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Questions tagged [engine-design]

Questions about the process and principles used when designing aircraft engines. Use "jet-engine" and "piston-engine" tags to specify a certain type of engine.

3 votes
1 answer
279 views

In the T700-GE-401C/D turboshaft used in Blackhawks and MH60s, the output shaft is coming off the front of the engine (inlet) and it connects to the input module. But the AGB (auxiliary gear box) is ...
YamchaAviator's user avatar
0 votes
1 answer
128 views

In the t700-GE-401c/d I get that the engine-driven Alternator is put in place to power the igniters, EDECU, and Ng readings. But how is the alternator providing electrical power for the igniters on ...
YamchaAviator's user avatar
1 vote
1 answer
115 views

In the T700-GE-401C/D used in Blackhawks and MH60s, where exactly is Ng sensor in this cross section picture? (I would also appreciate any better cross-section or description.)
YamchaAviator's user avatar
-1 votes
2 answers
110 views

Questions about the front drive turboshaft engine T700-GE-401C/D Where exactly are the thermocouples, Ng and Np sensors in the cross section picture below? if you have a better cross section or ...
YamchaAviator's user avatar
5 votes
2 answers
2k views

Like the Stratos 714 inside fuselage engine design, are there any other civilian airplanes examples alike?
gbe's user avatar
  • 8,513
7 votes
1 answer
1k views

Are there any differences in the number of components of a small jet engine like in the Cirrus Vision Jet (Williams International FJ33 engine) VS a big jet engine like in a Airbus 320(CFM56)? Is one ...
gbe's user avatar
  • 8,513
2 votes
1 answer
325 views

I have seen that ducted fans have stator vanes (guide vanes) behind them. What is the purpose of such vanes? Can't ducted fans be designed to operate without guide vanes to save cost and weight?
Isaac Ennison's user avatar
0 votes
4 answers
242 views

I am regularly seeing two interpretations of what an "engine core" is. The most common use I have noticed across the web is to call it all internal modules except the fan. However, in some ...
Łukasz Zotow's user avatar
5 votes
2 answers
3k views

If you look at a cross-section of an engine, generally you will see the shaft in the compressor section 'flares' out to form a 'drum' type structure, while aft in the turbine section, the blades are ...
TriJB's user avatar
  • 71
1 vote
1 answer
277 views

Recently I was reading (mainly CFM presentations) about flat rated engines and EGT margin. OAT limit (OATL) was mentioned a few times. OATL is not explained, only a formula and info that with engine ...
Konrad's user avatar
  • 2,227
6 votes
1 answer
848 views

I've been trying to get Google results for way too long;I know that most of the air is fed near the beginning as primary air, some is fed into the combustion later as intermediate air and the rest is ...
Jonathan Sang Student's user avatar
8 votes
4 answers
3k views

The fundamental rule for engine efficiency is higher bypass ratio is better since moving more air slower requires less energy for the same momentum. As such, if you could design an engine that ...
Oscar Smith's user avatar
1 vote
3 answers
379 views

I've seen a video on YouTube where someone was testing various fuels in a lawnmower just to see if they'd keep it running. Like most piston engine aircraft this lawnmower is a gasoline engine with a ...
MacGuffin's user avatar
  • 363
6 votes
1 answer
329 views

I fly the A350 and when full climb thrust is selected, I have noticed that the thrust target can vary. The A350 uses % THR as the primary parameter and I have noticed that sometimes with full climb ...
The Double A's user avatar
1 vote
1 answer
462 views

When looking at the GP7000 and Trent XWB, their spool up times are incredibly fast. Compare this to the GE90 on the 777 which takes several seconds longer, why would this be the case? Though yes, the ...
Joe Dahl's user avatar

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