably, the side fixedly connected with heating panel of fuselage, the louvre has been seted up to the inside of heating panel, and the inside fixedly connected with waterproof filter screen of louvre.
Preferably, the number of the connecting arms and the wing devices is four.
Preferably, the top of the rotating shaft is fixedly connected with a third connecting seat.
Preferably, the connecting plate is fixedly connected with an air tank bin.
Preferably, the gas tank is wired to an internal battery of the fuselage.
Preferably, the outer surface of the fuselage is fixedly connected with a waterproof coating.
Preferably, the outer side of the air bag is movably connected with an air bag plug.
Compared with the prior art, the beneficial effects of the utility model are that:
(1) this but surface of water floats prevents sinking model aeroplane and model ship remote control aircraft device is provided with the undercarriage base, and undercarriage base area of contact is big, when remote control aircraft landing on the surface of water, can not because the base is tiny and unable stable descending, the bottom fixedly connected with water sensor device of undercarriage base, the surface of water sensor device has the foam pad, can ensure when remote control aircraft landing on the surface of water, can not fall into the aquatic at once, and the device has improved remote control aircraft's stability greatly.
(2) This but surface of water floats prevents sinking model aeroplane and model ship remote control aircraft device is provided with gas pitcher storehouse and gasbag storehouse, when remote control aircraft fell on the surface of water, water sensor device give-out order, convey to the gas pitcher storehouse, the gas pitcher storehouse begins to aerify the gasbag, meanwhile, gasbag storehouse board begins to open, the gasbag is because the inflated reason, begin to gasbag storehouse external motion, at this moment, the foam pad of water sensor device bottom begins to sink because the fuselage is overweight, the gasbag has been opened, the loss of having avoided the fuselage to soak the aquatic and bringing for the user, remote control aircraft's practicality has been improved greatly.
Drawings
FIG. 1 is a schematic front view of the present invention;
FIG. 2 is a schematic top view of the present invention;
fig. 3 is a schematic view of the internal structure of the bottom of the fuselage taken in fig. 1.
In the figure: the aircraft comprises a fuselage 1, a first connecting seat 2, a connecting arm 3, a second connecting seat 4, a wing device 5, a waterproof shell 6, a rotating shaft 7, a wing 8, a third connecting seat 9, a landing gear 10, a landing gear base 11, a water immersion sensor device 12, a connecting rod 13, an air tank bin 14, an air tank 15, an air bag bin 16, an air bag 17, an air bag bin plate 18, a connecting plate 19, an electric control cradle head 20 and a camera device 21.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-3, the present invention provides a technical solution: a model airplane remote control plane capable of floating on water and preventing sinking comprises a plane body 1, a waterproof coating is fixedly connected to the outer surface of the plane body 1, a heat radiation plate is fixedly connected to the side surface of the plane body 1, heat radiation holes are formed in the heat radiation plate, a waterproof filter screen is fixedly connected to the inside of each heat radiation hole, first connecting seats 2 are fixedly connected to two sides of the middle of the plane body 1, connecting arms 3 are fixedly connected to the outer sides of the first connecting seats 2, the number of the connecting arms 3 and the number of wing devices 5 are four respectively, a second connecting seat 4 is fixedly connected to the right side of each connecting arm 3, a wing device 5 is fixedly connected to the right side of each second connecting seat 4, a waterproof shell 6 is fixedly connected to the top of each wing device 5, a rotating shaft 7 is movably connected to the top of each waterproof shell 6, a third connecting seat 9 is fixedly connected to, the bottom of the wing device 5 is fixedly connected with a fuselage undercarriage 10, the bottom of the fuselage undercarriage 10 is fixedly connected with an undercarriage base 11, the contact area of the undercarriage base 11 is large, when the remote control aircraft falls on the water surface, the remote control aircraft cannot stably land because the base is small, the bottom of the undercarriage base 11 is fixedly connected with a water sensor device 12, the outer surface of the water sensor device 12 is provided with a foam cushion, the remote control aircraft cannot immediately fall into the water when falling on the water surface, the device greatly improves the stability of the remote control aircraft, the bottom of the undercarriage base 11 is fixedly connected with the water sensor device 12, the outer surface of the water sensor device 12 is fixedly connected with foam, the bottoms of two sides of the fuselage 1 are fixedly connected with connecting rods 13, the bottom of the connecting rods 13 is fixedly provided with an air tank bin 14, the inside of the air tank bin 14 is fixedly provided with an air tank 15, and the air, the bottom fixedly connected with gasbag storehouse 16 in gas tank storehouse 14, the inside swing joint in gasbag storehouse 16 has gasbag 17, the outside swing joint of gasbag 17 has the gasbag stopper, the outside swing joint in gasbag storehouse 16 has gasbag storehouse board 18, the preceding bottom fixedly connected with connecting plate 19 of fuselage 1, connecting plate 19 fixedly connected with gas tank storehouse 14, the automatically controlled cloud platform 20 of bottom fixedly connected with of connecting plate 19, the bottom fixedly connected with camera device 21 of automatically controlled cloud platform 20.
The working principle is as follows: before the model airplane remote control device capable of floating on water and preventing sinking is used, gas in an air bag 17 is discharged firstly, the air bag 17 is folded and placed in an air bag bin 16, an air bag bin plate 18 is covered, when the device falls on the water surface, a water logging sensor device 12 sends an instruction and transmits the instruction to an air tank bin 14, the air tank bin 14 starts to inflate the air bag 17, meanwhile, the air bag bin plate 18 starts to be opened, the air bag 17 starts to move out of the air bag bin 16 due to the inflation reason, at the moment, a foam pad at the bottom of the water logging sensor device 12 starts to sink due to the fact that a machine body 1 is overweight, at the moment, the air bag 17 is opened, the air tank 15 is inflated subsequently, and when the air tank 15 can support the whole machine body 1, the air tank 15 stops working.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims (9)

1. The utility model provides a but surface of water floats prevents sinking model aeroplane and model ship remote control aircraft, includes fuselage (1), its characterized in that: the aircraft comprises a fuselage (1), a first connecting seat (2) is fixedly connected to two sides of the middle of the fuselage (1), a connecting arm (3) is fixedly connected to the outer side of the first connecting seat (2), a second connecting seat (4) is fixedly connected to the right side of the connecting arm (3), a wing device (5) is fixedly connected to the right side of the second connecting seat (4), a waterproof shell (6) is fixedly connected to the top of the wing device (5), a rotating shaft (7) is movably connected to the top of the waterproof shell (6), a wing (8) is fixedly connected to the top of the rotating shaft (7), a third connecting seat (9) is fixedly connected to the top of the wing (8), a fuselage undercarriage (10) is fixedly connected to the bottom of the wing device (5), a base (11) is fixedly connected to the bottom of the fuselage undercarriage (10), and a water logging sensor device (12) is fixedly connected to the, the utility model discloses an electronic control camera, including fuselage (1), both sides bottom fixedly connected with connecting rod (13), the bottom fixed mounting of connecting rod (13) has tank storehouse (14), the inside fixed mounting of tank storehouse (14) has gas pitcher (15), the bottom fixedly connected with gasbag storehouse (16) of tank storehouse (14), the inside swing joint in gasbag storehouse (16) has gasbag (17), the outside swing joint in gasbag storehouse (16) has gasbag storehouse board (18), the preceding bottom fixedly connected with connecting plate (19) of fuselage (1), the automatically controlled cloud platform (20) of bottom fixedly connected with of connecting plate (19), the bottom fixedly connected with camera device (21) of automatically controlled cloud platform (20).
2. The water-floatable anti-sinking model airplane telecontroller according to claim 1, wherein: and the outer surface of the water sensor device (12) is fixedly connected with foam.
3. The water-floatable anti-sinking model airplane telecontroller according to claim 1, wherein: the side fixedly connected with heating panel of fuselage (1), the louvre has been seted up to the inside of heating panel, the inside fixedly connected with waterproof filter screen of louvre.
4. The water-floatable anti-sinking model airplane telecontroller according to claim 1, wherein: the number of the connecting arms (3) and the number of the wing devices (5) are four respectively.
5. The water-floatable anti-sinking model airplane telecontroller according to claim 1, wherein: the top of the rotating shaft (7) is fixedly connected with a third connecting seat (9).
6. The water-floatable anti-sinking model airplane telecontroller according to claim 1, wherein: the connecting plate (19) is fixedly connected with an air tank bin (14).
7. The water-floatable anti-sinking model airplane telecontroller according to claim 1, wherein: the gas tank (15) is connected with an internal battery wire of the machine body (1).
8. The water-floatable anti-sinking model airplane telecontroller according to claim 1, wherein: the outer surface of the machine body (1) is fixedly connected with a waterproof coating.
9. The water-floatable anti-sinking model airplane telecontroller according to claim 1, wherein: the outer side of the air bag (17) is movably connected with an air bag plug.
CN201922423737.5U 2019-12-29 2019-12-29 Model airplane remote control aircraft capable of floating on water surface and preventing sinking Expired - Fee Related CN211863851U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201922423737.5U CN211863851U (en) 2019-12-29 2019-12-29 Model airplane remote control aircraft capable of floating on water surface and preventing sinking

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201922423737.5U CN211863851U (en) 2019-12-29 2019-12-29 Model airplane remote control aircraft capable of floating on water surface and preventing sinking

Publications (1)

Publication Number Publication Date
CN211863851U true CN211863851U (en) 2020-11-06

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201922423737.5U Expired - Fee Related CN211863851U (en) 2019-12-29 2019-12-29 Model airplane remote control aircraft capable of floating on water surface and preventing sinking

Country Status (1)

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CN (1) CN211863851U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112918664A (en) * 2021-03-12 2021-06-08 中航西飞民用飞机有限责任公司 Overwater floating balance structure and method for upper single-wing aircraft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112918664A (en) * 2021-03-12 2021-06-08 中航西飞民用飞机有限责任公司 Overwater floating balance structure and method for upper single-wing aircraft

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Granted publication date: 20201106