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Spanish to English translations [PRO]
Tech/Engineering - Aerospace / Aviation / Space | | Spanish term or phrase: Estator - 90% de las venas con impactos | Hi proz,
Translation about aircraft engine. Venas con impacto is what I'm looking for??
many thanks
J. |
|  Jenette HolyoakKudoZ activityQuestions: 634 (none open) ( 3 without valid answers) ( 4 closed without grading) Answers: 295
| Local time: 05:01
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| | 90% of stator vanes with impacts / impact damage | Explanation:
Hi Jenette,
EuroDicAutom gives “stator” for “estator,” and I have found several references to “stator veins,” although the real word is apparently VANES.
Axial Flow uses rotor blades and stator veins. Each pair of rotor-stators form a stage. Turbine drives the rotors which increases the pressure and the velocity of the air. Then the air is pushed through the static stator vanes which act as diffuser (increase pressure, and decrease velocity). (http://www.navygouge.com/api/basics/engines.html)
BLADE DEPOSITS.- Compressor blades and stator vanes exhibit varying degrees of cleanliness. Variables such as air-inlet configuration, ambient atmospheric conditions, and air contaminants (chemicals, salt, dirt, water, and so forth) all tend to affect the surface condition of the compressor rotor and stator blades.
Impactos are apparently “impacts,” or “impact damage” as in the following texts:
Airfoil Surface Defects.- Surface defects are the result of object damage or adjacent blade interference (tip clang). Impacts in the center section of the airfoil are not common. Tip clang damage is the result of a blade leading edge tip contacting the adjacent blade tip at approximately one-third of the chord length forward of the trailing edge on the low-pressure (convex) side of the blade (http://www.tpub.com/gtss/15.htm)
About half of the fan blades had impact damage to
the leading and trailing edges. Almost all of the impact damage to the airfoils could be matched to contact with the midspan shroud on an adjacent blade. One full length blade had four soft body impacts along the leading edge and a partial airfoil had a soft body impact, which had some streaking extending rearward. (http://www.ntsb.gov/events/twa800/exhibits/Ex_8A.pdf)
Do check out the links... they may help with your translation.
Cindy |
| Selected response from:
xxxtazdog
Spain
Local time: 06:01
| Grading comment Thank you so much for that!!
4 KudoZ points were awarded for this answer |
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| Discussion entries: 0 |
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Automatic update in 00:
|
3 hrs confidence:   peer agreement (net): +1 90% of stator vanes with impacts / impact damage
Explanation:
Hi Jenette,
EuroDicAutom gives “stator” for “estator,” and I have found several references to “stator veins,” although the real word is apparently VANES.
Axial Flow uses rotor blades and stator veins. Each pair of rotor-stators form a stage. Turbine drives the rotors which increases the pressure and the velocity of the air. Then the air is pushed through the static stator vanes which act as diffuser (increase pressure, and decrease velocity). (http://www.navygouge.com/api/basics/engines.html)
BLADE DEPOSITS.- Compressor blades and stator vanes exhibit varying degrees of cleanliness. Variables such as air-inlet configuration, ambient atmospheric conditions, and air contaminants (chemicals, salt, dirt, water, and so forth) all tend to affect the surface condition of the compressor rotor and stator blades.
Impactos are apparently “impacts,” or “impact damage” as in the following texts:
Airfoil Surface Defects.- Surface defects are the result of object damage or adjacent blade interference (tip clang). Impacts in the center section of the airfoil are not common. Tip clang damage is the result of a blade leading edge tip contacting the adjacent blade tip at approximately one-third of the chord length forward of the trailing edge on the low-pressure (convex) side of the blade (http://www.tpub.com/gtss/15.htm)
About half of the fan blades had impact damage to
the leading and trailing edges. Almost all of the impact damage to the airfoils could be matched to contact with the midspan shroud on an adjacent blade. One full length blade had four soft body impacts along the leading edge and a partial airfoil had a soft body impact, which had some streaking extending rearward. (http://www.ntsb.gov/events/twa800/exhibits/Ex_8A.pdf)
Do check out the links... they may help with your translation.
Cindy
as noted
| xxxtazdog
Spain
Local time: 06:01
Native speaker of: English
PRO pts in category: 20
|
| | Grading comment | Thank you so much for that!! |
|
| | Login to enter a peer comment (or grade) |
6 hrs confidence: Stator: 90% windings with impact marks...
Explanation:
Looks like the 'scars' left on the stator windings due to imbalance and/or bearing wear, very common on close-tolerance structures like aircraft engines.
Technical Translator
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