CN109484609A - A kind of general-purpose aircraft made of carbon fibre composite - Google Patents
A kind of general-purpose aircraft made of carbon fibre composite Download PDFInfo
- Publication number
- CN109484609A CN109484609A CN201811523159.6A CN201811523159A CN109484609A CN 109484609 A CN109484609 A CN 109484609A CN 201811523159 A CN201811523159 A CN 201811523159A CN 109484609 A CN109484609 A CN 109484609A
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- CN
- China
- Prior art keywords
- assembly
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- wing
- general
- carbon fibre
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- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Reinforced Plastic Materials (AREA)
- Laminated Bodies (AREA)
Abstract
The invention discloses a kind of general-purpose aircrafts made of carbon fibre composite, belong to cubpiston light-weight design manufacturing technology；It is characterized in that, it includes: radome fairing 1, propeller 2, head sub-assembly 3, fuselage sub-assembly 4, wing sub-assembly 5, empennage sub-assembly 6.The invention proposes a kind of general-purpose aircrafts made of carbon fibre composite, meet general-purpose aircraft Structural strength calls, reduce Aircraft Production cost, alleviate aircraft overall weight, reduce aircraft utilization energy consumption, improve aircraft cruise duration.
Description
Technical field
The invention belongs to cubpiston light-weight design manufacturing technologies, are related to a kind of using carbon fibre composite system
The general-purpose aircraft of work.
Background technique
With the sustainable and stable development of national economy, China has entered the industrial structure overall restructuring stage.Wherein, general boat
Empty industry is as one of most representative new industry by all circles' extensive concern.Hefei Beijing Institute of Aeronautics navigation industrial technology Co., Ltd
As country's navigation industrial technology Research-type Enterprises, the development of domestic navigation industry is led, first item general-purpose aircraft has been started
Development need to consider the development cost of general-purpose aircraft in development process, the problems such as cruise duration, energy consumption, and existing
Large Civil Aircraft and military aircraft main frame structure are still metal material using material.The increase of production cost is brought,
Aircraft is totally overweight, causes energy consumption big in use process, and cruise duration is reduced.
Summary of the invention
The purpose of the present invention is: it proposes a kind of general-purpose aircraft made of carbon fibre composite, meets general-purpose aircraft
Structural strength calls.Aircraft Production cost is reduced, aircraft overall weight is mitigated, reduces aircraft utilization energy consumption, improves aircraft continuation of the journey
Time.
The technical scheme is that a kind of general-purpose aircraft made of carbon fibre composite, which is characterized in that it
It include: radome fairing 1, propeller 2, head sub-assembly 3, fuselage sub-assembly 4, wing sub-assembly 5, empennage sub-assembly 6.Wherein head
Sub-assembly 3 includes head upper housing 3a, head lower case 3b, front-wheel protection shell 3c and connector frame 3d, fuselage sub-assembly 4
Including instrument tank tower 4a, preceding floor 4b, control tank tower 4c, cockpit side plate 4d, handrail transition frame 4e, seat 4f, wing mount brackets
4g, rear floor 4h, backsight cabin 4i and rear body cabin 4j, wing sub-assembly 5 include upside wing and downside wing, empennage group
Component 6 includes tailplane 6a and vertical tail 6b.The radome fairing 1 of general-purpose aircraft, propeller 2, head sub-assembly 3, fuselage group
Component 4, wing sub-assembly 5,6 six part of empennage sub-assembly are that carbon fibre composite is made.
The invention has the advantages that proposing a kind of general-purpose aircraft made of carbon fibre composite, meet general
Aircraft structure strength requirement.Aircraft Production cost is reduced, aircraft overall weight is alleviated, aircraft utilization energy consumption is reduced, mentions
High aircraft cruise duration.
Detailed description of the invention
Fig. 1 is structural front view of the invention.
Fig. 2 is structure sectional view of the invention.
Specific embodiment
The present invention is described in further details below.Referring to Fig. 1, Fig. 2, it is a kind of using carbon fibre composite production
General-purpose aircraft, which is characterized in that it includes: radome fairing 1, propeller 2, head sub-assembly 3, fuselage sub-assembly 4, wing sub-assembly
5, empennage sub-assembly 6.Wherein head sub-assembly 3 includes head upper housing 3a, head lower case 3b, front-wheel protection shell 3c and company
Junctor frame 3d, fuselage sub-assembly 4 include instrument tank tower 4a, preceding floor 4b, control tank tower 4c, cockpit side plate 4d, handrail transition
Frame 4e, seat 4f, wing mount brackets 4g, rear floor 4h, backsight cabin 4i and rear body cabin 4j, wing sub-assembly 5 include upper
Side wing and downside wing, empennage sub-assembly 6 include tailplane 6a and vertical tail 6b.The radome fairing 1 of general-purpose aircraft, spiral
Paddle 2, head sub-assembly 3, fuselage sub-assembly 4, wing sub-assembly 5,6 six part of empennage sub-assembly are carbon fibre composite system
It forms.
Described carbon fibre composite is to be bonded 3K carbon cloth using epoxy resin and curing agent.
The working principle of the invention is: the general-purpose aircraft that the present invention uses carbon fibre composite to make is for two people driving
Cubpiston and design, main structure includes: radome fairing 1, propeller 2, head sub-assembly 3, fuselage sub-assembly
4, wing sub-assembly 5, empennage sub-assembly 6.Wherein head sub-assembly 3 includes head upper housing 3a, head lower case 3b, front-wheel guarantor
Protective case body 3c and connector frame 3d, fuselage sub-assembly 4 include instrument tank tower 4a, preceding floor 4b, control tank tower 4c, cockpit side plate
4d, handrail transition frame 4e, seat 4f, wing mount brackets 4g, rear floor 4h, backsight cabin 4i and rear body cabin 4j, wing group
Component 5 includes upside wing and downside wing, and empennage sub-assembly 6 includes tailplane 6a and vertical tail 6b, structure are
Carbon fibre composite is made, and carbon fibre composite is to be bonded 3K carbon cloth using epoxy resin and curing agent.
One embodiment of the present of invention, it is finished product that carbon pricker, which ties up epoxy resin, curing agent, the 3K carbon cloth that composite material uses,
Material.
Claims (2)
1. a kind of general-purpose aircraft made of carbon fibre composite, which is characterized in that it includes: radome fairing (1), propeller
(2), head sub-assembly (3), fuselage sub-assembly (4), wing sub-assembly (5), empennage sub-assembly (6).Wherein head sub-assembly (3)
Including head upper housing (3a), head lower case (3b), front-wheel protection shell (3c) and connector frame (3d), fuselage sub-assembly
It (4) include instrument tank tower (4a), preceding floor (4b), control tank tower (4c), cockpit side plate (4d), handrail transition frame (4e), seat
(4f), wing mount brackets (4g), rear floor (4h), backsight cabin (4i) and rear body cabin (4j), wing sub-assembly (5) include
Upside wing and downside wing, empennage sub-assembly (6) include tailplane (6a) and vertical tail (6b).The rectification of general-purpose aircraft
Cover (1), propeller (2), head sub-assembly (3), fuselage sub-assembly (4), wing sub-assembly (5), (6) six part of empennage sub-assembly
It is that carbon fibre composite is made.
2. a kind of general-purpose aircraft made of carbon fibre composite according to claim 1, which is characterized in that described
Carbon fibre composite be to be bonded 3K carbon cloth using epoxy resin and curing agent.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811523159.6A CN109484609A (en) | 2018-12-13 | 2018-12-13 | A kind of general-purpose aircraft made of carbon fibre composite |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811523159.6A CN109484609A (en) | 2018-12-13 | 2018-12-13 | A kind of general-purpose aircraft made of carbon fibre composite |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109484609A true CN109484609A (en) | 2019-03-19 |
Family
ID=65710172
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811523159.6A Pending CN109484609A (en) | 2018-12-13 | 2018-12-13 | A kind of general-purpose aircraft made of carbon fibre composite |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109484609A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2841502Y (en) * | 2005-10-28 | 2006-11-29 | 南京轻型飞机股份有限公司 | Light aircraft |
| CN105691586A (en) * | 2016-01-15 | 2016-06-22 | 中国人民解放军国防科学技术大学 | Small-sized light unmanned aerial vehicle structure with strike-resistant and impact dispersing and recycling functions |
| CN106741823A (en) * | 2016-12-30 | 2017-05-31 | 易瓦特科技股份公司 | Unmanned plane body prepared by composite and preparation method thereof |
| US20170152014A1 (en) * | 2015-10-07 | 2017-06-01 | Carbon Flyer LLC | Aircraft body and method of making the same |
| CN108502139A (en) * | 2018-04-28 | 2018-09-07 | 成都航空职业技术学院 | Three-wing-surface general-purpose aircraft |
-
2018
- 2018-12-13 CN CN201811523159.6A patent/CN109484609A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2841502Y (en) * | 2005-10-28 | 2006-11-29 | 南京轻型飞机股份有限公司 | Light aircraft |
| US20170152014A1 (en) * | 2015-10-07 | 2017-06-01 | Carbon Flyer LLC | Aircraft body and method of making the same |
| CN105691586A (en) * | 2016-01-15 | 2016-06-22 | 中国人民解放军国防科学技术大学 | Small-sized light unmanned aerial vehicle structure with strike-resistant and impact dispersing and recycling functions |
| CN106741823A (en) * | 2016-12-30 | 2017-05-31 | 易瓦特科技股份公司 | Unmanned plane body prepared by composite and preparation method thereof |
| CN108502139A (en) * | 2018-04-28 | 2018-09-07 | 成都航空职业技术学院 | Three-wing-surface general-purpose aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20190319 |
|
| WD01 | Invention patent application deemed withdrawn after publication |