CN2626857Y - Floating ball cabin of retractable satellite receiving/emitting antenna for submergence - Google Patents
Floating ball cabin of retractable satellite receiving/emitting antenna for submergence Download PDFInfo
- Publication number
- CN2626857Y CN2626857Y CN 03259305 CN03259305U CN2626857Y CN 2626857 Y CN2626857 Y CN 2626857Y CN 03259305 CN03259305 CN 03259305 CN 03259305 U CN03259305 U CN 03259305U CN 2626857 Y CN2626857 Y CN 2626857Y
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- China
- Prior art keywords
- cabin
- antenna
- ball float
- satellite
- dual
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- Expired - Fee Related
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Abstract
The utility model relates to a planet emitting/receiving antenna floating ball cabin for marine use, the emitting/receiving antenna carrier capable of diving deeply and resisting pressure and suitable for communication engineering antenna floating ball cabin of underwater human-carrying establishment such as underwater viewing marine, human-carrying deep sea detector and underwater life boat. The carrier includes an emitting/receiving antenna, a longitudinal horizontal ring, a longitudinal horizontal shaft, a transverse horizontal ring, a transverse horizontal shaft, an antenna base horizontal platform, a platform shaft, an in-cabin planet emitting/receiving feed line interface, a space cabin, an electric heating dehumidity drier, a floating cabin, a float ball cabin, a holding-releasing pulling ring, a ring-shaped wave-preventing stabilizing ring, a float ball shell, a waterproof and pressure-resisting high frequency plug at outside of the float ball cabin, a holding-releasing assembled cable for the planet antenna floating cabin, an upper-lower balls connecting wire, and a sealed water-proof rubber ring. The float ball shell is composed of an upper and a lower semispherical shell, and a rotating damping bar made of hydrophilic material is provided at lower part of the float ball shell. The planet antenna floating cabin holding-releasing assembled cable is composed of a steel cable, an emitting/receiving optical fiber transmission wire, a planet positioning feed line, and a drier low voltage power supply wire.
Description
Technical field
What relate to retractable formula satellite dual-mode antenna ball float cabin is the withstand voltage retractable formula of a kind of deep diving antenna carrier but the utility model is dived, and is applicable under water tour submarine, manned deep ocean survey vechicle, the communication engineering antenna ball float cabin body of manned facility under water such as life boat under water.
Background technology
Underwater communication at present mainly is long-wave communication, underwater sound communication and cable wire communication.Because long-wave communication equipment is huge, also only can be by bank station to the unidirectional logical communication of broadcasting under water, underwater sound communication and cable wire communication distance are too short.
Summary of the invention
But the purpose of this utility model is to provide a kind of latent usefulness retractable formula satellite dual-mode antenna ball float cabin at above-mentioned weak point, communication antenna equipment such as small-sized shortwave, ultrashort waves, satellite dual-mode antenna, satellite positioning antenna can be made to put in the ball float as antenna carrier in this antenna ball float cabin, thereby the increase communication distance has solved the difficult problem of underwater communication, two way communication under water.
Latent usefulness can be received, putting formula satellite dual-mode antenna ball float cabin takes following scheme to realize: latent usefulness can be received, put formula satellite dual-mode antenna ball float cabin and comprise dual-mode antenna, the vertical equity circle, the vertical equity axle, the transverse horizontal circle, transverse horizontal axis, the antenna mounting horizontal stand, platform axle, satellite transmitting-receiving feeder line interface in the cabin, the cabin, space, electrical warming removal moisture drying device, buoyancy compartment, ball float cabin folding and unfolding draw ring, the annular wave resistance waves stabilization ring, the ball float shell, the withstand voltage out of my cabin waterproof High-frequency plug of ball float, satellite antenna buoyancy compartment folding and unfolding combination cable, last lower sphere connection lead, the water-tight cushion rubber.The ball float shell is provided with disjunctor annular wave resistance and waves stabilization ring.The ball float shell is made up of upper and lower hemisphere housing, between the upper and lower hemisphere housing water-tight cushion rubber is housed, ball float shell lower semisphere housing line of centers two end devices have vertical equity axle and vertical equity circle, by vertical equity circle line of centers two end devices transverse horizontal axis is arranged, device has the transverse horizontal circle on the transverse horizontal axis, line of centers two ends by the transverse horizontal circle are connected with the antenna platform axle again, the antenna platform shaft device has the antenna mounting horizontal stand, make the antenna mounting horizontal stand when wave waves, keep horizontality, make and dive and dual-mode antenna energy normal operation.Can dual-mode antenna be arranged device on the antenna mounting horizontal stand, dual-mode antenna comprises the active satellite dual-mode antenna, grapefruit satellite antenna, satellite positioning antenna and other antennas, termination feeder line (in the cabin) under the antenna mounting horizontal stand, ball float shell the latter half is the cabin, space, electric drying apparatus is equipped with in space bilge portion, prevents the gathering of condensed water.Buoyancy compartment is located in the cabin, space, buoyancy compartment is the vacuum buoyancy compartment, in be provided with the triangle reinforced rib, ball float shell the latter half outer casing bottom has ball float cabin folding and unfolding draw ring, and ball float out of my cabin device withstand voltage waterproof High-frequency plug or fiber-optical socket are arranged, device has satellite antenna buoyancy compartment folding and unfolding combination cable, have withstand voltage, pulling force is strong, the certain softness of tool, constitute by wirerope transmitting-receiving optical fiber transmission line, satellite positioning feeder line, moisture separator low potential source line.
Principle of work: during use, but by folding and unfolding satellite cable will dive climb up on top of the water with retractable formula satellite dual-mode antenna ball float cabin on, by satellite retractable equipment in the ships and light boats electric signal is radiated the work that communicates on the Aerospace Satellite by the satellite dual-mode antenna that feeder line is transferred in the ball float cabin, antenna or other antenna transmission are inside and outside on the reception facilities in the cabin via satellite carries out two way communication for the external communication electric signal.Be recoverable to when not using, do not influence navigation, recovery place on the ship should have the identical half slot of ball float shell lower semisphere part, pastes after the buoyancy spheroid reclaims and obeys in groove and fastening, does not influence navigation.
But dive with the advantage in retractable formula satellite dual-mode antenna ball float cabin:
1, can take multiple means of communication to solve underwater communication.
2, solve the difficult problem of two way communication.
3, can solve face-to-face communication.
4, the aquanaut can see satellite television, increase work and sightseeing enjoyment, adjusting aquanaut, traveller's nervous psychology.
Description of drawings
The utility model is described in further detail below with reference to accompanying drawing.
But Fig. 1 dives with retractable formula satellite dual-mode antenna ball float cabin structure scheme drawing.
But Fig. 2 dives with retractable formula satellite dual-mode antenna ball float cabin birds-eye view.
The specific embodiment
With reference to accompanying drawing 1,2, latent usefulness can be received, put formula satellite dual-mode antenna ball float cabin structure and comprise dual-mode antenna 1, vertical equity axle 3, vertical equity circle 22, transverse horizontal circle 23, transverse horizontal axis 4, antenna mounting horizontal stand 5, platform axle 24, satellite transmitting-receiving feeder line interface 6 in the cabin, cabin, space 7, electrical warming removal moisture drying device 9, be connected with moisture separator power lead 8, buoyancy compartment 11, ball float cabin folding and unfolding draw ring 13, the annular wave resistance waves stabilization ring 14, ball float shell 15, the withstand voltage out of my cabin waterproof High-frequency plug 16 of ball float, satellite antenna buoyancy compartment folding and unfolding combination cable 17, last lower sphere connection lead 18, water-tight cushion rubber 19.Ball float shell 15 is provided with disjunctor annular wave resistance and waves stabilization ring 14.Ball float shell 15 is by last, the lower semisphere housing is formed, fix by last lower house binding bolt 20, on, water-tight cushion rubber 19 is housed between the lower semisphere housing, ball float shell lower semisphere housing line of centers two end devices have vertical equity axle 3 and vertical equity circle 22, by vertical equity circle 22 line of centerss two end devices transverse horizontal axis 4 is arranged, device has transverse horizontal circle 23 on the transverse horizontal axis 4, line of centers two ends by transverse horizontal circle 23 are connected with antenna platform axle 24 again, antenna platform axle 24 devices have antenna mounting horizontal stand 5, make antenna mounting horizontal stand 5 when wave waves, keep horizontality, make and dive and dual-mode antenna energy normal operation.Can dual-mode antenna be arranged device on the antenna mounting horizontal stand 5, dual-mode antenna comprises active satellite dual-mode antenna 1, grapefruit satellite antenna, satellite positioning antenna 2 and other antennas.Device has the automatic tracking servosystem on the antenna mounting horizontal stand 5.5 times termination feeder lines of antenna mounting horizontal stand (in the cabin), ball float shell lower semisphere partly are the cabin, space, and electric drying apparatus 9 is equipped with in bilge portion in space, prevents the gathering of condensed water.Buoyancy compartment 11 is located in the cabin, space, and buoyancy compartment 11 is the vacuum buoyancy compartment, in be provided with triangle reinforced rib 12.Ball float shell lower semisphere part outer casing bottom has ball float cabin folding and unfolding draw ring 13, and ball float out of my cabin device withstand voltage waterproof High-frequency plug 16 or fiber-optical socket are arranged, device has satellite antenna buoyancy compartment folding and unfolding combination cable 17, have withstand voltage, pulling force is strong, the certain softness of tool, constitute by wirerope transmitting-receiving optical fiber transmission line, satellite positioning feeder line, moisture separator low potential source line.Ball float shell 15 adopts the withstand voltage non-metallic material of conduction to make, ball float shell 15 profiles are carried out necessary color camouflage as jellyfish, and the following part that increases of ball float shell 15 is equipped with the damping due to rotation bar 21 that the hydrophilic soft material is made, its effect is that the simulation jellyfish must rotate freely in prevention, plays the damping turning effort.Water wetted material is met water nature spreading, but is squeezed and draining.
Claims (5)
1, a kind of latent usefulness can be received, put formula satellite dual-mode antenna ball float cabin, it is characterized in that structure comprises dual-mode antenna, the vertical equity circle, the vertical equity axle, the transverse horizontal circle, transverse horizontal axis, the antenna mounting horizontal stand, platform axle, satellite transmitting-receiving feeder line interface in the cabin, the cabin, space, electrical warming removal moisture drying device, buoyancy compartment, ball float cabin folding and unfolding draw ring, the annular wave resistance waves stabilization ring, the ball float shell, the withstand voltage out of my cabin waterproof High-frequency plug of ball float, satellite antenna buoyancy compartment folding and unfolding combination cable, last lower sphere connection lead, the water-tight cushion rubber, the ball float shell is provided with disjunctor annular wave resistance and waves stabilization ring, the ball float shell is by last, the lower semisphere housing is formed, on, the water-tight cushion rubber is housed between the lower semisphere housing, ball float shell lower semisphere housing line of centers two end devices have vertical equity axle and vertical equity circle, by vertical equity circle line of centers two end devices transverse horizontal axis is arranged, device has the transverse horizontal circle on the transverse horizontal axis, line of centers two ends by the transverse horizontal circle are connected with the antenna platform axle again, the antenna platform shaft device has the antenna mounting horizontal stand, device has dual-mode antenna on the antenna mounting horizontal stand, termination feeder line under the antenna mounting horizontal stand, ball float shell lower semisphere partly is the cabin, space, electric drying apparatus is equipped with in space bilge portion, buoyancy compartment is located in the cabin, space, buoyancy compartment is the vacuum buoyancy compartment, in be provided with the triangle reinforced rib, ball float shell lower semisphere part outer casing bottom has ball float cabin folding and unfolding draw ring, and ball float out of my cabin device withstand voltage waterproof High-frequency plug or fiber-optical socket are arranged, device has satellite antenna buoyancy compartment folding and unfolding combination cable.
2, but latent usefulness retractable formula satellite dual-mode antenna ball float according to claim 1 cabin is characterized in that ball float shell the latter half is equipped with the damping due to rotation bar that water wetted material is made.
But 3, latent usefulness retractable formula satellite dual-mode antenna ball float according to claim 1 cabin is characterized in that satellite antenna buoyancy compartment folding and unfolding combination cable is made of wirerope, transmitting-receiving optical fiber transmission line, satellite positioning feeder line, moisture separator low potential source line.
4, but latent usefulness retractable formula satellite dual-mode antenna ball float according to claim 1 cabin is characterized in that the dual-mode antenna that installs on the antenna mounting horizontal stand comprises active satellite dual-mode antenna, grapefruit satellite antenna, satellite positioning antenna.
5, but latent usefulness retractable formula satellite dual-mode antenna ball float according to claim 1 cabin is characterized in that device has the automatic tracking servosystem on the antenna mounting horizontal stand.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 03259305 CN2626857Y (en) | 2003-07-04 | 2003-07-04 | Floating ball cabin of retractable satellite receiving/emitting antenna for submergence |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 03259305 CN2626857Y (en) | 2003-07-04 | 2003-07-04 | Floating ball cabin of retractable satellite receiving/emitting antenna for submergence |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2626857Y true CN2626857Y (en) | 2004-07-21 |
Family
ID=34254810
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 03259305 Expired - Fee Related CN2626857Y (en) | 2003-07-04 | 2003-07-04 | Floating ball cabin of retractable satellite receiving/emitting antenna for submergence |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2626857Y (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103921914A (en) * | 2014-04-22 | 2014-07-16 | 中国船舶重工集团公司第七○二研究所 | Connection release device for escape capsule |
| CN104062458A (en) * | 2014-06-24 | 2014-09-24 | 无锡市崇安区科技创业服务中心 | Water flow velocity detector for field exploration |
| CN104538779A (en) * | 2014-12-08 | 2015-04-22 | 河北汉光重工有限责任公司 | Subdivision airtight structure |
| CN106741766A (en) * | 2016-11-18 | 2017-05-31 | 宁波市镇海丹发机械科技有限公司 | Midget submarine self-floating signal receiving device |
| CN108352108A (en) * | 2015-10-30 | 2018-07-31 | 卢特龙电子公司 | Wireless control apparatus with the antenna being illuminated by visible light |
| CN112985479A (en) * | 2021-02-09 | 2021-06-18 | 山东省科学院海洋仪器仪表研究所 | Real-time health condition monitoring system and method for ocean buoy communication antenna |
| CN113978621A (en) * | 2021-11-05 | 2022-01-28 | 西北工业大学 | Stability augmentation device for water surface buoy |
| US11362408B2 (en) | 2015-10-30 | 2022-06-14 | Lutron Technology Company Llc | Wireless control device having an antenna illuminated with visible light |
-
2003
- 2003-07-04 CN CN 03259305 patent/CN2626857Y/en not_active Expired - Fee Related
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103921914A (en) * | 2014-04-22 | 2014-07-16 | 中国船舶重工集团公司第七○二研究所 | Connection release device for escape capsule |
| CN104062458A (en) * | 2014-06-24 | 2014-09-24 | 无锡市崇安区科技创业服务中心 | Water flow velocity detector for field exploration |
| CN104062458B (en) * | 2014-06-24 | 2016-08-03 | 无锡市崇安区科技创业服务中心 | A kind of ground observation water flow velocity detector |
| CN104538779A (en) * | 2014-12-08 | 2015-04-22 | 河北汉光重工有限责任公司 | Subdivision airtight structure |
| CN108352108A (en) * | 2015-10-30 | 2018-07-31 | 卢特龙电子公司 | Wireless control apparatus with the antenna being illuminated by visible light |
| CN108352108B (en) * | 2015-10-30 | 2020-09-18 | 路创技术有限责任公司 | Wireless control device with antenna illuminated with visible light |
| US11362408B2 (en) | 2015-10-30 | 2022-06-14 | Lutron Technology Company Llc | Wireless control device having an antenna illuminated with visible light |
| US11870127B2 (en) | 2015-10-30 | 2024-01-09 | Lutron Technology Company Llc | Wireless control device having an antenna illuminated with visible light |
| CN106741766A (en) * | 2016-11-18 | 2017-05-31 | 宁波市镇海丹发机械科技有限公司 | Midget submarine self-floating signal receiving device |
| CN112985479A (en) * | 2021-02-09 | 2021-06-18 | 山东省科学院海洋仪器仪表研究所 | Real-time health condition monitoring system and method for ocean buoy communication antenna |
| CN113978621A (en) * | 2021-11-05 | 2022-01-28 | 西北工业大学 | Stability augmentation device for water surface buoy |
| CN113978621B (en) * | 2021-11-05 | 2023-02-10 | 西北工业大学 | Stability augmentation device for water surface buoy |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |