CN110027716A - A kind of installation method of aircraft engine air inlet protection sheet - Google Patents
A kind of installation method of aircraft engine air inlet protection sheet Download PDFInfo
- Publication number
- CN110027716A CN110027716A CN201910434457.6A CN201910434457A CN110027716A CN 110027716 A CN110027716 A CN 110027716A CN 201910434457 A CN201910434457 A CN 201910434457A CN 110027716 A CN110027716 A CN 110027716A
- Authority
- CN
- China
- Prior art keywords
- protection sheet
- installation
- air inlet
- aircraft engine
- engine air
- 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.)
- Withdrawn
Links
- 238000009434 installation Methods 0.000 title claims abstract description 57
- 238000000034 method Methods 0.000 title claims abstract description 19
- 230000015572 biosynthetic process Effects 0.000 claims 1
- 238000011900 installation process Methods 0.000 abstract description 5
- 230000007123 defense Effects 0.000 abstract description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
Classifications
-
- 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
- B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Details Of Aerials (AREA)
Abstract
The present invention discloses a kind of installation method of aircraft engine air inlet protection sheet, comprising the following steps: a. is inflated protection sheet；B. protection sheet supports certain prefabricated shape, reaches installation strength；C. installation protects sheet to engine intake radome fairing；The present invention is to need more people's operations, using improving in installation ladder, the installation mode that time-consuming in the installation of traditional defense sheet, and protection sheet installation uses airing form, and installation process is simple, without using installation ladder, operator is rapidly completed, and reduces labor intensity, manpower is saved, is improved efficiency.
Description
Technical field
The present invention relates to aircraft engine air inlets to protect sheet installing area, especially a kind of aircraft engine air inlet
Protect the installation method of sheet.
Background technique
Existing aircraft engine air inlet protection sheet generallys use ladder mode and installs, aircraft engine outer dimension one
As it is larger, engine head can not be realized easily on ground and be mounted directly between the 2.5-3.5m of ground, conventional mounting
Mode needs several operators to be climbed to engine head position using installation ladder and installed, and time-consuming for installation, pushes away ladder back and forth
Great work intensity.
Summary of the invention
In order to solve the more people's operations of available engine protection sheet installation process, the high, installation using the terraced working strength of installation
Personnel are more and install the problem of time-consuming, and the present invention provides a kind of installation method of aircraft engine air inlet protection sheet.
Technical purpose of the invention is achieved through the following technical solutions: a kind of peace of aircraft engine air inlet protection sheet
Dress method, passes through following steps: a. is inflated protection sheet；B. protection sheet supports certain prefabricated shape, reaches peace
Fill intensity；C. installation protects sheet to engine intake radome fairing；Installation process is easy to operate, can be terraced without using installation,
Entire installation is rapidly completed in operator.
The installation method of aircraft engine air inlet protection sheet according to the present invention, comprising the following steps:
A. protection sheet is inflated；B. protection sheet supports certain prefabricated shape, reaches installation strength；C. installation protection
Sheet is to engine intake radome fairing.
In step a, the protection sheet is inflatable.
In stepb, the protection sheet fitting design is matched with engine intake radome fairing outer dimension.
In step c, protection sheet two sides are sewed with symmetrical puller strap, and puller strap is connect with stretch cord；Protect sheet bullet
Power rope one end hangs with hook and is affixed on engine tail nozzle, for fixed entire protection sheet.
In step c, after protection sheet installation, fitting package cowling shape.
The present invention is to need more people operation, enterprising using installation ladder, the installation mode that time-consuming in the installation of traditional defense sheet
Row improves, and protection sheet uses airing form, and pass through following steps: a. is inflated protection sheet；B. protection sheet support
Certain prefabricated shape is played, installation strength is reached；C. installation protects sheet to engine intake radome fairing；Installation process operation letter
Single, without using installation ladder, operator is rapidly completed.
The beneficial effects of the present invention are: the installation method of 1, the protection sheet, installation is lifted after inflatable, it is light easy
Operation is saved artificial.
2, the installation method of the protection sheet shortens the set-up time, reduces labor intensity without installing ladder.
3, the installation method of the protection sheet, simple installation, disassembly are easy, save manpower, improve efficiency.
Detailed description of the invention
Present invention will be further explained below with reference to the attached drawings and examples.
The scheme of installation of the installation method of aircraft engine air inlet protection sheet of the invention is shown in Fig. 1.
Specific embodiment
The scheme of installation of the installation method of aircraft engine air inlet protection sheet of the invention is shown in Fig. 1.Root
According to the installation method of aircraft engine air inlet protection sheet of the invention, comprising the following steps: a. fills protection sheet
Gas；B. protection sheet supports certain prefabricated shape, reaches installation strength；C. installation protection sheet is rectified to engine intake
Cover.
In step a, the protection sheet is inflatable.
In stepb, the protection sheet fitting design is matched with engine intake radome fairing outer dimension.
In step c, protection sheet two sides are sewed with symmetrical puller strap, and puller strap is connect with stretch cord；Protect sheet bullet
Power rope one end hangs with hook and is affixed on engine tail nozzle, for fixed entire protection sheet.
In step c, after protection sheet installation, fitting package cowling shape.
The present invention is to need more people operation, enterprising using installation ladder, the installation mode that time-consuming in the installation of traditional defense sheet
Row improves, and protects the installation of sheet using airing form, passes through following steps: a. is inflated protection sheet；B. protective cloth
Cover supports certain prefabricated shape, reaches installation strength；C. installation protects sheet to engine intake radome fairing；Installation process
Easy to operate, without using installation ladder, operator is quickly interior to be completed, and is reduced labor intensity, is saved manpower, improve efficiency.
Claims (5)
1. a kind of installation method of aircraft engine air inlet protection sheet, which comprises the following steps:
A. protection sheet is inflated；
B. protection sheet supports certain prefabricated shape, reaches installation strength；
C. installation protects sheet to engine intake radome fairing.
2. the installation method of aircraft engine air inlet protection sheet according to claim 1, which is characterized in that in step
In a, the protection sheet is inflatable.
3. the installation method of aircraft engine air inlet protection sheet according to claim 1, which is characterized in that in step
In b, after the protection sheet inflation, formation and engine intake radome fairing size matched prefabricated shape are bonded after installation
Cowling shape is wrapped up, when storage, openable gas nozzle was deflated.
4. the installation method of aircraft engine air inlet protection sheet according to claim 1, which is characterized in that in step
In c, after the protection sheet inflation, lifts and be installed to engine intake radome fairing.
5. the installation method of aircraft engine air inlet protection sheet according to claim 1, which is characterized in that in step
In c, protection sheet two sides are sewed with symmetrical puller strap, and puller strap is connect with stretch cord, and one end hangs with hook and is affixed to engine
On nozzle, for fixed entire protection sheet.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910434457.6A CN110027716A (en) | 2019-05-23 | 2019-05-23 | A kind of installation method of aircraft engine air inlet protection sheet |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910434457.6A CN110027716A (en) | 2019-05-23 | 2019-05-23 | A kind of installation method of aircraft engine air inlet protection sheet |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110027716A true CN110027716A (en) | 2019-07-19 |
Family
ID=67243091
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910434457.6A Withdrawn CN110027716A (en) | 2019-05-23 | 2019-05-23 | A kind of installation method of aircraft engine air inlet protection sheet |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110027716A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110550227A (en) * | 2019-09-14 | 2019-12-10 | 山东威西特斯航空科技有限公司 | Installation method of aircraft engine air inlet protective cover |
| CN111169652A (en) * | 2019-11-15 | 2020-05-19 | 陕西飞机工业（集团）有限公司 | Engine tail spout protective equipment |
| WO2021007761A1 (en) * | 2019-07-16 | 2021-01-21 | 田庆亮 | Method for mounting protective fabric cover at air inlet of aircraft engine |
| WO2021051243A1 (en) * | 2019-09-16 | 2021-03-25 | 田庆亮 | Method for installing air inlet duct protective cover of aircraft engine |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2761407A1 (en) * | 1997-03-28 | 1998-10-02 | Zodiac Int | Thermal camouflage for motor vehicle internal combustion engine |
| CN1326527A (en) * | 1998-09-25 | 2001-12-12 | 伊恩·杰勒德·内格尔 | inflatable shed |
| DE10333720A1 (en) * | 2003-07-23 | 2005-03-03 | Theo Koutsoulas | Hail protection cover, especially for motor vehicles is inflatable and has end piece for inflating it that can be connected to exhaust tail pipe of motor vehicle; end piece can be adapted to cross-section of exhaust tail pipe |
| CN101885383A (en) * | 2009-05-12 | 2010-11-17 | 刘铁华 | Aircraft engine protective cover |
| CN201980059U (en) * | 2011-03-16 | 2011-09-21 | 凌昕 | Inflatable car protective clothing cover |
| CN204327338U (en) * | 2014-11-14 | 2015-05-13 | 中国商用飞机有限责任公司 | Engine air inlet protective cover |
| CN104608932A (en) * | 2014-12-19 | 2015-05-13 | 江阴古贝叶工业技术开发有限公司 | Aircraft engine protective device |
| CN206267572U (en) * | 2016-11-30 | 2017-06-20 | 春秋航空技术发展江苏有限公司 | Aircraft engine mobile working canopy |
| CN107939526A (en) * | 2016-10-12 | 2018-04-20 | 通用电气公司 | Inlet cowl for a turbine engine |
-
2019
- 2019-05-23 CN CN201910434457.6A patent/CN110027716A/en not_active Withdrawn
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2761407A1 (en) * | 1997-03-28 | 1998-10-02 | Zodiac Int | Thermal camouflage for motor vehicle internal combustion engine |
| CN1326527A (en) * | 1998-09-25 | 2001-12-12 | 伊恩·杰勒德·内格尔 | inflatable shed |
| DE10333720A1 (en) * | 2003-07-23 | 2005-03-03 | Theo Koutsoulas | Hail protection cover, especially for motor vehicles is inflatable and has end piece for inflating it that can be connected to exhaust tail pipe of motor vehicle; end piece can be adapted to cross-section of exhaust tail pipe |
| CN101885383A (en) * | 2009-05-12 | 2010-11-17 | 刘铁华 | Aircraft engine protective cover |
| CN201980059U (en) * | 2011-03-16 | 2011-09-21 | 凌昕 | Inflatable car protective clothing cover |
| CN204327338U (en) * | 2014-11-14 | 2015-05-13 | 中国商用飞机有限责任公司 | Engine air inlet protective cover |
| CN104608932A (en) * | 2014-12-19 | 2015-05-13 | 江阴古贝叶工业技术开发有限公司 | Aircraft engine protective device |
| CN107939526A (en) * | 2016-10-12 | 2018-04-20 | 通用电气公司 | Inlet cowl for a turbine engine |
| CN206267572U (en) * | 2016-11-30 | 2017-06-20 | 春秋航空技术发展江苏有限公司 | Aircraft engine mobile working canopy |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2021007761A1 (en) * | 2019-07-16 | 2021-01-21 | 田庆亮 | Method for mounting protective fabric cover at air inlet of aircraft engine |
| CN110550227A (en) * | 2019-09-14 | 2019-12-10 | 山东威西特斯航空科技有限公司 | Installation method of aircraft engine air inlet protective cover |
| WO2021051243A1 (en) * | 2019-09-16 | 2021-03-25 | 田庆亮 | Method for installing air inlet duct protective cover of aircraft engine |
| CN111169652A (en) * | 2019-11-15 | 2020-05-19 | 陕西飞机工业（集团）有限公司 | Engine tail spout protective equipment |
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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 | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20190719 |