Feb 17 16:44
2 mos ago
19 viewers *
English term

Ramps

English to Russian Tech/Engineering Aerospace / Aviation / Space aircraft
The structure of the FLE2 composite panel is divided into different repair areas:

Area A:
Edge band and edge band attachment areas (Monolithic composite area).

Area B:
Ramps and general honeycomb areas (Sandwich composite area).

Proposed translations

11 mins
Selected

рампы

если не совсем понятно, что это
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4 KudoZ points awarded for this answer.
+2
1 hr

клинья (регулируемых воздухозаборников)

см. поз. 36 на чертеже по ссылке ниже

Компоновочная схема самолета МиГ-29СД
https://joyreactor.cc/post/1103128
36. Гидроцилиндр привода задней панели клина воздухозаборника
Main air intake variable-area ramp hydraulic actuator

Englsh-Russian aviation and space dictionary > ramp actuator
https://translate.academic.ru/ramp actuator/xx/xx/
1 ramp actuator
силовой привод [воздействующий механизм] регулируемого воздухозаборника

2 ramp actuator motor
мотор привода клина воздухозаборника
Peer comment(s):

agree Michael Volia
5 days
agree ImPad
5 days
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20 hrs

*

участки переходного (законцовочного) профиля (переменной толщины сотового наполнителя)

https://www.google.com/url?sa=t&rct=j&q=&esrc=s&source=web&c...
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Reference comments

19 hrs
Reference:

https://etd.lib.metu.edu.tr/upload/12623558/index.pdf
In addition, a typical industrial sandwich panel has ramp regions where
the height of a core is escalated to its full length gradually. Ramp regions are designed
to avoid abrupt thickness changes and stress concentrations.

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Note added at 19 hrs (2024-02-18 12:08:55 GMT)
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https://patents.google.com/patent/US6180206B1/en

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Note added at 19 hrs (2024-02-18 12:13:43 GMT)
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https://reaa.ru/threads/remont-su-29.12282/#lg=post-657695&s...

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Note added at 20 hrs (2024-02-18 13:05:26 GMT)
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https://digitalcollections.sdsu.edu/do/4f5331bc-7f5b-4be2-9d...
To overcome this difficulty the sandwich laminate is tapered down to a solid composite laminate at the end regions where attachments using mechanical fasteners are required. The transition region from the sandwich laminate is
referred to as the rampdown region
Figure 2.7. Rampdown structure with honeycomb core and
composite facesheet for NASA composite crew module
(CCM).
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