CN105437633A - High-temperature-resisting protective film for UAV (unmanned aerial vehicle) - Google Patents
High-temperature-resisting protective film for UAV (unmanned aerial vehicle) Download PDFInfo
- Publication number
- CN105437633A CN105437633A CN201510851131.5A CN201510851131A CN105437633A CN 105437633 A CN105437633 A CN 105437633A CN 201510851131 A CN201510851131 A CN 201510851131A CN 105437633 A CN105437633 A CN 105437633A
- Authority
- CN
- China
- Prior art keywords
- layer
- protective film
- resisting
- temperature
- high temperature
- 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
- 230000001681 protective effect Effects 0.000 title abstract 9
- 239000010410 layer Substances 0.000 claims abstract description 24
- 229920000049 Carbon (fiber) Polymers 0.000 claims abstract description 12
- 239000004917 carbon fiber Substances 0.000 claims abstract description 12
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims abstract description 12
- 239000003973 paint Substances 0.000 claims abstract description 11
- 239000011241 protective layer Substances 0.000 claims abstract description 11
- 238000005299 abrasion Methods 0.000 claims description 9
- 239000011248 coating agent Substances 0.000 claims description 3
- 238000000576 coating method Methods 0.000 claims description 3
- 230000009970 fire resistant effect Effects 0.000 claims description 3
- 230000001771 impaired effect Effects 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000004590 computer program Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 241000282326 Felis catus Species 0.000 description 1
- 230000006399 behavior Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000004088 simulation Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
- B32B9/005—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising one layer of ceramic material, e.g. porcelain, ceramic tile
- B32B9/007—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising one layer of ceramic material, e.g. porcelain, ceramic tile comprising carbon, e.g. graphite, composite carbon
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B33/00—Layered products characterised by particular properties or particular surface features, e.g. particular surface coatings; Layered products designed for particular purposes not covered by another single class
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/106—Carbon fibres, e.g. graphite fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/30—Properties of the layers or laminate having particular thermal properties
- B32B2307/306—Resistant to heat
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Professional, Industrial, Or Sporting Protective Garments (AREA)
Abstract
The invention discloses a high-temperature-resisting protective film for a UAV (unmanned aerial vehicle). The high-temperature-resisting protective film comprises a high-temperature-resisting protective film body, a flame-retarding protective film, a wear-resisting layer, a carbon fiber layer and a nano-paint protective layer, wherein the flame-retarding protective film is arranged on the outer side of the high-temperature-resisting protective film body; the wear-resisting layer is arranged on the outer side of the flame-retarding protective film; the carbon fiber layer is arranged on the outer side of the wear-resisting layer; the nano-paint protective layer is arranged on the outer side of the carbon fiber layer. With adoption of the scheme, the high-temperature-resisting protective film for the UAV is simple in structure and can protect the UAV from being damaged easily at a high temperature.
Description
Technical field
The present invention relates to novel robot field, particularly relate to the high temperature resistant diaphragm of a kind of unmanned plane.
Background technology
Robot comprises the machinery (as robot dog, machine cat, robot vehicle etc.) of all simulating human behaviors or thought and simulation other biological.Also have a lot of classification and dispute to the definition of robot in the narrow sense, some computer program is even also referred to as robot.In contemporary industry, robot refers to the man-made machine device that can automatically perform task, in order to replace or to assist human work, can be generally electromechanical assembly, by computer program or electronic circuit control.
Summary of the invention
The technical problem that the present invention mainly solves is to provide the high temperature resistant diaphragm of a kind of unmanned plane, and structure is simple, unmanned plane can be protected not to be subject to high temperature impaired.
For solving the problems of the technologies described above; the technical scheme that the present invention adopts is: provide a kind of unmanned plane high temperature resistant diaphragm; comprise: high temperature resistant diaphragm body, fire-resisting protection film, anti abrasion layer, carbon fiber layer and nano-paint protective layer; the outside of described high temperature resistant diaphragm body is provided with fire-resisting protection film; anti abrasion layer is provided with outside described fire-resisting protection film; the outside of described anti abrasion layer is provided with carbon fiber layer, and the outside of described carbon fiber layer is provided with nano-paint protective layer.
In a preferred embodiment of the present invention, the thickness of described fire-resisting protection film is 0.8-1.6cm.
In a preferred embodiment of the present invention, the surface of described nano-paint protective layer scribbles fire resistant coating.
The invention has the beneficial effects as follows: the high temperature resistant diaphragm of unmanned plane of the present invention, structure is simple, unmanned plane can be protected not to be subject to high temperature impaired.
Detailed description of the invention
Be clearly and completely described to the technical scheme in the embodiment of the present invention below, obviously, described embodiment is only a part of embodiment of the present invention, instead of whole embodiments.Based on the embodiment in the present invention, those of ordinary skill in the art, not making other embodiments all obtained under creative work prerequisite, belong to the scope of protection of the invention.
The embodiment of the present invention comprises:
The high temperature resistant diaphragm of a kind of unmanned plane; comprise: high temperature resistant diaphragm body, fire-resisting protection film, anti abrasion layer, carbon fiber layer and nano-paint protective layer; the outside of described high temperature resistant diaphragm body is provided with fire-resisting protection film; anti abrasion layer is provided with outside described fire-resisting protection film; the outside of described anti abrasion layer is provided with carbon fiber layer, and the outside of described carbon fiber layer is provided with nano-paint protective layer.
In addition, the thickness of described fire-resisting protection film is 0.8-1.6cm.
In addition, the surface of described nano-paint protective layer scribbles fire resistant coating.
The unmanned plane of the present invention beneficial effect of high temperature resistant diaphragm is:
Structure is simple, unmanned plane can be protected not to be subject to high temperature impaired.
The foregoing is only embodiments of the invention; not thereby the scope of the claims of the present invention is limited; every utilize description of the present invention to do equivalent structure or equivalent flow process conversion; or be directly or indirectly used in other relevant technical field, be all in like manner included in scope of patent protection of the present invention.
Claims (3)
1. the high temperature resistant diaphragm of unmanned plane; it is characterized in that; comprise: high temperature resistant diaphragm body, fire-resisting protection film, anti abrasion layer, carbon fiber layer and nano-paint protective layer; the outside of described high temperature resistant diaphragm body is provided with fire-resisting protection film; anti abrasion layer is provided with outside described fire-resisting protection film; the outside of described anti abrasion layer is provided with carbon fiber layer, and the outside of described carbon fiber layer is provided with nano-paint protective layer.
2. the high temperature resistant diaphragm of unmanned plane according to claim 1, is characterized in that, the thickness of described fire-resisting protection film is 0.8-1.6cm.
3. the high temperature resistant diaphragm of unmanned plane according to claim 1, is characterized in that, the surface of described nano-paint protective layer scribbles fire resistant coating.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510851131.5A CN105437633A (en) | 2015-11-30 | 2015-11-30 | High-temperature-resisting protective film for UAV (unmanned aerial vehicle) |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510851131.5A CN105437633A (en) | 2015-11-30 | 2015-11-30 | High-temperature-resisting protective film for UAV (unmanned aerial vehicle) |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105437633A true CN105437633A (en) | 2016-03-30 |
Family
ID=55548480
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510851131.5A Pending CN105437633A (en) | 2015-11-30 | 2015-11-30 | High-temperature-resisting protective film for UAV (unmanned aerial vehicle) |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105437633A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110558856A (en) * | 2019-10-18 | 2019-12-13 | 珠海格力电器股份有限公司 | Baking tray with flying function, oven and use method of oven |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101011874A (en) * | 2007-01-22 | 2007-08-08 | 浙江大学 | Lightening fire resistant polymer porous membrane laminated composite material and manufacturing method thereof |
| CN102241166A (en) * | 2011-04-15 | 2011-11-16 | 天津全华时代航天科技发展有限公司 | Special-purposed cellular composite material used for small unmanned air vehicle |
| CN102267264A (en) * | 2011-05-16 | 2011-12-07 | 苏州斯迪克电子胶粘材料有限公司 | Ultrasonic sealing film for preparing insulating sealable bags on inside walls of aircrafts, and preparation method thereof |
| KR20120080838A (en) * | 2011-01-10 | 2012-07-18 | 율촌화학 주식회사 | Lamination film coated by carbon |
| CN203982843U (en) * | 2014-06-17 | 2014-12-03 | 昆山市新智成电子科技有限公司 | A kind of antistatic flexible electric wire |
-
2015
- 2015-11-30 CN CN201510851131.5A patent/CN105437633A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101011874A (en) * | 2007-01-22 | 2007-08-08 | 浙江大学 | Lightening fire resistant polymer porous membrane laminated composite material and manufacturing method thereof |
| KR20120080838A (en) * | 2011-01-10 | 2012-07-18 | 율촌화학 주식회사 | Lamination film coated by carbon |
| CN102241166A (en) * | 2011-04-15 | 2011-11-16 | 天津全华时代航天科技发展有限公司 | Special-purposed cellular composite material used for small unmanned air vehicle |
| CN102267264A (en) * | 2011-05-16 | 2011-12-07 | 苏州斯迪克电子胶粘材料有限公司 | Ultrasonic sealing film for preparing insulating sealable bags on inside walls of aircrafts, and preparation method thereof |
| CN203982843U (en) * | 2014-06-17 | 2014-12-03 | 昆山市新智成电子科技有限公司 | A kind of antistatic flexible electric wire |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110558856A (en) * | 2019-10-18 | 2019-12-13 | 珠海格力电器股份有限公司 | Baking tray with flying function, oven and use method of oven |
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| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20160330 |
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| WD01 | Invention patent application deemed withdrawn after publication |