CN203528804U - Large-size rescue amphibious aircraft - Google Patents
Large-size rescue amphibious aircraft Download PDFInfo
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- CN203528804U CN203528804U CN201320472811.2U CN201320472811U CN203528804U CN 203528804 U CN203528804 U CN 203528804U CN 201320472811 U CN201320472811 U CN 201320472811U CN 203528804 U CN203528804 U CN 203528804U
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Abstract
The utility model discloses a large-size rescue amphibious aircraft which comprises an aircraft body, wings, an empennage, a landing gear, engines and nacelles, wherein the aircraft body adopts a hull type structure; the wings are fixed on a hump on the back of the aircraft body and are cantilever-type; the engines, the nacelles and floating barrels are arranged on the wings on two sides respectively; the floating barrels are arranged on the lower parts of the outer ends of the wings; the empennage comprises a horizontal tail, a vertical fin and a dorsal fin; the vertical fin and the dorsal fin are spliced on the tail of the back of the aircraft body; and the upper part of the vertical fin is connected with the horizontal tail and is T-shaped. According to the technical scheme disclosed by the utility model, the take-off and landing properties over the water and on the ground can be realized; meanwhile, a large storage space is used for arranging search and rescue equipment; and the large-size rescue amphibious aircraft can quickly fly to an accidental sea area to search persons in distress, and targeted rescue work can be executed according to a sea condition, so that the rescue efficiency is high.
Description
Technical field
The utility model relates to a kind of rescue at sea transportation device, relates in particular to a kind of large-scale rescue amphibious aircraft.
Background technology
When there is casualty, existing rescue at sea transportation device mainly relies on helicopter and rescue ship.Helicopter, because the restriction of voyage and weather condition generally can not be rescued, can only rely on rescue ship to go to rescue, but ship speed is low, and when stormy waves is larger, is difficult to rescue, and causes rescue efficiency low, distress personnel survive wish little.Now, in the urgent need to a kind of landing of airport by land, also can be in water surface landing, the rescue at sea equipment that transport capacity is large.
Summary of the invention
Main purpose of the present utility model is to overcome above-mentioned the deficiencies in the prior art and a kind of rescue at sea ability that has is provided, can be in the water surface, land landing, and the large-scale rescue amphibious aircraft that transport capacity is large, rescue efficiency is high.
In order to solve the problems of the technologies described above, the utility model provides a kind of large-scale rescue amphibious aircraft, and it comprises fuselage, wing, empennage, alighting gear, driving engine and nacelle, and described fuselage is hull formula structure; Described wing is fixed on the hump of described fuselage back, is cantilevered, and both sides wing is respectively provided with driving engine and nacelle and floating drum, and described floating drum is arranged on the bottom of described wing outer end; Described empennage comprises horizontal tail, vertical fin and dorsal fin, and described vertical fin and described dorsal fin splice the afterbody in described fuselage back, and described vertical fin top is connected with described horizontal tail.
As the improvement of technique scheme, described horizontal tail and vertical fin are equipped with the rudder wing, can carry out respectively upper and lower, left and right directions swing.
As the improvement of technique scheme, described both sides wing is respectively provided with a described floating drum.
As the improvement of technique scheme, the upright position of described floating drum is higher than described belly, and lower than described driving engine propeller circle revolution nadir.
As the improvement of technique scheme, described alighting gear is retractable.
As the improvement of technique scheme, the empennage that described vertical fin and described horizontal tail are formed by connecting is T-tail.
As the improvement of technique scheme, described both sides wing is respectively provided with two driving engines and nacelle.
As the improvement of technique scheme, described driving engine is propeller turbine.
Implement the technical solution of the utility model, there is following beneficial effect:
Large-scale rescue amphibious aircraft of the present utility model, compared with prior art, this technical scheme is to utilize hull structure, floating drum, retractable landing gear to realize the water surface, land landing ability, there is larger storage space simultaneously and be used for arranging search and wrecking equipment, can fly to fast accident sea area, search distress personnel, and carry out salvage work targetedly according to sea situation, rescue efficiency is high.
Accompanying drawing explanation
In order to be illustrated more clearly in the technical scheme of the utility model embodiment, below the accompanying drawing to embodiment is briefly described.
Fig. 1 is the front view of a kind of large-scale rescue amphibious aircraft of the utility model;
Fig. 2 is the birds-eye view of a kind of large-scale rescue amphibious aircraft of the utility model;
Fig. 3 is the left view of a kind of large-scale rescue amphibious aircraft of the utility model.
The specific embodiment
Below in conjunction with accompanying drawing, further describe the specific embodiment of the present utility model.
As shown in Figure 1, Figure 2, Figure 3 shows, preferential embodiment as a kind of large-scale rescue amphibious aircraft of the utility model, the present embodiment comprises fuselage 1, wing 2, empennage 3, alighting gear 4, driving engine and nacelle 5, preferably, described fuselage 1 is hull formula structure, described wing 2 is fixed on the hump at described fuselage 1 back, be cantilevered, both sides wing is respectively provided with driving engine and nacelle 5 and floating drum 6, driving engine and nacelle 5 are preferably at both sides wing and are respectively arranged with two, i.e. four driving engines and nacelle 5 altogether, floating drum 6 can arrange one and also can arrange a plurality of.Described floating drum 6 is arranged on the bottom of described wing 2 outer ends, and described empennage 3 comprises horizontal tail 31, vertical fin 32 and dorsal fin 33, and described vertical fin 32 splices in the afterbody at described fuselage 1 back with described dorsal fin 33, and described vertical fin 32 tops are connected with described horizontal tail 31, T-shaped.
When the water surface berths, above-mentioned fuselage 1 is to utilize the distinctive buoyancy of hull structure that aircraft is held up, to guarantee safety, park and slide against on the water surface, in fuselage, there is larger space for wrecking equipment being set and arranging seat, thereby there is larger transport capacity for loading and being connected other each parts.When the water surface takes off, 4 screw propeller entrys into service of above-mentioned driving engine and nacelle 5, produce airflow and act on above-mentioned wing 2, and wing 2 has certain angle of lift, for aircraft provides power and lift, thereby makes aircraft planking, ascends to heaven.While sliding, above-mentioned floating drum 6 can supply lateral stability by assisted Extraction.During flight, above-mentioned horizontal tail 31, the fore-and-aft stability of major control aircraft and road-holding property; Above-mentioned vertical fin 32, the lateral stability of major control aircraft and road-holding property; Dorsal fin 33, for improving the horizontal navigation stability of aircraft.
Above-mentioned horizontal tail 31 and vertical fin 32 are provided with the rudder wing 34,35, can carry out respectively upper and lower, left and right directions swing, thereby improve the maneuverability of aircraft under state of flight.
Above-mentioned alighting gear 4 is retractable, when aircraft is by land during landing, launches alighting gear 4, packs up alighting gear 4, thereby both had landing ability on road when hydroplaning, again can be in hydroplaning.
Preferentially, above-mentioned driving engine 5 is propeller turbine, makes aircraft maximum flying speed can reach 560,000 ms/h.
The upright position of above-mentioned floating drum 6 is higher than above-mentioned fuselage 1 belly, and lower than above-mentioned driving engine 1 propeller circle revolution nadir, in order to avoid touch the water surface during screw propeller rotation, guarantees the water surface landing in high 2 meters of wave simultaneously.
Large-scale rescue amphibious aircraft of the present utility model, it is the fixed wing aircraft for rescue at sea, its maximum flying speed can reach 560,000 ms/h, can be in the water surface landing of high 2 meters of wave, can arrive at fast accident sea area and carry out searching rescue, in the situation that at sea environment is exceedingly odious, can rescue article bag by air-drop and provide the article of urgent need for distress personnel.It utilizes hull structure, floating drum, retractable landing gear to realize the water surface, land landing ability, there is larger storage space simultaneously and be used for arranging search and wrecking equipment, when flying to accident sea area fast, can search for distress personnel, and carry out salvage work targetedly according to sea situation, rescue efficiency is high, thereby can effectively solve, existing rescue at sea equipment and technology transportation is difficult, an inefficient difficult problem.
Above disclosed is only a kind of preferred embodiment of the utility model, certainly can not limit with this interest field of the utility model, and the equivalent variations of therefore doing according to the utility model claim, still belongs to the scope that the utility model is contained.
Claims (8)
1. a large-scale rescue amphibious aircraft, comprises fuselage, wing, empennage, alighting gear, driving engine and nacelle, it is characterized in that: described fuselage is hull formula structure; Described wing is fixed on the hump of described fuselage back, is cantilevered, and both sides wing is respectively provided with driving engine and nacelle and floating drum, and described floating drum is arranged on the bottom of described wing outer end; Described empennage comprises horizontal tail, vertical fin and dorsal fin, and described vertical fin and described dorsal fin splice the afterbody in described fuselage back, and described vertical fin top is connected with described horizontal tail.
2. large-scale rescue amphibious aircraft according to claim 1, is characterized in that: described horizontal tail and vertical fin are equipped with the rudder wing, can carry out respectively upper and lower, left and right directions swing.
3. large-scale rescue amphibious aircraft according to claim 1, is characterized in that: described both sides wing is respectively provided with a described floating drum.
4. large-scale rescue amphibious aircraft according to claim 3, is characterized in that: the upright position of described floating drum is higher than described belly, and lower than described driving engine propeller circle revolution nadir.
5. large-scale rescue amphibious aircraft according to claim 1, is characterized in that: described alighting gear is retractable.
6. large-scale rescue amphibious aircraft according to claim 1, is characterized in that: the empennage that described vertical fin and described horizontal tail are formed by connecting is T-tail.
7. large-scale rescue amphibious aircraft according to claim 1, is characterized in that: described both sides wing is respectively provided with two driving engines and nacelle.
8. large-scale rescue amphibious aircraft according to claim 1, is characterized in that: described driving engine is propeller turbine.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320472811.2U CN203528804U (en) | 2012-12-14 | 2013-08-05 | Large-size rescue amphibious aircraft |
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201220698680.5 | 2012-12-14 | ||
| CN201220698680 | 2012-12-14 | ||
| CN201320472811.2U CN203528804U (en) | 2012-12-14 | 2013-08-05 | Large-size rescue amphibious aircraft |
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| Publication Number | Publication Date |
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| CN203528804U true CN203528804U (en) | 2014-04-09 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201320472811.2U Expired - Lifetime CN203528804U (en) | 2012-12-14 | 2013-08-05 | Large-size rescue amphibious aircraft |
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| CN (1) | CN203528804U (en) |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105383695A (en) * | 2015-12-03 | 2016-03-09 | 上海奥科赛飞机有限公司 | Retractable landing gear of amphibious aircraft |
| CN105620733A (en) * | 2014-10-28 | 2016-06-01 | 中航通飞研究院有限公司 | Position alarm device for amphibious aircraft undercarriage folding and unfolding mechanism |
| CN106516082A (en) * | 2016-12-01 | 2017-03-22 | 顺丰科技有限公司 | T-shaped empennage and aircraft with same |
| CN106621379A (en) * | 2017-01-16 | 2017-05-10 | 王长民 | Telecontrolled amphibious aircraft |
| CN107618659A (en) * | 2017-09-12 | 2018-01-23 | 上海优伟斯智能系统有限公司 | A kind of double hair aircraft |
| CN109358654A (en) * | 2018-11-16 | 2019-02-19 | 江苏科技大学 | A kind of empty amphibious search and rescue support unmanned vehicle system of water |
| CN109435602A (en) * | 2018-11-26 | 2019-03-08 | 杨清太 | The amphibious dilatory bird of corner power rises aircraft constructive method |
| CN109435601A (en) * | 2018-11-26 | 2019-03-08 | 杨清太 | The amphibious large-scale dilatory bird of self power generation corner power rises aircraft constructive method |
| CN109774937A (en) * | 2017-11-13 | 2019-05-21 | 中航通飞华南飞机工业有限公司 | The airborne rescue system of large-scale amphibious aircraft inclination waterborne and method |
| CN110282150A (en) * | 2019-07-05 | 2019-09-27 | 中航通飞华南飞机工业有限公司 | A kind of amphibious aircraft emergency guarantee method waterborne |
| CN113232832A (en) * | 2021-03-29 | 2021-08-10 | 南京航空航天大学 | Amphibious aircraft |
-
2013
- 2013-08-05 CN CN201320472811.2U patent/CN203528804U/en not_active Expired - Lifetime
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105620733A (en) * | 2014-10-28 | 2016-06-01 | 中航通飞研究院有限公司 | Position alarm device for amphibious aircraft undercarriage folding and unfolding mechanism |
| CN105620733B (en) * | 2014-10-28 | 2017-11-17 | 中航通飞研究院有限公司 | A kind of amphibious aircraft wheel-retracting gear position warning device |
| CN105383695A (en) * | 2015-12-03 | 2016-03-09 | 上海奥科赛飞机有限公司 | Retractable landing gear of amphibious aircraft |
| CN106516082A (en) * | 2016-12-01 | 2017-03-22 | 顺丰科技有限公司 | T-shaped empennage and aircraft with same |
| CN106621379A (en) * | 2017-01-16 | 2017-05-10 | 王长民 | Telecontrolled amphibious aircraft |
| CN107618659A (en) * | 2017-09-12 | 2018-01-23 | 上海优伟斯智能系统有限公司 | A kind of double hair aircraft |
| CN109774937A (en) * | 2017-11-13 | 2019-05-21 | 中航通飞华南飞机工业有限公司 | The airborne rescue system of large-scale amphibious aircraft inclination waterborne and method |
| CN109358654A (en) * | 2018-11-16 | 2019-02-19 | 江苏科技大学 | A kind of empty amphibious search and rescue support unmanned vehicle system of water |
| CN109358654B (en) * | 2018-11-16 | 2022-03-29 | 江苏科技大学 | Water-air amphibious search and rescue support unmanned aerial vehicle system |
| CN109435602A (en) * | 2018-11-26 | 2019-03-08 | 杨清太 | The amphibious dilatory bird of corner power rises aircraft constructive method |
| CN109435601A (en) * | 2018-11-26 | 2019-03-08 | 杨清太 | The amphibious large-scale dilatory bird of self power generation corner power rises aircraft constructive method |
| CN110282150A (en) * | 2019-07-05 | 2019-09-27 | 中航通飞华南飞机工业有限公司 | A kind of amphibious aircraft emergency guarantee method waterborne |
| CN113232832A (en) * | 2021-03-29 | 2021-08-10 | 南京航空航天大学 | Amphibious aircraft |
| CN113232832B (en) * | 2021-03-29 | 2023-08-22 | 南京航空航天大学 | Amphibious aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20201204 Address after: 519000 Building 201, No. 999 Jinhai Middle Road, Jinwan District, Zhuhai City, Guangdong Province Patentee after: SOUTH CHINA AIRCRAFT INDUSTRY CO., LTD. OF CHINA AVIATION INDUSTRY GENERAL AIRCRAFT Co.,Ltd. Address before: 218 floor 2, building 2, 3 Xiasha street, Wan Chai, Xiangzhou District, Zhuhai, Guangdong, 519040 Patentee before: R&D INSTITUTE OF CHINA AVIATION INDUSTRY GENERAL AIRCRAFT Co.,Ltd. |
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| TR01 | Transfer of patent right | ||
| CX01 | Expiry of patent term |
Granted publication date: 20140409 |
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| CX01 | Expiry of patent term |