Hi,
The engine that you are talking about was not designed for the JF17----.
If you read my post again---it refers to the " chinese engine that was being readied for the JF17 "---for that engine---it has a bolt on solution already provided.
Now as for for modular design---it is not for only electronics gadgets only---even houses have modules and offices as well---the pre---fabricated ones---then there are toilet modules as well---and modular space provided for engines and transmissions as well.
In the 90's---Ford came out with their famous 4.6 Liter V 8 and a 6.8 Liter V10----they were known as the " modular " engines---. Even space station has modules.
Welcome to the world kid---.
@ MASTERKHAN
brother you are desperatly trying to proof your point.. i agree madular design has open architecture and amendments for for engines,intakes can be made but please rethink can you really belive without changing just with bolt solution you can fit that lager engine ?? is only for engines upgrades like for f 16...
The initial powerplant selected for the single-engined F-16 was the
pratt ant witney 100 FW 200 afterburning engines, a modified version of the F-15's F100-PW-100, rated at 23,830 lbf (106.0 kN) thrust. During testing, the engine was found to be prone to compressor stalls and "rollbacks," wherein the engine's thrust would spontaneously reduce to idle. Until resolved, the Air Force ordered F-16s to be operated within dead stick landing distance of its bases. It was the standard F-16 engine through the Block 25, except for new-build Block 15s with the Operational Capability Upgrade (OCU). The OCU introduced the 23,770 lbf (105.7 kN) F100-PW-220, later installed on Block 32 and 42 aircraft: the main advance being a Digital Electronic Engine Control (DEEC) unit, which improved reliability and reduced stall occurrence. Beginning production in 1988, the "-220" also supplanted the F-15's "-100", for commonality. Many of the "-220" engines on Block 25 and later aircraft were upgraded from 1997 onwards to the "-220E" standard, which enhanced reliability and maintainability; unscheduled engine removals were reduced by 35%.
The F100-PW-220/220E was the result of the USAF's Alternate Fighter Engine (AFE) program (colloquially known as "the Great Engine War"), which also saw the entry of General Electric as an F-16 engine provider. Its F 110 GE turbofan was limited by the original inlet to thrust of 25,735 lbf (114.5 kN), the Modular Common Inlet Duct allowed the F110 to achieve its maximum thrust of 28,984 lbf (128.9 kN). (To distinguish between aircraft equipped with these two engines and inlets, from the Block 30 series on, blocks ending in "0" (e.g., Block 30) are powered by GE, and blocks ending in "2" (e.g., Block 32) are fitted with Pratt & Whitney engines.)
The Increased Performance Engine (IPE) program led to the 29,588 lbf (131.6 kN) F110-GE-129 on the Block 50 and 29,160 lbf (129.4 kN) F100-PW-229 on the Block 52. F-16s began flying with these IPE engines in the early 1990s. Altogether, of the 1,446 F-16C/Ds ordered by the USAF, 556 were fitted with F100-series engines and 890 with F110s.The United Arab Emirates’ Block 60 is powered by the General Electric F110-GE-132 turbofan with a maximum thrust of 32,500 lbf (144.6 kN), the highest thrust engine developed for the F-16
you don,t change the engines completely ok above is all you answers how a modular design and engines are compatible..or made compatible.
again cars and aircrafts are totally different and as you said i read some things on 1980 cares ford mustang,pinto,orion etc they definitely come with v6 later v8 engines but sir fighter plane is totally different complex design and read about mustang specially it had to go under changed suspension , transmission system and shaft to accommodate lager and powerful engine v8 although made other changes were also made to better its performance