CN105015778B - Amphibious aircraft with wave inhibition groove outer plate - Google Patents
Amphibious aircraft with wave inhibition groove outer plate Download PDFInfo
- Publication number
- CN105015778B CN105015778B CN201410289915.9A CN201410289915A CN105015778B CN 105015778 B CN105015778 B CN 105015778B CN 201410289915 A CN201410289915 A CN 201410289915A CN 105015778 B CN105015778 B CN 105015778B
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- outside plate
- amphibious aircraft
- wave suppression
- trough
- group
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Abstract
An amphibious aircraft with a wave inhibition groove outer plate comprises an amphibious aircraft body (1) and is further provided with a wave inhibition groove outer plate (2) and a group of connecting rods (3). The wave inhibition groove outer plate (2) is installed at the bottom of the amphibious aircraft body (1) through the group of connecting rods (3) and forms a wave inhibition groove (1-1) together with a fuselage of the amphibious aircraft body (1). The amphibious aircraft has the advantages of remarkably improving spattering performance, enhancing seakeeping capacity, and improving attendance rate.
Description
Technical field
The present invention relates to amphibious aircraft production field is and in particular to a kind of fly with the amphibious of wave suppression trough outside plate
Machine.
Background technology
At present, in amphibious aircraft in water surface take-off process, substantial amounts of high speed splash current, these splash water are produced
Stream will impact aircraft power plant, wing flap, and empennage, and this not only makes these component undergoes deformation cannot normally use, or even
Directly it is damaged, and impact current also can corrode said structure for a long time, this spraying state is more serious under wave state.
Content of the invention
The purpose of the present invention is aiming at present, and amphibious aircraft, in water surface take-off process, produces substantial amounts of high speed
Splash current, these splash current will impact aircraft power plant, wing flap, and empennage, and this not only makes these parts become
Shape cannot normally use, or even is directly damaged, and impact current also can corrode said structure, under wave state for a long time
The more serious deficiency of this spraying state, and a kind of amphibious aircraft with wave suppression trough outside plate is provided.
The present invention includes amphibious aircraft body, and it also has wave suppression trough outside plate and one group of connecting rod, and wave suppression trough outside plate leads to
Cross one group of connecting rod and be arranged on amphibious aircraft body bottom portion, and form wave suppression trough with the fuselage of amphibious aircraft body.
Wave suppression trough outside plate has one group of vent hole.
Wave suppression trough outside plate includes outside plate and inner panel, and outside plate is arranged on inner panel by one group of connecting shaft.
Outside plate and inner panel are metallic plate.
The method have the advantages that: the present invention is obviously improved aircraft splash performance, improves the sea-keeping of aircraft, increases amphibious
The rate of attendance of aircraft.
Brief description
Fig. 1 is present configuration schematic diagram.
Fig. 2 is wave suppression trough outer panel structure schematic diagram.
Specific embodiment
As shown in Figure 1, 2, the present invention includes amphibious aircraft body 1, and it also has wave suppression trough outside plate 2 and one group of connecting rod
3, wave suppression trough outside plate 2 is arranged on amphibious aircraft body 1 bottom by one group of connecting rod 3, and with amphibious aircraft body 1
Fuselage formed wave suppression trough 1-1.
Wave suppression trough outside plate 2 has one group of vent hole.
Wave suppression trough outside plate 2 includes outside plate 4 and inner panel 5, and outside plate 4 is arranged on inner panel 5 by one group of connecting shaft 4-1.
Outside plate 4 and inner panel 5 are metallic plate.
Operation principle: wave suppression trough outside plate and airplane hull form groove, i.e. wave suppression trough, the splash current that hull produces
Enter in 1-1, sprayed backward by rotation, thus be now obviously reduced the momentum of current, and then reduce the height that current spray,
To reach the effect (current that wave suppression trough outside plate is mainly used in entry deterrence wave suppression trough outwards spray at a high speed) of suppression splash.
Claims (1)
1. a kind of amphibious aircraft with wave suppression trough outside plate, it includes amphibious aircraft body (1) it is characterised in that it
Also have wave suppression trough outside plate (2) and one group of connecting rod (3), wave suppression trough outside plate (2) is arranged on amphibious by one group of connecting rod (3)
Aircraft body (1) bottom, and form wave suppression trough (1-1) with the fuselage of amphibious aircraft body (1)；Wave suppression trough outside plate (2) is opened
There is one group of vent；Wave suppression trough outside plate (2) includes outside plate (4) and inner panel (5), and outside plate (4) passes through one group of connecting shaft (4-1) and installs
On inner panel (5)；Outside plate (4) and inner panel (5) are metallic plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410289915.9A CN105015778B (en) | 2014-06-26 | 2014-06-26 | Amphibious aircraft with wave inhibition groove outer plate |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410289915.9A CN105015778B (en) | 2014-06-26 | 2014-06-26 | Amphibious aircraft with wave inhibition groove outer plate |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105015778A CN105015778A (en) | 2015-11-04 |
| CN105015778B true CN105015778B (en) | 2017-01-25 |
Family
ID=54406173
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410289915.9A Active CN105015778B (en) | 2014-06-26 | 2014-06-26 | Amphibious aircraft with wave inhibition groove outer plate |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105015778B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108082475B (en) * | 2017-11-08 | 2022-11-18 | 中航通飞华南飞机工业有限公司 | Wave suppression structure of seaplane |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB316751A (en) * | 1928-07-07 | 1929-08-08 | Samuel Edgar Saunders | Improvements in and relating to boat and other bodies |
| GB530520A (en) * | 1938-06-25 | 1940-12-13 | Ashley Chadbourne Mckinley | Improvements in or relating to aircraft floats |
| CA958948A (en) * | 1971-07-30 | 1974-12-10 | Blade Hulls | High speed boat with planing hull |
| US3854679A (en) * | 1974-01-07 | 1974-12-17 | Lockheed Aircraft Corp | Water-based airplane especially designed for adaptation to stol |
| US4691881A (en) * | 1985-10-08 | 1987-09-08 | Gioia G Leonard | High performance amphibious airplane |
| RU2015068C1 (en) * | 1992-07-30 | 1994-06-30 | Таганрогский авиационный научно-технический комплекс им.Г.М.Бериева | Seaplane spray deflector |
| CN2555229Y (en) * | 2002-04-30 | 2003-06-11 | 广州天象地效飞行器股份有限公司 | Ground effect aircraft having specific water dynamic distribution |
-
2014
- 2014-06-26 CN CN201410289915.9A patent/CN105015778B/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN105015778A (en) | 2015-11-04 |
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