![]() |
If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|
Thread Tools | Display Modes |
|
#1
|
|||
|
|||
![]()
Looking over the available illustrations on the net it appears
that the typical radial aircraft engine had a stroke longer than the bore (undersquare). Is that right? It would make sense for high torque at lower RPMs. -- FF |
#2
|
|||
|
|||
![]()
From Wikipedia, the free encyclopedia
Pratt & Whitney R-2800The Pratt & Whitney R-2800 Double Wasp was an aircraft engine, and part of the long-lived Wasp family. It was a two- row, 18-cylinder, air-cooled radial design. Displacement was 2,804 cubic inches (46 liters); bore and stroke were 5.75" and 6". Specifications Pratt & Whitney (R-4360-51) Wasp Major General characteristics Type: 28-cylinder supercharged air-cooled four-row radial engine Bo 5.75 in. (146 mm) Stroke: 6.00 in. (152 mm) Displacement: 4,360 in³ (71.4 L) Length: 96.5 in. (2 451 mm) Diameter: 55 in (1397 mm) Dry weight: 3,870 lb (1,755 kg) Specifications Wright R3350 18 cylinder, air-cooled, two-row radial displacement: 3,342 cubic inches (54.8 liters) bore x stroke: 6.125 x 6.3125 inches I grabbed these specs from a quick Google search. At least in terms of the larger later-model radials, the stroke is a little greater than the bore. But as a percentage, its not a huge difference like in some car engines where the bore exceeds the stroke by 25% or more. I don't know if radials qualify as "strokers" by those numbers. Harry "we'll think about and engine next year" Frey On Apr 19, 9:30 am, wrote: Looking over the available illustrations on the net it appears that the typical radial aircraft engine had a stroke longer than the bore (undersquare). Is that right? It would make sense for high torque at lower RPMs. -- FF |
#3
|
|||
|
|||
![]()
Earlier, wrote:
Looking over the available illustrations on the net it appears that the typical radial aircraft engine had a stroke longer than the bore (undersquare). Is that right? ... I think that most radials have bore to stroke ratios in line with similar engines of other configuration. However, they often have fairly long connecting rods (which is independent of stroke), which tends to visually exaggerate the stroke. Thanks, Bob K. |
#4
|
|||
|
|||
![]()
On Apr 19, 12:37 pm, Bob Kuykendall wrote:
Earlier, wrote: Looking over the available illustrations on the net it appears that the typical radial aircraft engine had a stroke longer than the bore (undersquare). Is that right? ... I think that most radials have bore to stroke ratios in line with similar engines of other configuration. However, they often have fairly long connecting rods (which is independent of stroke), which tends to visually exaggerate the stroke. Thanks, Bob K. I'll have to check a few of my Dad's radial engine A&P books from the 50's & 60's. Lots of interesting specs and procedures for tearing down and rebuilding. Its interesting to see how only the master rod is connected to the crankshaft, and all of the other rods connect to the master rod. Very interesting lower end geometry, and I'm sure the resulting harmonics are even more entertaining when plotted. Its a lot like music when you think about it! Harry |
#5
|
|||
|
|||
![]() "wright1902glider" wrote Its interesting to see how only the master rod is connected to the crankshaft, and all of the other rods connect to the master rod. Very interesting lower end geometry, and I'm sure the resulting harmonics are even more entertaining when plotted. Its a lot like music when you think about it! Yep, the first time I saw how the rods of a radial were configured, I was floored! Part of the reason for to long rods and long stroke, are _because_ of how the rods connect to the master rod. If the rods were too short, the angles at the quarter strokes would be too great for good efficiency. -- Jim in NC |
#6
|
|||
|
|||
![]()
On Apr 19, 6:37 pm, Bob Kuykendall wrote:
Earlier, wrote: Looking over the available illustrations on the net it appears that the typical radial aircraft engine had a stroke longer than the bore (undersquare). Is that right? ... I think that most radials have bore to stroke ratios in line with similar engines of other configuration. However, they often have fairly long connecting rods (which is independent of stroke), which tends to visually exaggerate the stroke. I think you are right, however: I found a long list of WWII era radials and scanned through it. In general (with a couple of exceptions) the German radials were all close to square (bore = stroke) the British and Japanese were undersquare and the Americans were all over the place. -- FF |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
Light weight low cost four stroke engines, good Rotax replacements. | Jim Carriere | Naval Aviation | 0 | July 8th 05 02:31 AM |
Light weight low cost four stroke engines, good Rotax replacements. | [email protected] | Home Built | 15 | July 3rd 05 05:31 PM |
Recoil starters on small 2-stroke engines | [email protected] | Home Built | 17 | February 26th 05 01:35 PM |
High-Strength Aluminum Helps 2-Stroke Engines | sanman | Home Built | 4 | April 29th 04 12:32 AM |
High-Strength Aluminum Helps 2-Stroke Engines | sanman | Rotorcraft | 4 | April 29th 04 12:32 AM |