CN2903421Y - Bullet shape airplane turbine protecting cover - Google Patents
Bullet shape airplane turbine protecting cover Download PDFInfo
- Publication number
- CN2903421Y CN2903421Y CN 200620083002 CN200620083002U CN2903421Y CN 2903421 Y CN2903421 Y CN 2903421Y CN 200620083002 CN200620083002 CN 200620083002 CN 200620083002 U CN200620083002 U CN 200620083002U CN 2903421 Y CN2903421 Y CN 2903421Y
- Authority
- CN
- China
- Prior art keywords
- protective cover
- protecting cover
- airplane
- bullet shape
- airplane turbine
- 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.)
- Expired - Fee Related
Links
- 230000001681 protective Effects 0.000 claims abstract description 17
- 241000271566 Aves Species 0.000 abstract 2
- 230000003014 reinforcing Effects 0.000 abstract 1
- 238000000034 method Methods 0.000 description 2
- 238000005266 casting Methods 0.000 description 1
Abstract
The utility model discloses a stray bullet shaped airplane turbine protective cover which belongs to a protective cover and comprises a protective cover body which is basically cone-shaped composed of a longitudinal stud and a transverse reinforcing rib. An installment board is fixed at the lower end of the protective cover body. The airplane turbine protective cover has reasonable structure and can effectively prevents birds from entering the engine after installed at the air inlet end of the airplane turbine engine, thereby allowing for low level fly and gliding when the airplane gets out of order instead of high level fly to avoid birds, which improves the fly safety and reduces the possibilities of accidents.
Description
Technical field
The utility model provides a kind of protective equipment, especially a kind of usefulness protective equipment aboard.
Background technique
Existing aircraft does not all have protective equipment as the inlet end of the turbogenerator of airliner, transport airplane, can not prevent effectively that flying objects such as flying bird, balloon from entering in the engine turbine.Therefore, near existing airport, scarer to be set, in the landing process of aircraft, bump against preventing with flying bird.But, when in the flight course of aircraft, breaking down,,, can not carry out low-latitude flying, thereby reduce the Security of flight for hiding flying bird etc. owing to there is not protective equipment, improved possibility of accident occurrence.
Summary of the invention
Technical problem to be solved in the utility model is, a kind of stray bullet shape aircraft turbine protective housing is provided, and it can prevent effectively that flying bird etc. from entering in the aircraft turbine engine, improves the Security of aircraft flight.
The utility model is achieved in that stray bullet shape aircraft turbine protective housing, and it has tapered basically protecting cover, and protecting cover is made of stud longitudinally and the horizontal stiffening rib that is fixed on the stud, and the protecting cover lower end is fixed with mounting plate.
Adopt the stray bullet shape aircraft turbine protective housing of said structure, rational in infrastructure, be installed on the inlet end of aircraft turbine engine after, can prevent effectively that flying bird from entering in the motor.Like this, when aircraft breaks down, but low-latitude flying or glide, needn't be for hiding flying bird etc. in high-altitude flight, thus improved the Security of flight, reduced possibility of accident occurrence.
Description of drawings
Fig. 1 is the schematic representation of the utility model structure.
Fig. 2 is the plan view of Fig. 1.
Embodiment
The embodiment who provides below in conjunction with accompanying drawing illustrates concrete structure of the present utility model.
As shown in drawings, the stray bullet shape aircraft turbine protective housing of the utility model, it has tapered basically protecting cover (1), and protecting cover is made of stud (1-1) longitudinally and the horizontal stiffening rib (1-2) that is fixed on the stud, and the protecting cover lower end is fixed with mounting plate (2).
Basically tapered protecting cover profile approaches stray bullet shape.Stud, stiffening rib constitute tower structure, and whole protective roof can be by casting disposable making.Mounting plate ringwise.
During use, can utilize bolt this protective housing to be fixed on the inlet end of aircraft turbine engine by the hole on the mounting plate (3).When flying bird etc. bumped against the protecting cover middle, impact force was disperseed by the whole protection cover body.When bumping against the side of protecting cover, flying bird is slipped over along the protecting cover outer surface.Like this, just can prevent the danger that flying bird is caused aircraft flight.
Claims (1)
1, stray bullet shape aircraft turbine protective housing, it is characterized in that, it has tapered basically protecting cover (1), and protecting cover is made of stud (1-1) longitudinally and the horizontal stiffening rib (1-2) that is fixed on the stud, and the protecting cover lower end is fixed with mounting plate (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200620083002 CN2903421Y (en) | 2006-04-12 | 2006-04-12 | Bullet shape airplane turbine protecting cover |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200620083002 CN2903421Y (en) | 2006-04-12 | 2006-04-12 | Bullet shape airplane turbine protecting cover |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2903421Y true CN2903421Y (en) | 2007-05-23 |
Family
ID=38078832
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200620083002 Expired - Fee Related CN2903421Y (en) | 2006-04-12 | 2006-04-12 | Bullet shape airplane turbine protecting cover |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2903421Y (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2011091591A1 (en) * | 2010-01-29 | 2011-08-04 | Zhang Haihu | Anti-impaction net of aero plane engine |
| CN102345512A (en) * | 2010-09-07 | 2012-02-08 | 李艳君 | Protective cover |
| CN102678333A (en) * | 2012-05-23 | 2012-09-19 | 哈尔滨工程大学 | Imported protective net cover |
| CN103569369A (en) * | 2012-07-27 | 2014-02-12 | 刘彦癸 | Anti-bird safety hood for aircraft engine |
| CN104724294A (en) * | 2013-12-18 | 2015-06-24 | 朱津材 | Manufacturing method of shield capable of preventing foreign matters from entering aviation jet engine |
-
2006
- 2006-04-12 CN CN 200620083002 patent/CN2903421Y/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2011091591A1 (en) * | 2010-01-29 | 2011-08-04 | Zhang Haihu | Anti-impaction net of aero plane engine |
| CN102345512A (en) * | 2010-09-07 | 2012-02-08 | 李艳君 | Protective cover |
| CN102345512B (en) * | 2010-09-07 | 2015-03-18 | 李艳君 | Protective cover |
| CN102678333A (en) * | 2012-05-23 | 2012-09-19 | 哈尔滨工程大学 | Imported protective net cover |
| CN103569369A (en) * | 2012-07-27 | 2014-02-12 | 刘彦癸 | Anti-bird safety hood for aircraft engine |
| CN104724294A (en) * | 2013-12-18 | 2015-06-24 | 朱津材 | Manufacturing method of shield capable of preventing foreign matters from entering aviation jet engine |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |