4 bladed Hellcat props

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The XF6F-4 was outfitted with 4-bladed prop.
As to why there was no 4-bladed prop on earlier models - probably there was no need for the power installed. The prop was of big diameter, 13 ft 1 in.
 
XF6F-6_Hellcat_NAN9-88.jpg

XF6F-6, two built using the same engine as the F4U-4. Production canceled with the end of the war.
Perhaps they thought the F6F and F4U didn't need 4 blades for the power they had at the altitudes they were flying?

Tomo beat me to it :)

P-47 with it's turbo made several hundred more HP at higher altitudes (thinner air) and may well have needed extra "bite".
 
Thank you gents. I guess the performance gain wasnt enough to justify it. Although the Corsairs and Thunderbolts put the 4 bladed props to good use.
 
Thank you gents. I guess the performance gain wasnt enough to justify it. Although the Corsairs and Thunderbolts put the 4 bladed props to good use.
Thunderbolts had a more stumpy undercarriage so maybe four blades was the way to go. Is there anywhere to find easily the distance between the prop centre line and the ground at take off.
 
Prop clearance, level stance:
- F6F: 7.31 in
- F4U: 9.1 in
- P-47 (with 13 ft prop): 4.15 in; roughly all the pre-1944 P-47s were with 12 ft 2 in prop

per 'America's hundred tousand'
Great info tomo, however I was thinking that there would be different minimum prop clearance for naval planes to prevent a prop strike after bouncing back after arrest.
 
The XF6F-4 was outfitted with 4-bladed prop.
As to why there was no 4-bladed prop on earlier models - probably there was no need for the power installed. The prop was of big diameter, 13 ft 1 in.

The F4U-1 did without a 4 bladed prop, and it had the same, essentially, engine as the Hellcat.
 
It's not the weight of the prop. it's the weight of the airframe between the Hellcat and the Bearcat.
An F6F weighs about 9200lbs empty, AN F8F-2 weighs about 7650lbs empty. The F6F has a 334 sq ft wing, one of the largest (in not the largest on any single engine fighter in large scale use) compared to the F8Fs 244sq ft.
The Fuselage is sort of in proportion being almost 6 feet longer on the F6F.
Bigger fuel tank/s and so on.
Loaded it just gets worse.

You can put drag slicks on a 1968 427 Impala
52aaf715a9f3e2e0c0c6bda1cc69963d.jpg

Doesn't mean you are going to come close to a 68 427 Corvette.
 
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Interesting. In the Mustang family, the Na-73, Xp-51, A-36 and the P-51a all had 3 bladed props. Looks like right around the P-51b they went with a 4 bladed prop. Don't have my books available right now, but wonder if the Packard Merlin had anything to do with this. I'm sure someone here knows the answer.
 
Interesting. In the Mustang family, the Na-73, Xp-51, A-36 and the P-51a all had 3 bladed props. Looks like right around the P-51b they went with a 4 bladed prop. Don't have my books available right now, but wonder if the Packard Merlin had anything to do with this. I'm sure someone here knows the answer.
Don't have references, but the greatly improved high altitude power of the Merlin is probably the reason.
 
With due respect to all, the B-36 only ever swung a 3 bladed prop, but 2 different versions, the square tip one, IIRC , being the high altitude prop while just about everything else with an R-4360 had a 4 blade propeller. Just thinking...
 
B-36 used a 19ft prop,
A B-50D used a 16'8" prop
The Super Corsair used a 13'6' prop.

B-36 prop had about 283 sq ft of disc area.
B-50 prop had about 217 sq ft of disc area.
F2G prop had about 143 sa ft of disc area.

I have no idea what the prop blade areas were
 

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