AvisQueMetallum
Recruit
- 3
- Jul 4, 2018
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Good point, Greg.In the case of the N1K1 the floatplane had a mid-wing and the landplane's landing gear had to get shorter as it retracted. The mechanism proved unreliable.
In the case of the Ki-84, there was nothing inherently wrong with the landing gear. Late-war attack made it hard to get the landing gear delivered, and late war manufacturing sometimes produced poor heat treatment of steel, resulting in landing gear failures. If the gear made it to the plane and if it was heat treated correctly, there were no landing gear issues. The two issues above are not a design issue; they are related to constant air attack..
You can ask any Ploiesti survivors if the Romanian IAR-80s and -81s were bad fighters - nobody who made it would say that was true!
Just for the record, the Romanians fielded the IAR 80B in defense of Ploesti, along with Bf109s and Bf110s. The Bulgarians mauled the departing bombers with their Bf109s and B-534s.You can ask any Ploiesti survivors if the Romanian IAR-80s and -81s were bad fighters
Your English is WAY better than my Japanese! I do not have the reports, and would love to read them, too.
Up to now, all I have seen are references to landing gear heat treatment issues in several books, all by western authors, with no endnotes or other references to Japanese reports or documents.
Besides the Ki-84 low oil pressure in engine problem, which wasn't satisfactorily solved even by war's end, the issues with the landing gear are described by many authors in English language texts. Just Google: Ki-84 landing gear and select Books from menu and see about 8 hits which describe that problem.
The attached pic is a text capture from the Leszek A. Wieliczko book "Ki-84 Hayate" published by Kagero, 2005, which describes the landing gear problems.
To summarise, the Hayate's landing gear problems were caused by:
1. manufacturing problems relating to strength of landing gear legs
2. pilot inexperience as shock absorbers unable to cope with heavy landings
3. over-inflation of tyres
I haven't checked any Japanese language texts such as FAOW to see if they are in agreement.
Darryl
That was an excerp from a translated document.As a career aircraft mechanic I kind of cringe at that attached description as it sounds like someone with a very limited mechanical, let alone aircraft, background. "The low quality of thermal processing" is strange-speak for poor heat treatment. And "too weak shock absorbers" doesn't mean anything specific as he's talking about oleo struts. Is the stroke too short or the oil too thin/metering orifice too large? Does the plane bounce too much or the gear bottom out too easily? Does he even know? The "even a slight excess of pressure in the tires" line is particularly odd, I can't even imagine how that would work. Maybe if he actually means the strut, then, yeah, that might make sense as a bit too much pressure might blow seals when bottomed out. The Frank at Freeman Field, Indiana (T-2 302) was one of the most reliable aircraft there, once the exhaust stacks had been repaired, and in the T-2 report on it no mention was made of any unusual or difficult characteristics of the type as far as landing and takeoff regimes were concerned. It actually says it was quite good in those areas but notes that both three-point visibility and the brakes are poor so the pilot can't be lazy. Offhand then I'd guess that the problems the Japanese experienced could be largely be chocked up to the steel and its heat treatment (an industry-wide problem) and poor pilot training (and, maybe, the airfields used?).
That was an excerp from a translated document.
The "slight excess of tire pressure" means the tires were over-inflated, which can have adverse effects on landing gear (and quality of landing) as it makes the tires too firm.