CN109353502A - A kind of overwater flight experience autogyro - Google Patents
A kind of overwater flight experience autogyro Download PDFInfo
- Publication number
- CN109353502A CN109353502A CN201811436008.7A CN201811436008A CN109353502A CN 109353502 A CN109353502 A CN 109353502A CN 201811436008 A CN201811436008 A CN 201811436008A CN 109353502 A CN109353502 A CN 109353502A
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- CN
- China
- Prior art keywords
- floating drum
- hydrofoil
- autogyro
- module
- fuselage
- 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
Links
- 230000003014 reinforcing effect Effects 0.000 claims abstract description 16
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 14
- 238000009434 installation Methods 0.000 claims description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C35/00—Flying-boats; Seaplanes
Abstract
The invention discloses a kind of overwater flight to experience autogyro, includes gyroplane module, floating drum module, hydrofoil modules；Gyroplane module mainly includes fuselage, rotor, propeller, empennage；Floating drum module includes floating drum, preceding floating drum supporting beam, rear floating drum supporting beam, preceding floating drum reinforcing beam, rear floating drum reinforcing beam；Hydrofoil modules include preceding hydrofoil, rear hydrofoil, rear hydrofoil supporting beam；Floating drum module is connected by floating drum supporting beam and gyroplane fuselage, and floating drum reinforcing beam and floating drum are rigidly connected, and improves spar structures stability；Preceding hydrofoil and floating drum are connected, and rear hydrofoil is connected by rear hydrofoil supporting beam and gyroplane fuselage.The invention has the advantages that simple and practical, safe and reliable, at low cost, novel appearance can make sightseeing tour waterborne, flight experience.
Description
Technical field
The present invention relates to aviation fields, and in particular to a kind of overwater flight experience autogyro.
Background technique
In recent years, with the fast development of aviation industry, more and more aircraft are applied to sightseeing tour, flying body
It tests, is favored by people, autogyro is in the industry cycle obtained because of the advantages that its structure is simple, manufacturing cost is low, highly-safe
Extensive concern has a extensive future.Current autogyro generally can only be in land takeoff and anding, and needs specific runway, for
Disadvantages described above, the present invention devise a kind of overwater flight experience autogyro, can be used as the water surface and go sightseeing, flight experience is used
On the way.
Summary of the invention
Problem to be solved by this invention is can only to provide one in this problem of land face landing for current autogyro
Autogyro is experienced in kind overwater flight.
The present invention uses following technical scheme in order to solve the above problem: a kind of overwater flight experience autogyro, described
Autogyro includes gyroplane module, floating drum module, hydrofoil modules；Wherein, the gyroplane module is the flight with rotor
Device, the floating drum module are installed on the lower section of the gyroplane module fuselage, for generating buoyancy of aircraft when on the water surface；
The hydrofoil modules are installed on the lower section of the floating drum module, are located under water, for cutting the face of striking, generate lift, will rotate certainly
Wing machine is integrally lifted away from the water surface, and resistance reduces, until autogyro lift-off flight.
Further, the gyroplane module includes fuselage, rotor, propeller, empennage；The body upper installation rotation
Propeller is installed in the wing, dead astern；The empennage is installed on the extended part of the fuselage bottom.
Further, the floating drum module include floating drum, preceding floating drum supporting beam, rear floating drum supporting beam, preceding floating drum reinforcing beam,
Floating drum reinforcing beam afterwards；The floating drum is divided into left and right two, is strip tubular, is arranged along fuselage direction, passes through forward and backward floating drum branch
Support beam is connected on the fuselage；It is reinforced between the left and right floating drum by horizontally disposed forward and backward floating drum reinforcing beam.
Further, the hydrofoil modules include preceding hydrofoil, rear hydrofoil, rear hydrofoil supporting beam；The preceding hydrofoil is bar shaped,
It is vertically installed below the floating drum；Hydrofoil is bar shaped after described, is horizontally disposed with, passes through rear hydrofoil supporting beam and gyroplane machine
Body is connected.
As a preference, the preceding hydrofoil is divided into left and right two, respectively symmetrically it is installed below left and right floating drum, it is described
It is angled between preceding hydrofoil and vertical direction.
The invention adopts the above technical scheme compared with prior art, has following technical effect that
Simply, practical, safe and reliable, at low cost, novel appearance can make sightseeing tour waterborne, flight experience.
Detailed description of the invention
Fig. 1 is shaft side figure of the invention；
Fig. 2 is front view of the invention；
In figure, 1- fuselage, 2- rotor, 3- propeller, 4- empennage, 5- floating drum, floating drum supporting beam after 6-, floating drum reinforcing beam before 7-,
Floating drum reinforcing beam after 8-, hydrofoil before 9-, hydrofoil after 10-, hydrofoil supporting beam after 11-, floating drum supporting beam before 12-.
Specific embodiment
Technical solution of the present invention is described in further detail with reference to the accompanying drawing:
Embodiment 1
As shown in Figure 1 and Figure 2, autogyro is experienced in a kind of overwater flight provided by the invention, and the autogyro includes rotation
Wing machine module, floating drum module, hydrofoil modules；Wherein, the gyroplane module is the aircraft with rotor 2, the floating drum module
It is installed on the lower section of the gyroplane module fuselage 1, for generating buoyancy of aircraft when on the water surface；The hydrofoil modules peace
Lower section loaded on the floating drum module is located under water, for cutting the face of striking, generates lift, autogyro is integrally lifted away from water
Face, resistance reduce, until autogyro lift-off flight.
Further, the gyroplane module includes fuselage 1, rotor 2, propeller 3, empennage 4；Pacify above the fuselage 1
Rotor 2 is filled, propeller 3 is installed in dead astern；The empennage 4 is installed on the extended part of 1 bottom of fuselage.
Further, the floating drum module includes floating drum, preceding floating drum supporting beam 12, rear floating drum supporting beam 6, the reinforcement of preceding floating drum
Beam 7, rear floating drum reinforcing beam 8；The floating drum is divided into left and right two, is strip tubular, is arranged along 1 direction of fuselage, by forward and backward
Floating drum supporting beam 6 is connected on the fuselage 1；Added between the left and right floating drum by horizontally disposed forward and backward floating drum reinforcing beam
Gu.
Further, the hydrofoil modules include preceding hydrofoil 9, rear hydrofoil 10, rear hydrofoil supporting beam 11；The preceding hydrofoil 9
For bar shaped, vertically it is installed below the floating drum；Hydrofoil 10 is bar shaped after described, is horizontally disposed with, and is supported by rear hydrofoil 10
Beam and gyroplane fuselage 1 are connected.
As a preference, the preceding hydrofoil 9 is divided to control two, respectively symmetrically it is installed below left and right floating drum, it is described
It is angled between preceding hydrofoil 9 and vertical direction.
The present invention is such to work and implements, and autogyro is experienced in a kind of overwater flight, comprising gyroplane module,
Floating drum module, hydrofoil modules；Gyroplane module mainly includes fuselage 1, rotor 2, propeller 3, empennage 4；Floating drum module includes floating
Cylinder 5, preceding floating drum supporting beam 12, rear floating drum supporting beam 6, preceding floating drum reinforcing beam 7, rear floating drum reinforcing beam 8；Hydrofoil modules include preceding water
The wing 9, rear hydrofoil 10, rear hydrofoil supporting beam 11；Floating drum module is connected by floating drum supporting beam 12,6 and gyroplane fuselage 1, floating drum
Reinforcing beam 7,8 and floating drum 5 are rigidly connected, and improve 5 structural stability of floating drum；Preceding hydrofoil 9 is connected with floating drum 5, and rear hydrofoil 10 passes through
Hydrofoil supporting beam 11 and gyroplane fuselage 1 are connected afterwards.
On the buoyancy that autogyro relies on floating drum 5 to generate before taking off is bubbled through the water column, propeller 3 works when taking off, and generates
Forward thrust pushes autogyro to travel forward, and as 3 revolving speed of propeller improves, thrust increases, and autogyro advances
Speed increases, the high speed rotation under the promotion of air-flow of rotor 2, generates lift, while being placed in the hydrofoil 9 of autorotating rotor motor spindle,
10 cut the face of striking, and generate lift, and autogyro is integrally lifted away from the water surface, and resistance reduces, until autogyro lift-off flight.
Those skilled in the art can understand that unless otherwise defined, all terms used herein include skill
Art term and scientific term have meaning identical with the general understanding of those of ordinary skill in fields of the present invention.Also answer
It should be appreciated that those terms such as defined in the general dictionary should be understood that have in the context of the prior art
The consistent meaning of meaning, and unless defined as here, it will not be explained in an idealized or overly formal meaning.
Above-described specific embodiment has carried out further the purpose of the present invention, technical scheme and beneficial effects
It is described in detail, it should be understood that being not limited to this hair the foregoing is merely a specific embodiment of the invention
Bright, all within the spirits and principles of the present invention, any modification, equivalent substitution, improvement and etc. done should be included in the present invention
Protection scope within.
Claims (5)
1. autogyro is experienced in a kind of overwater flight, which is characterized in that the autogyro includes gyroplane module, floating drum
Module, hydrofoil modules；Wherein, the gyroplane module is the aircraft with rotor, and the floating drum module is installed on the rotor
The lower section of machine module fuselage, for generating buoyancy of aircraft when on the water surface；The hydrofoil modules are installed on the floating drum mould
The lower section of block is located under water, for cutting the face of striking, generates lift, autogyro is integrally lifted away from the water surface, resistance reduces, directly
It goes up to the air and flies to autogyro.
2. autogyro is experienced in a kind of overwater flight according to claim 1, which is characterized in that the gyroplane module
Including fuselage, rotor, propeller, empennage；The body upper installs rotor, and propeller is installed in dead astern；The empennage installation
In on the extended part of the fuselage bottom.
3. autogyro is experienced in a kind of overwater flight according to claim 2, which is characterized in that the floating drum module packet
Containing floating drum, preceding floating drum supporting beam, rear floating drum supporting beam, preceding floating drum reinforcing beam, rear floating drum reinforcing beam；The floating drum is divided into left and right two
It is a, it is strip tubular, is arranged along fuselage direction, is connected on the fuselage by forward and backward floating drum supporting beam；It is described left and right
It is reinforced between floating drum by horizontally disposed forward and backward floating drum reinforcing beam.
4. autogyro is experienced in a kind of overwater flight according to claim 3, which is characterized in that the hydrofoil modules packet
Containing preceding hydrofoil, rear hydrofoil, rear hydrofoil supporting beam；The preceding hydrofoil is bar shaped, is vertically installed below the floating drum；Water after described
The wing is bar shaped, is horizontally disposed with, and is connected by rear hydrofoil supporting beam and gyroplane fuselage.
5. autogyro is experienced in a kind of overwater flight according to claim 4, which is characterized in that the preceding hydrofoil is divided into
Left and right two is respectively symmetrically installed below left and right floating drum, angled between the preceding hydrofoil and vertical direction.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811436008.7A CN109353502A (en) | 2018-11-28 | 2018-11-28 | A kind of overwater flight experience autogyro |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811436008.7A CN109353502A (en) | 2018-11-28 | 2018-11-28 | A kind of overwater flight experience autogyro |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109353502A true CN109353502A (en) | 2019-02-19 |
Family
ID=65343539
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811436008.7A Pending CN109353502A (en) | 2018-11-28 | 2018-11-28 | A kind of overwater flight experience autogyro |
Country Status (1)
| Country | Link |
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| CN (1) | CN109353502A (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB163034A (en) * | 1920-05-07 | 1922-07-18 | Alexander Graham Bell | Improvements in and relating to hydroplane vessels, hydro-aeroplanes and the like |
| RU2024418C1 (en) * | 1992-01-16 | 1994-12-15 | Демидченко Владимир Иванович | Seaplane |
| US20080251308A1 (en) * | 2005-08-24 | 2008-10-16 | Dezso Molnar | Ground Air Water Craft |
| CN209479986U (en) * | 2018-11-28 | 2019-10-11 | 南京航空航天大学 | A kind of overwater flight experience autogyro |
-
2018
- 2018-11-28 CN CN201811436008.7A patent/CN109353502A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB163034A (en) * | 1920-05-07 | 1922-07-18 | Alexander Graham Bell | Improvements in and relating to hydroplane vessels, hydro-aeroplanes and the like |
| RU2024418C1 (en) * | 1992-01-16 | 1994-12-15 | Демидченко Владимир Иванович | Seaplane |
| US20080251308A1 (en) * | 2005-08-24 | 2008-10-16 | Dezso Molnar | Ground Air Water Craft |
| CN101365624A (en) * | 2005-08-24 | 2009-02-11 | 莫尔纳里公司 | Ground air water craft |
| CN209479986U (en) * | 2018-11-28 | 2019-10-11 | 南京航空航天大学 | A kind of overwater flight experience autogyro |
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