KR20130065905A - Hovercraft - Google Patents
Hovercraft Download PDFInfo
- Publication number
- KR20130065905A KR20130065905A KR1020110132506A KR20110132506A KR20130065905A KR 20130065905 A KR20130065905 A KR 20130065905A KR 1020110132506 A KR1020110132506 A KR 1020110132506A KR 20110132506 A KR20110132506 A KR 20110132506A KR 20130065905 A KR20130065905 A KR 20130065905A
- Authority
- KR
- South Korea
- Prior art keywords
- propeller
- hull
- casing
- air
- blades
- Prior art date
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60V—AIR-CUSHION VEHICLES
- B60V1/00—Air-cushion
- B60V1/14—Propulsion; Control thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60V—AIR-CUSHION VEHICLES
- B60V1/00—Air-cushion
- B60V1/18—Body structure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H7/00—Propulsion directly actuated on air
- B63H7/02—Propulsion directly actuated on air using propellers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/001—Shrouded propellers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/16—Blades
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/16—Blades
- B64C11/20—Constructional features
- B64C11/205—Constructional features for protecting blades, e.g. coating
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Exhaust Silencers (AREA)
Abstract
Description
The present invention relates to an air buoy, and more particularly, by configuring the casing formed on the outer periphery of the propeller in a closed structure, by minimizing the noise generated in the intake or exhaust process by the rotational force of the propeller, external exposure An air lift is provided to reduce and improve external sound insulation.
In general, an Hovercraft supplies air force from the flotation propeller to the lower surface of the hull, and the supplied air force inflates the skirt to support the hull, and the floated hull is one side of the hull. It is an amphibious hull which is moved by the wind power of the propeller propeller constructed in.
As such, the air lift boat is provided with a floating propeller for supplying air to the lower part of the hull at the upper part of the hull, and around the lower part of the hull, the air supplied from the floating propeller flows out to the lower end and at the same time a flexible oxford cloth for supporting the hull. A skirt made of rubber is installed, and on one side of the hull, an engine providing power to move the air lift and a propulsion propeller generating a moving propulsion force by wind power while rotating by the rotation force provided from the engine.
As shown in FIG. 1, the
The
The
The propeller (4) provides a propulsion force to the air buoy (1) by providing wind power from the stern of the hull (2) to the tail while rotating while receiving power from the engine (3).
The casing 5 is configured on the outer periphery of the
In addition, behind the casing 5, a plurality of blades 6 for changing the direction of the wind exhausted to the rear end are configured so that the direction of the
Accordingly, the direction of the wind intake air through the
In addition, the structure of the
However, the
In particular, since the wind speed generated by the rotational force of the propulsion propeller is the propulsion force of the air support, the noise increases as the propulsion force is increased or decreased, and there is a problem of destroying the fatigue and natural environment of the surrounding environment by pollution caused by the noise.
In addition, since the front of the casing is open, there is a problem that there is a risk of a safety accident that can be sucked by the wind of the propeller due to carelessness of the hull, in particular, the driver or occupant.
In particular, the conventional air flotation, it is possible to move forward and change direction, but can not reverse, there is a problem that there is a limit of use because the space to turn for the reverse is relatively large.
As proposed to solve the above problems, an object of the present invention, by configuring a casing formed on the outer periphery of the propeller in a closed structure, by minimizing the noise generated in the intake or exhaust process by the rotational force of the propeller, It is to provide an air lift to reduce external exposure and improve external sound insulation.
Another object of the present invention is to configure the rear and side exhaust pipes on the rear and side of the casing, the rear and side blades on the rear and side exhaust pipes, respectively, and to configure the first and second transfer parts to open and close them, the direction change And to provide an air booster to enable the reverse to strengthen the product competitiveness.
The present invention for achieving the above object, in the air buoy operated by the wind speed generated by the rotational force of the propeller propeller configured on one side of the hull, to be configured on one side of the hull to protect the propeller propeller A configured casing; The casing is of a hermetic type; A plurality of inlet ports configured on the front side and a plurality of rear and side exhaust ports on the rear and side sides; Each of the rear and side exhaust vents may include rear and side blades for selectively opening and closing the rear or side exhaust vents for turning or reversing.
In the present invention, it is preferable that each of the rear and side blades further includes first and second transfer parts for providing a transfer force to open and close the rear or side exhaust.
In the present invention, it is preferable that the side exhaust pipe further includes an induction blade for guiding the direction of the wind to be exhausted forward in the diagonal direction.
According to the present invention, by configuring the casing formed on the outer periphery of the propeller in a closed structure, by minimizing the noise generated during the intake or exhaust process by the rotational force of the propeller, to reduce the external exposure, to improve the external sound insulation It works.
In addition, by minimizing the noise generated by the propulsion propeller, there is an effect to significantly improve the leisure activity that does not destroy the fatigue and natural environment in the surrounding environment.
In addition, the rear and side exhaust mechanisms are formed at the rear and side of the casing, and the rear and side blades are configured at the rear and side exhaust mechanisms, respectively, and the first and second transfer parts for opening and closing them are configured to be able to change direction and backward. It has the effect of strengthening product competitiveness.
1 is a schematic diagram of a typical air lift.
2 is a schematic view of an air lift lift in accordance with the present invention.
Figure 3 is an enlarged plan view of the casing of the air lift lift in accordance with the present invention.
4 is a partially enlarged view schematically showing a state in which the rear and side exhaust vents are blocked by the rear and side blades according to the present invention.
Figure 5 is a plan view of the advanced casing of the air buoy according to the present invention.
Figure 6 is a plan view of the casing of the air lift lift in accordance with the present invention.
7 is a plan view of the reverse state of the air lift lift in accordance with the present invention.
Hereinafter, the present invention will be described with reference to the accompanying drawings (the same reference numerals refer to the same elements as in the related art, and a detailed description thereof will be omitted).
As shown in FIG. 2, the
The
The
As shown in FIG. 3, the
The
As shown in FIG. 4, each of the rear and
The rear and
Of course, the present invention is not limited thereto, and any method may be adopted as long as the rear and
In addition, each of the rear and
The first and
The first and
Accordingly, the rear and
The
Looking at the action state of the air lift lift configured as described above are as follows.
As shown in FIG. 5, when the
Therefore, the
When the air lift (1) is to change the direction, as shown in Figure 6, the
In addition, the
Therefore, the air intake through the
When the
Therefore, the wind intake by the rotational force of the
What has been described above is just one embodiment for performing the air lift according to the present invention, the present invention is not limited to the above embodiment, without departing from the gist of the invention claimed in the claims below Anyone with ordinary knowledge in the field of the present invention will have the technical spirit of the present invention to the extent that various modifications can be made.
50: casing 52: intake vent
53: guide blade 54: rear exhaust vent
55: rear blade 56: side exhaust
57: side blade 58: the first transfer unit
59: second transfer unit
Claims (3)
A casing (50) configured on one side of the hull (2) and configured to protect the propulsion propeller (4);
The casing 50 is configured in a sealed type;
A plurality of inlet ports 52 configured on the front side and a plurality of rear and side exhaust pipes 54, 56 on the rear and sides;
Each of the rear and side vents 54 and 56 includes rear and side blades 55 and 57 for selectively opening and closing the rear or side vents 54 and 56 for turning or reversing. Air lift, characterized in that.
Air lift, characterized in that it further comprises a first and second transfer unit (58) (59) to provide a transfer force to enable the opening and closing of the rear or side exhaust (54) (56).
Air induction head further comprises a guide blade (53) for guiding the direction of the wind to be exhausted forward in the diagonal direction.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020110132506A KR20130065905A (en) | 2011-12-12 | 2011-12-12 | Hovercraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020110132506A KR20130065905A (en) | 2011-12-12 | 2011-12-12 | Hovercraft |
Publications (1)
Publication Number | Publication Date |
---|---|
KR20130065905A true KR20130065905A (en) | 2013-06-20 |
Family
ID=48862308
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
KR1020110132506A KR20130065905A (en) | 2011-12-12 | 2011-12-12 | Hovercraft |
Country Status (1)
Country | Link |
---|---|
KR (1) | KR20130065905A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20200065431A (en) * | 2018-11-30 | 2020-06-09 | 선진정공 주식회사 | Airboat with skid part |
KR102240710B1 (en) * | 2020-01-02 | 2021-04-15 | 주식회사 케이마린 | hovercraft having stealth function |
KR20220144493A (en) | 2021-04-20 | 2022-10-27 | 한국항공우주산업 주식회사 | Hovercraft symulation system and symultion method using the same |
-
2011
- 2011-12-12 KR KR1020110132506A patent/KR20130065905A/en not_active Application Discontinuation
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20200065431A (en) * | 2018-11-30 | 2020-06-09 | 선진정공 주식회사 | Airboat with skid part |
KR102240710B1 (en) * | 2020-01-02 | 2021-04-15 | 주식회사 케이마린 | hovercraft having stealth function |
WO2021137368A1 (en) * | 2020-01-02 | 2021-07-08 | 주식회사 케이마린 | Air-cushion vehicle having stealth function |
US11724683B2 (en) | 2020-01-02 | 2023-08-15 | K-Marine Co., Ltd. | Hovercraft having stealth function |
KR20220144493A (en) | 2021-04-20 | 2022-10-27 | 한국항공우주산업 주식회사 | Hovercraft symulation system and symultion method using the same |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
A201 | Request for examination | ||
E902 | Notification of reason for refusal | ||
E601 | Decision to refuse application |