CN103043213A - Carbon fiber composite aircraft - Google Patents
Carbon fiber composite aircraft Download PDFInfo
- Publication number
- CN103043213A CN103043213A CN2013100103408A CN201310010340A CN103043213A CN 103043213 A CN103043213 A CN 103043213A CN 2013100103408 A CN2013100103408 A CN 2013100103408A CN 201310010340 A CN201310010340 A CN 201310010340A CN 103043213 A CN103043213 A CN 103043213A
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- main
- carbon fiber
- fiber composite
- seat
- frame
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Abstract
The invention discloses a carbon fiber composite aircraft which comprises a manned seat bin and a paragliding, wherein the manned seat bin is provided with a seat bin framework made of a carbon fiber composite material; a driving assembly is arranged at the rear part of the seat bin framework; the seat bin framework comprises a left main supporting ring beam, a right main supporting ring beam and a back frame; the bottoms of the two main supporting ring beams are connected with each other through a plurality of transverse supporting rods; a front seat and a rear seat are arranged above the transverse supporting rods; a main front beam connection rod is arranged between the two main supporting ring beams on the front part of the seat bin framework; an arched front shock absorption supporting frame is arranged in the middle of the main front beam connection rod; the left side and the right side of the rear part of the seat bin framework are respectively hinged with a left rear shock absorption supporting frame and a right rear shock absorption supporting frame; and heavy load shock absorption springs are arranged between the rear shock absorption supporting frames. Shock absorption supports are arranged on front wheels and rear wheels of the manned seat bin framework made of the carbon fiber composite material, so that the weight of the manned seat bin is greatly reduced, and a passenger is wrapped in the manned seat bin framework; when the aircraft is landed, impact is greatly reduced; and the passenger is effectively protected.
Description
Technical field
The present invention relates to a kind of low-latitude flying equipment, particularly a kind of carbon fiber composite aircraft.
Background technology
In the prior art, low flyer generally comprises seat storehouse and the Aircraft of drive, and its weak point is that manned seat storehouse weight is large, bears huge impulsive force during landing, lacks effective protection to taking the people.
Summary of the invention
The technical problem to be solved in the present invention is for the deficiencies in the prior art, has proposed a kind of from heavy and light, protection carbon fiber composite aircraft well.
The technical problem to be solved in the present invention is achieved through the following technical solutions; a kind of carbon fiber composite aircraft; comprise manned seat storehouse and Aircraft; be characterized in: described manned seat storehouse is provided with the seat Hatch Coaming frame of being made by carbon fiber composite material; the driving assembly is equipped with at present Hatch Coaming frame rear portion; two main collar tie beam and backrests of supporting about seat Hatch Coaming frame comprises; two main bottoms of supporting collar tie beam connect by some transverse support bar; front seats and back seats is housed above transverse support bar; two main the supports between the collar tie beam in the front portion of present Hatch Coaming frame are provided with main front-axle beam pipe link; arc front shock-absorbing support frame is housed at the middle part of main front-axle beam pipe link; at the two ends, the left and right sides of front shock-absorbing support frame two front-wheels are housed; shock-absorbing support frame after about the left and right sides, rear portion of present Hatch Coaming frame is hinged with respectively; trailing wheel all is equipped with in outer end at rear shock-absorbing support frame; the heavy lift damping spring upwards and between the backrest is equipped with in the middle part of rear shock-absorbing support frame; two main the supports between the collar tie beam in the top of present Hatch Coaming frame are provided with the instrument mounting rod; drive assembly and be provided with engine-driven screw propeller; be provided with engine bed in backrest; driving engine is contained on the engine bed; periphery at screw propeller is provided with the back up ring, and described back up ring joins by guard bar support and backrest.
The technical problem to be solved in the present invention can also be come to realize that further described back up ring and guard bar support are made one-shot forming by carbon fiber composite material by the following technical programs.
The technical problem to be solved in the present invention can also be come to realize that further driving engine is provided with the oil cooling heat abstractor by the following technical programs.
The present invention compared with prior art; adopt carbon fiber composite material to make the framework in manned seat storehouse; front and back wheel is equipped with shock-absorbing support; so not only greatly alleviate the weight in manned seat storehouse; and will take in the framework that the people wraps in manned seat storehouse; impulsive force greatly reduces when landing, and plays the actv. protective effect to taking the people.
Description of drawings
Fig. 1 is constructional drawing of the present invention;
Fig. 2 is front shock-absorbing support shelf structure figure;
Fig. 3 is heavy lift damping spring erection plan.
The specific embodiment
A kind of carbon fiber composite aircraft; comprise manned seat storehouse and Aircraft; described manned seat storehouse is provided with the seat Hatch Coaming frame of being made by carbon fiber composite material; the driving assembly is equipped with at present Hatch Coaming frame rear portion; two main collar tie beam 2 and backrests 4 of supporting about seat Hatch Coaming frame comprises; two main bottoms of supporting collar tie beam connect by some transverse support bar 10; front chair 12 is housed above transverse support bar 10; back seat 11; two main the supports between the collar tie beam in the front portion of present Hatch Coaming frame are provided with main front-axle beam pipe link; arc front shock-absorbing support frame 1 is housed at the middle part of main front-axle beam pipe link; at the two ends, the left and right sides of front shock-absorbing support frame 1 two front-wheels 13 are housed; shock-absorbing support frame 7 after about the left and right sides, rear portion of present Hatch Coaming frame is hinged with respectively; trailing wheel 8 all is equipped with in outer end at rear shock-absorbing support frame 7; heavy lift damping spring 9 upwards and between the backrest 4 is equipped with in the middle part of rear shock-absorbing support frame 8; two main the supports between the collar tie beam in the top of present Hatch Coaming frame are provided with instrument mounting rod 3; drive assembly and be provided with engine-driven screw propeller; be provided with engine bed in backrest; driving engine is contained on the engine bed; periphery at screw propeller is provided with back up ring 6, and described back up ring 6 joins by guard bar support 5 and backrest 4.Driving engine is provided with the oil cooling heat abstractor.
Described back up ring and guard bar support are made one-shot forming by carbon fiber composite material.
The rotation of engine drive screw propeller produces power, and slide forward in manned seat storehouse, adjusts the angle of Aircraft, makes it to produce lift upwards, just can take off.
Claims (3)
1. carbon fiber composite aircraft; comprise manned seat storehouse and Aircraft; it is characterized in that: described manned seat storehouse is provided with the seat Hatch Coaming frame of being made by carbon fiber composite material; the driving assembly is equipped with at present Hatch Coaming frame rear portion; two main collar tie beam and backrests of supporting about seat Hatch Coaming frame comprises; two main bottoms of supporting collar tie beam connect by some transverse support bar; front seats and back seats is housed above transverse support bar; two main the supports between the collar tie beam in the front portion of present Hatch Coaming frame are provided with main front-axle beam pipe link; arc front shock-absorbing support frame is housed at the middle part of main front-axle beam pipe link; at the two ends, the left and right sides of front shock-absorbing support frame two front-wheels are housed; shock-absorbing support frame after about the left and right sides, rear portion of present Hatch Coaming frame is hinged with respectively; trailing wheel all is equipped with in outer end at rear shock-absorbing support frame; the heavy lift damping spring upwards and between the backrest is equipped with in the middle part of rear shock-absorbing support frame; two main the supports between the collar tie beam in the top of present Hatch Coaming frame are provided with the instrument mounting rod; drive assembly and be provided with engine-driven screw propeller; be provided with engine bed in backrest; driving engine is contained on the engine bed; periphery at screw propeller is provided with the back up ring, and described back up ring joins by guard bar support and backrest.
2. carbon fiber composite aircraft according to claim 1, it is characterized in that: described back up ring and guard bar support are made one-shot forming by carbon fiber composite material.
3. carbon fiber composite aircraft according to claim 1, it is characterized in that: driving engine is provided with the oil cooling heat abstractor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013100103408A CN103043213A (en) | 2013-01-11 | 2013-01-11 | Carbon fiber composite aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013100103408A CN103043213A (en) | 2013-01-11 | 2013-01-11 | Carbon fiber composite aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103043213A true CN103043213A (en) | 2013-04-17 |
Family
ID=48056116
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2013100103408A Pending CN103043213A (en) | 2013-01-11 | 2013-01-11 | Carbon fiber composite aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103043213A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110549638A (en) * | 2019-09-06 | 2019-12-10 | 杭州友凯船艇有限公司 | Technical scheme for preventing composite material of fiber reinforced plastic base material from brittle failure |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2581614A1 (en) * | 1985-05-13 | 1986-11-14 | Gallas Yves Jean | Aircraft of the motorised microlight or very light category with optimum safety |
| CN2551571Y (en) * | 2002-06-13 | 2003-05-21 | 张长义 | Triangular wing aircraft |
| US20050230521A1 (en) * | 2003-09-23 | 2005-10-20 | Medsker James A | Powerchute apparatus |
| WO2006023885A2 (en) * | 2004-08-24 | 2006-03-02 | Howard Kenneth D | Flying all-terrain vehicle |
| CN201095422Y (en) * | 2007-06-13 | 2008-08-06 | 杨玉德 | Aircraft |
| CN102774261A (en) * | 2012-07-25 | 2012-11-14 | 无锡市中捷减震器有限公司 | Shock-absorbing device for engine support |
| CN203127145U (en) * | 2013-01-11 | 2013-08-14 | 连云港迎雁新材料有限责任公司 | Carbon fiber composite aircraft |
-
2013
- 2013-01-11 CN CN2013100103408A patent/CN103043213A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2581614A1 (en) * | 1985-05-13 | 1986-11-14 | Gallas Yves Jean | Aircraft of the motorised microlight or very light category with optimum safety |
| CN2551571Y (en) * | 2002-06-13 | 2003-05-21 | 张长义 | Triangular wing aircraft |
| US20050230521A1 (en) * | 2003-09-23 | 2005-10-20 | Medsker James A | Powerchute apparatus |
| WO2006023885A2 (en) * | 2004-08-24 | 2006-03-02 | Howard Kenneth D | Flying all-terrain vehicle |
| CN201095422Y (en) * | 2007-06-13 | 2008-08-06 | 杨玉德 | Aircraft |
| CN102774261A (en) * | 2012-07-25 | 2012-11-14 | 无锡市中捷减震器有限公司 | Shock-absorbing device for engine support |
| CN203127145U (en) * | 2013-01-11 | 2013-08-14 | 连云港迎雁新材料有限责任公司 | Carbon fiber composite aircraft |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110549638A (en) * | 2019-09-06 | 2019-12-10 | 杭州友凯船艇有限公司 | Technical scheme for preventing composite material of fiber reinforced plastic base material from brittle failure |
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| PB01 | Publication | ||
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| C12 | Rejection of a patent application after its publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20130417 |