CN203127145U - Carbon fiber composite aircraft - Google Patents
Carbon fiber composite aircraft Download PDFInfo
- Publication number
- CN203127145U CN203127145U CN 201320013948 CN201320013948U CN203127145U CN 203127145 U CN203127145 U CN 203127145U CN 201320013948 CN201320013948 CN 201320013948 CN 201320013948 U CN201320013948 U CN 201320013948U CN 203127145 U CN203127145 U CN 203127145U
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- China
- Prior art keywords
- frame
- main
- carbon fiber
- fiber composite
- cabin
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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.)
- Expired - Lifetime
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Abstract
The utility model discloses a carbon fiber composite aircraft, comprising a manned cabin and a paraglider, wherein the manned cabin is provided with a cabin frame made of a carbon fiber composite; a drive assembly is arranged at the rear of the cabin frame; the cabin frame comprises a left main support ring beam, a right main support ring beam and a frame carrier; the bottom parts of the two main support ring beams are connected through a plurality of transverse support bars; a front seat and a rear seat are arranged above the transverse support bars; a main front beam connecting rod is arranged between the two main support ring beams at the front part of the cabin frame; an arch front damping support rack is arranged at the middle part of the main front beam connecting rod; left and right rear damping support racks are respectively hinged with the left side and the right side of the rear part of the cabin frame; and a heavy load damping spring is arranged between the rear damping support rack and the frame carrier. The frame of the manned cabin is made of the carbon fiber composite, and damping supporters are arranged at front and rear wheels, so that not only is the weight of the manned cabin greatly reduced, but also passengers are enclosed inside the frame of the manned cabin. The landing impact force is greatly reduced, and the passengers are effectively protected.
Description
Technical field
The utility model 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 big, bears huge impact power during landing, lacks effective protection to taking the people.
Summary of the invention
The technical problems to be solved in the utility model is at the deficiencies in the prior art, has proposed a kind of from heavy and light, protection carbon fiber composite aircraft well.
The technical problems to be solved in the utility model 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 back of the body framves 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 preceding damping bracing frame is housed at the middle part of main front-axle beam pipe link; at the two ends, the left and right sides of preceding damping bracing frame two front-wheels are housed; damping bracing frame in back 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 back damping bracing frame; the heavy lift damping spring upwards and between the back of the body frame is equipped with in the middle part of back damping bracing 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 at back of the body frame; 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 back of the body frame.
The technical problems to be solved in the utility model can also be come to realize that further driving engine is provided with the oil cooling heat abstractor by the following technical programs.
The utility model compared with prior art; adopt carbon fiber composite material to make the framework in manned seat storehouse; front and back wheel is equipped with damping and supports; so not only alleviate the weight in manned seat storehouse greatly; and will take in the framework that the people wraps in manned seat storehouse; impulsive force significantly 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 preceding damping support frame 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 back of the body framves 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 preceding damping bracing 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 preceding damping bracing frame 1 two front-wheels 13 are housed; back damping bracing frame 7 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 back damping bracing frame 7; heavy lift damping spring 9 upwards and between the back of the body frame 4 is equipped with in the middle part of back damping bracing 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 at back of the body frame; 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 back of the body frame 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 (2)
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 back of the body framves 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 preceding damping bracing frame is housed at the middle part of main front-axle beam pipe link; at the two ends, the left and right sides of preceding damping bracing frame two front-wheels are housed; damping bracing frame in back 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 back damping bracing frame; the heavy lift damping spring upwards and between the back of the body frame is equipped with in the middle part of back damping bracing 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 at back of the body frame; 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 back of the body frame.
2. 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 |
|---|---|---|---|
| CN 201320013948 CN203127145U (en) | 2013-01-11 | 2013-01-11 | Carbon fiber composite aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320013948 CN203127145U (en) | 2013-01-11 | 2013-01-11 | Carbon fiber composite aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203127145U true CN203127145U (en) | 2013-08-14 |
Family
ID=48935148
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201320013948 Expired - Lifetime CN203127145U (en) | 2013-01-11 | 2013-01-11 | Carbon fiber composite aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203127145U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103043213A (en) * | 2013-01-11 | 2013-04-17 | 连云港神鹰碳纤维自行车有限责任公司 | Carbon fiber composite aircraft |
-
2013
- 2013-01-11 CN CN 201320013948 patent/CN203127145U/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103043213A (en) * | 2013-01-11 | 2013-04-17 | 连云港神鹰碳纤维自行车有限责任公司 | Carbon fiber composite aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 222000 No. 84 happiness Middle Road, Haizhou District, Jiangsu, Lianyungang Co-patentee after: LIANYUNGANG SHENYING CARBON FIBER BICYCLE CO.,LTD. Patentee after: Lianyungang Yingyan Novel Material Co.,Ltd. Address before: 222000 No. 84 happiness Middle Road, Haizhou District, Jiangsu, Lianyungang Co-patentee before: LIANYUNGANG SHENYING CARBON BIKE Co.,Ltd. Patentee before: Lianyungang Yingyan Novel Material Co.,Ltd. |
|
| CP01 | Change in the name or title of a patent holder | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20200303 Address after: 222000 Jiangsu province Lianyungang Dapu industrial zone of Lianyungang economic and Technological Development Zone Cloud Road No. 6 Patentee after: LIANYUNGANG SHENYING CARBON FIBER BICYCLE CO.,LTD. Address before: 222000 No. 84 happiness Middle Road, Haizhou District, Jiangsu, Lianyungang Co-patentee before: LIANYUNGANG SHENYING CARBON FIBER BICYCLE CO.,LTD. Patentee before: Lianyungang Yingyan Novel Material Co.,Ltd. |
|
| TR01 | Transfer of patent right | ||
| CX01 | Expiry of patent term |
Granted publication date: 20130814 |
|
| CX01 | Expiry of patent term |