CN101054113A - Hydroplanes - Google Patents
Hydroplanes Download PDFInfo
- Publication number
- CN101054113A CN101054113A CN 200710052299 CN200710052299A CN101054113A CN 101054113 A CN101054113 A CN 101054113A CN 200710052299 CN200710052299 CN 200710052299 CN 200710052299 A CN200710052299 A CN 200710052299A CN 101054113 A CN101054113 A CN 101054113A
- Authority
- CN
- China
- Prior art keywords
- wing
- floatplane
- hydroairplane
- bodies
- floating drum
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
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Abstract
The invention discloses a floatplane, which includes floatplane bodies, wings, pontoons, a rudder and an engine. Characteristic of the invention is: the wings include a front wing which is mounted at front of the floatplane bodies, and a rear wing which is mounted at back of the floatplane bodies; the pontoons are disposed at two sides of the floatplane bodies bottom; the floatplane bodies are streamline oblate and are equipped abreast of two or above two. Advantages of the floatplane are short slip distance and safety.
Description
Technical field:
The invention belongs to aircraft, especially a kind of hydroairplane.
Background technology:
At present, during the seaplane take-off of single-wing, take off because of wanting integral body, require coasting distance far away, during the landing water surface, whole landing is prone to accidents.
Summary of the invention:
The object of the present invention is to provide a kind of coasting distance shorter, the hydroairplane of safety.
Technical solution of the present invention is as follows:
1, a kind of hydroairplane, comprise by body, wing, floating drum, yaw rudder, driving engine, feature is that described wing is made of preceding wing and back wing, wing is installed in front part of a body before described, described back wing be installed in After-Body above, described floating drum is installed in both sides, body bottom surface.
2, as technical scheme 1 described hydroairplane, wherein, described body is made as the streamline contour oblate body.
3, as technical scheme 1 described hydroairplane, wherein, described body is installed two or more side by side.
The present invention compared with prior art has shorter, the safe advantage of coasting distance.
Description of drawings:
Fig. 1 is an integral structure front view of the present invention.
Fig. 2 is an integral structure left view of the present invention.
Fig. 3 is an integral structure birds-eye view of the present invention.
Fig. 4 is embodiments of the invention 2 front views.
Fig. 5 is embodiments of the invention 2 left views.
Fig. 6 is embodiments of the invention 2 birds-eye vieies.
Among Fig. 1～Fig. 6, body (1), preceding wing (2), floating drum (3), yaw rudder (4), back wing (5), driving engine (6).
The specific embodiment:
Embodiment 1: with reference to Fig. 1～shown in Figure 3, a kind of hydroairplane, comprise by body, wing, floating drum, yaw rudder, driving engine, wherein, described wing is made of preceding wing (2) and back wing (5), wing (2) is installed in body (1) front portion before described, described back wing (5) be installed in body (1) rear portion above, described floating drum (3) is installed in body (1) both sides, bottom surface.
Embodiment 2: shown in Fig. 4～6, described wing is made of preceding wing (2) and back wing (6), and is identical with embodiment 1 structure, and difference is that two-shipper body (1) replaces floating drum (3), and described body (1) is made as the streamline contour oblate body; Described body (1) is installed two or more side by side.
Principle of work: when taking off, anterior body (1) is risen with preceding wing (2); Use back wing (5) that body (1) rear portion is risen again.During landing, earlier with back wing (5) with the landing of body (1) rear portion, after sliding a segment distance and slowing down, anterior body (1) is landed with preceding wing (2).Reach purpose of safety.
Claims (3)
1, a kind of hydroairplane, comprise by body, wing, floating drum, yaw rudder, driving engine, it is characterized in that, described wing is made of preceding wing (2) and back wing (6), wing (2) is installed in body (1) front portion before described, described back wing (6) be installed in body (1) rear portion above, described floating drum (3) is installed in body (1) both sides, bottom surface.
According to the described hydroairplane of claim 1, it is characterized in that 2, described body (1) is made as the streamline contour oblate body.
According to the described hydroairplane of claim 1, it is characterized in that 3, described body (1) is installed two or more side by side.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200710052299 CN101054113A (en) | 2007-05-24 | 2007-05-24 | Hydroplanes |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200710052299 CN101054113A (en) | 2007-05-24 | 2007-05-24 | Hydroplanes |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN101054113A true CN101054113A (en) | 2007-10-17 |
Family
ID=38794207
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200710052299 Pending CN101054113A (en) | 2007-05-24 | 2007-05-24 | Hydroplanes |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN101054113A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102424110A (en) * | 2011-11-23 | 2012-04-25 | 向天立 | Variable wing miniature amphibious aircraft |
-
2007
- 2007-05-24 CN CN 200710052299 patent/CN101054113A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102424110A (en) * | 2011-11-23 | 2012-04-25 | 向天立 | Variable wing miniature amphibious aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |