| Author | Comment | ||
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solobaric |
8 Blades? |
Lead | |
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I have some pictures my uncle sent me from Ohio. It appears to be an E with 8 bladed props. If anyone wants the pics let me know. You might be able to better tell me what the hell is going on in the pics. There is also an A beside it and a DC-3 behind it.
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Natops1 |
Re: 8 Blades? | ||
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Check out Snow Aviation........
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hurk130 |
NP2000. I thought it was dead! | ||
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AFMC rejected it because it drove the VMCA through the roof on takeoff. So you would have to put a fillet along the rudder like the C-123K. Well that also changed how the air flowed over the tail with the NP2000 so you had to change the elevators abit. In the end, it did not give that much performance on the top end and made assult takeoffs more dangerous. We did not recommend it. We gave it to the Navy who put it on a C-2 Greyhound and found the same things out about it. I think that might be the companies test bed. If you could send me a pic at hurk130@hotmail.com when you get the chance and I can tell you more.
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Jbob |
Re: NP2000. I thought it was dead! | ||
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I had thought it was the Navy who was orginally testing this new prop out and the AF was waiting for results. I wondered what the results were.
If AFMC is using the Vmca as an excuse well that just shows what kind of thoughtless engineers we have at the SPO as well as OPs in general. It is that kind of pointless decisions that lead to less than capable airframes. The mentality that thinks everything in terms of Max power. That is/was the issue with that latest 1-1 fiasco. What the 130 needed is Vmca charts for less than max power. Vmca problem solved. The B-29 had a bad Vmca problem on three engines. Funny how that issue went away with the B-50 and more powerful engines. |
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hurk130 |
Hey Jbob, I really respect what you have to say.... | ||
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but I am a bit confused. There is only so much money out there. We knew the wing issues were coming up fast. AMP, anti-missile stuff, short term repairs, upgrades and updates. The Afghan war was in full swing and the winds of war were blowing in Iraq.
We thought the money could be spent better in other areas. Our initial test gave us data that said the plane would not be that much faster or fly higher but would cause problems with paratroopers because of the airflow patterns over the fuselage, Vmca and other directional problems, logistics, I think there was even a problem with it not fitting in the back of the plane. I could be wrong on that one. There were a lot of other things in the decision to not pursue it. Oh, and it was just a recommendation to the SPO and there were a few DET's that came to the same conclusion on their own. Like I said, I really respect your opinion and do not understand a few of your comments. "Pointless". I know the B-50 had some real power behind it with the new engines and turbos. I am not so sure it pulled the same kind of torque the -15's with Ham-Stan props. I would like to hear anything you have to say on the subject. I got to tell you that I wanted to do that prop so bad. It would have kept me employed for years and gave me a job after retirement not to mention it made the Herk look bad ass and modern (as a herk can look). But it just wasn't right for the troops. I do agree with you and the -1-1. I hate that thing. Two line Staff Sgts at the Rock could have done a better job on it. My opinion only. |
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Jbob |
Re: Hey Jbob, I really respect what you have to say.... | ||
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Ok, my main concern was for the Vmca excuse. I really do understand the other stuff. If it was a plethora of things then that makes more sense. Funny but aren't some of those other issues also applicable in the "J"? No "J" bashing here! My understanding of the 8 bladed prop too was on the -15 motor produced almost as much thrust at the "J" motor. Perhaps that was incorrect info then. Did the Navy test it on a Herk on just an E-2? Which engine? Series 4 on the E-2's!
My thoughts on the Vmca thing though is as I mentioned using the B-50 as an example. The reason the Vmca was not such an issue on it as opposed to the B-29 is because of the increased 3 engine power available they could reduce power on the assymetric engine thus reducing Vmca affect. Same for the Herk. More power does not necessarily have to translate to increased Vmca speeds. I tried explaining this during an AMC/1-1 conference before I retired. Unfortunately the powers to be either did not comprehend or were unwilling to flinch. The main issue is that Vmca is based on Max power on remaining engines. Here is an example scenario: Cold day Vmca is higher than warm day Vmca due to increased engine output thrust. In scenario 1, max torque is 19,000 and in scenario 2 max torque is 15,000. Depending on circumstances most missions would take off using a reduced power setting anyway and only advance throttles as needed. So if the herk in scenario 2 can make a safe takeoff with a lower max power available then why can't the herk in scenario 1 just use the lower torque settings to base it's Vmca speeds on? In that case Vmca would not have as much affect as lower power settings are being utilized. Even in an emergency three engine scenario the "H" -1 calls for applying power on remaining engines "as required", or it did anyway! The main idea is that if the plane in scenario 2 could make a safe takeoff in a 3 engine emergency with the lower max power available the the same holds true for the plane in scenario 1. The only difference is that Vmca was affecting scenario 1 more so than 2. This is why reduced power Vmca charts are needed. This would not be applicable in all situations like heavy weight/short field where maximum ACL is needed however in normal operations this would practically illiminate those Vmca/Vmcg enduced limitations. The other thought is to go to "Uh Oh" split throttle takeoffs. lol I think the AWACS already utilizes this procedure due to limited rudder effectiveness caused by the rotodome on top. I do understand the money thing. Believe me. I also remember the talk of re-engining the herk in the late 80's. Not sure if they were looking at series 3 or series 4 motors though. That talk was that the engine upgrades would pay for themselves in fuel saving alone in 5 years. Not a bad deal especially since from what I understand the cost to overhaul a -7 motor now is more that a -15 since the -7 components are not manufactured anymore. But this whole wing crack thing has really shaken up the Herk world. Edit: Well the way some of your post read I had assumed you were at the SPO but according to your profile you are a FE at Dyess. I had assumed that you were speaking like you had some inside track on what went on with the testing of the 8 bladed prop. Well I'm retired now and really don't keep up as much as I used to anymore. But I did retire from Robins and used to work with the SPO quite a bit. I did see some of the stuff that goes on there. |
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US Herk |
Re: Hey Jbob, I really respect what you have to say.... | ||
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Give me high Vmcas ANY DAY! Make 'em 50 knots higher! That means I've got more power - why is this one hard to figure out?
The risk elimination squad has decided that higher Vmcas are bad because they don't understand power available vs power required. Reduced power takeoff charts would be one mitigation factor with greatly increased power/Vmca. Proper training would be the other. In some AFs, Max-Effort takeoffs are conducted at what we would consider extremely low airspeeds (less than 86kts) - lose an engine immediately after rotate & you better understand Vmca & the requirement to pull your good asyemmetric engine immediately or you are a smoking hole. The technique there was to pull both outboards back about half-way - no thinking or analyzing required. As control is attained, feed power back in as able...simple. The same could be done if our Vmca was 150kts & rotate speeds stayed the same. Alternatively, reduced power takeoffs would be the order of the day, engine life would be increased, & the world would be happier. |
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herc2 |
Re: Hey Jbob, I really respect what you have to say.... | ||
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The J automatically pulls power from the outboard engine on the opposite side if an outboard engine fails during take off. You can only do that with a FADEC controlled engine. Also, the J has a HUD, which provides an immediate indication that the airplane is yawing during the roll. You can't count on an "eyes in" display to do that, for obvious reasons. Both features were used to keep the Vmcg reasonable. The J is better than the sum of its parts.
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RZ Hill |
Re: Hey Jbob, I really respect what you have to say.... | ||
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Now who is slamming who?
Having a fadec and a hud doesn't guarantee a successful recovery. Having a properly trained pilot is a much better solution to the problem. As proven many tims in actual experiences a profecient pilot will pull the opposite throttle back as he has been trained, it's second nature!! Having a Fe insures that the tie will be broken and is another redundant system that can and does think, and who can operate the throttles as needed while the pilots fly the airplane. I have been in this situation numerous times and everything operates as advertised. Now who is slamming who? RZ Hill |
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solobaric |
re | ||
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damn guys i wasn't asking for you to bash the J. I was just seeing what info you had on the 8 bladed herk. Because i got pictures in my email of it. I'll see if i can get more pictures.
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RZ Hill |
Re: re | ||
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WHO'S BANGIN THE j? NOT ME
RZHILL |
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hurk130 |
I just wrote a long letter explaining all and.... | ||
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hit Add Reply only to get an error message. When I went back, the comment section was empty and the letter gone. I got to go to work and can't waste that much time again. I will try to retype it tonight. Kel
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SEFEGeorge |
Re: Hey Jbob, I really respect what you have to say.... | ||
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The J automatically pulls power.... How available is that engine to the crew? Can the pilot just push the throttle, etc., and get the throttle/engine back? I don't know about any of the other "old heads" but having an engine "taken away" just when I might need it is a little un-nerving. Sort of reminds me of the auto-feather switch on the Convairs (T-29 and C-131). I always got that thing turned off as soon as I could.
Most of the pilots I flew with taught and used the staggered throttle technique with an outboard out. / \ Always seemed to work pretty good. An on-the-ball FE could help by closing the eng bleed valve on the engine-out wing. |
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US Herk |
Re: Hey Jbob, I really respect what you have to say.... | ||
Quote: I don't consider myself an old head, but I certainly don't like it! The F16A had an auto-recover capability - if it felt the pilot was going to stall the plane, it rolled to the nearest horizon & accelerated away. First thing changed in their block cycle updates! F15 guys would just take 'em vertical until the computer got "worried" & roll in & kill 'em... The fear of high Vmca is ungrounded. I'd rather have more power any day - it means when I do lose that engine(s), I've got a better chance of continuing to fly instead of finding a crash site! |
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Dan Wilson |
Re: Hey Jbob, I really respect what you have to say.... | ||
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"the J has a HUD, which provides an immediate indication that the airplane is yawing during the roll."
This is not against the J, but this is a silly statement! How about the Pilots butt? If he cannot feel an adverse yaw that would threaten safety of flight then he must not have an inner ear! An also if it happens in the daytime you can see it out the windows and at night or in the weather you arent looking out anyways (nothing to see) and are looking at instruments be it HUD or slip and turn. On a different tack here but question for the J crowd, with the airflow changes caused by the new props does it still have the danger or capability of fin stall? I know during flight testing they had a real problem getting the plane to stall its wing because of airflow changes (this is good) but wonder if it affects the tail as well???? Dan |
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SEFEGeorge |
Re: Hey Jbob, I really respect what you have to say.... | ||
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Guess my "old-heads" was more directed at us older guys that flew the recips, like the T-29 and C-131 (with the auto feather), and the C-121, C-118, etc., where the FE actually handled the throttles. But I can see you understand what I was getting at.
Not sure who's all familiar with the auto-feather system, but on take-off if an engine lost power (can't remember now how much torgue loss/BMEP loss, seems like it was 15lbs of tourque, but....) the system would have that prop standing at attention faster than you could say "oh s..." So now you're on heavy and on 1 engine when you might have been able to coax some power out of the bad one, if the AF sys hadn't caged it for you. |
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DC10FE |
Re: Hey Jbob, I really respect what you have to say.... | ||
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George,
As I remember, if the TOP (torque oil pressure) dropped below 40 psi (I think) for a short period of time, 3 or 4 seconds (again, I think), that prop would automatically feather. Of course, the throttles had to be advanced above a certain position to arm the system. Funny how this thread has gone from a question about a photo of an old C-130 with 8-bladed props to the feathering system on a C-131/T-29. Don R. |
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Colin C Tigwell |
Re: Hey Jbob, I really respect what you have to say.... | ||
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I suspect the problem of too many blades, may be the reason why the Britts developed the contra rotation props for their higher HP engines.
I also note that the A400M, has the props turning in opposite directions, from side to side. Regards Col Tigwell |
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Index DataXFer BLANK |
J | ||
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The HUD , and aural alert "ENGINE ONE, FAIL" are designed to, and DO reduce the reaction time to an EFATO. It has been proven.
The Auto-Thrust Control System (ATCS) automatically reduces power to prevent a dynamic Vmca problem. IT automatically schedules the outboard power back up to 100% as speed increases [keeping you from rolling on your back.].. you can override it if you wish by clicking the button on the side of the outboard throttles. I certainly wouldn't be trying it unless I was going to hit something without the power, and had some other plan for preventing her from rolling over. RZ: No offence RZ but the last thing I'm going to do with an EFATO at Vmca is take my hand off the throttles and let someone play with them. airflow & para - no problem . This has been PROVEN. |
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hurk130 |
What I know | ||
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Jbob Quote:"Well the way some of your post read I had assumed you were at the SPO but according to your profile you are a FE at Dyess. I had assumed that you were speaking like you had some inside track on what went on with the testing of the 8 bladed prop."
Short history here: I was a Helo mechanic at Kirtland 88-91 then went to Rhein-Main on E's Talon-1's C-5's, C-141's and C-9's. While I was there CMSgt Mike Jolly talked me into becoming a FE. Got sent to Dyess 94 to 2000. Jim Woods was my Instructor. Jim, I am chief instructor at the 39th now so I guess you did do something right. I am still worried why you retired right after qualifying me. I hope I didn't have something to do with that! Then worked with Big Safari at Plant 42 Lockheed Skunkworks. Defined: The 645 Materiels Squadron Det 4 has been operating under the umbrella of Big Safari for 30+ years of acquisition and development of special systems aircraft. Big Safari operates through the Reconnaissance Systems Program Office, Wright Patterson AFB, Ohio. Specifically, Det 4 supports special mission systems C-130 applications, such as Compass Call (Rivet Fire), Commando Solo (Rivet Rider) and Senior Scout. Det 4 supports development, acquisition, modification, sustainment to multiple systems from cradle to grave. Detachment 4, 645 MATS, is currently located at L-3 Communications in Waco, TX as an AFMC C-130 Flight Test organization. They were formerly located at the Lockheed Martin Skunkworks in Palmdale, CA. I took over for Craig Walsingham and worked with George Neds for the next two years. Then his replacement was one of the most gifted FE's I have ever met and is a mentor to me to this day. Steve Hennessy. Brilliant guy. He is right up there with Steve Judd out at Marietta. Steve Hennessy did most of the number crunching on the NP2000 and ran some of the numbers by me. We both came to the conclusion that it just wasn't worth the money, energy, effort and logistics involved. Vmca numbers could not account for pilot technique. The plane has to be built for many levels of pilots to fly. There was some great jets out there but it took the best pilots to fly. F-104 comes to mind first. The Herc has always been a forgiving plane. Not with these new props in my opinion. I might be wrong on this but I think the prop would not even fit in the back of a herc. Afghan war was winding down and Iraq was looming. It wasn't a good use of our resources. Yes we even looked into retro-modding the herc with a type of FADEC system or ATCS type system. Some other mods would have to be made too. And AMP was a hot item on the list of things needed along with Pre-armored paratroop doors with wide windows and seats built in. Believe me, I wanted it. It made the Herc look much newer than it was. (If you can do that) But it just wasn't what the Herc needed right then. Times change. When I was read out of the Det in 2004, I lost all my contacts. I don't know what is going on at the SPO or special projects. I went back to Dyess because it is near time to retire and I am from Houston. This new A model with the NP2000 was news to me. They just might be a private company trying to sell something no one wants to deal with. If I remember right Snow was trying to sell a cheap version of the AMP that would have worked out very nicely if the AF bought it. I could be wrong.
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WestC |
Re: What I know | ||
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JBob
The B-50 problem was somewhat corrected with a taller Vertical Stabilizer than the B-29 Vertical Stabilizer. It supposedly corrected for the assemetrical Engine power on the 4360's of the B-50 over the 3350's on the B-29's. Chuck |
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