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Image:Europrop.png is being used on this article. I notice the image page specifies that the image is being used under fair use but there is no explanation or rationale as to why its use in Wikipedia articles constitutes fair use. In addition to the boilerplate fair use template, you must also write out on the image description page a specific explanation or rationale for why using this image in each article is consistent with fair use.
Please go to the image description page and edit it to include a fair use rationale. Using one of the templates at Wikipedia:Fair use rationale guideline is an easy way to insure that your image is in compliance with Wikipedia policy, but remember that you must complete the template. Do not simply insert a blank template on an image page.
If there is other other fair use media, consider checking that you have specified the fair use rationale on the other images used on this page. Note that any fair use images uploaded after 4 May, 2006, and lacking such an explanation will be deleted one week after they have been uploaded, as described on criteria for speedy deletion. If you have any questions please ask them at the Media copyright questions page. Thank you. BetacommandBot 06:52, 4 June 2007 (UTC)
This was on a C-130K on December 17 2008, according to
http://www.amtonline.com/article/article.jsp?id=7012&siteSection=1
and ought to be mentioned.
86.181.119.232 ( talk) 11:36, 2 June 2011 (UTC)
It states: "...output can be up to 100 kNm (6840 Ft-Lb) of torque...". One of these numbers is wrong, 100 KNm = 73756 lb*ft and 6840 lb*ft = 9273 Nm.
I do not know which one of these is right so I will not correct the article. — Preceding unsigned comment added by 69.131.44.254 ( talk) 23:12, 11 November 2011 (UTC)
How can one have a turbine with an intermediate compressor but no low pressure compressor? The entire meaning of "intermediate" is that is'the stage between two other stages. If it was because it was pressuring air to a greater extent than a typical low-pressure compressor or less than a hi-pressure compressor, "medium" compressor would be more appropriate. But I don't believe that's why it's called that. I think someone decided to call it "intermediate pressure" because it happens to be on the same spool as the intermediate turbine. If it was a 3-spool turbofan, it would be completely correct to call it the "intermediate compressor", but it's not. The Low-pressure turbine is driving the prop, which doesn't count as a compression stage. So to be accurate, the intermediate turbine is driving the low-pressure compressor, and the hi-pressure turbine is driving the hi-pressure compressor. They don't need to correspont with their partners, the name is actually descriptive of what the the compressor (or turbine) actually IS. Calling it "intermediate" because it's on the same stage as the intermediate turbine is as bad as calling aftercoolers "intercoolers" (but in a different way)
Idumea47b (
talk)
06:04, 17 December 2018 (UTC)
https://www.wikiwand.com/en/Europrop_TP400 In wikiwand the heading "Specification" is coming after the contents of the section.Ahmed Afif Khan 14:49, 10 April 2020 (UTC) — Preceding unsigned comment added by Ahmedafifkhan ( talk • contribs)
< The HPC has six total stages, with four of them as fixed stages (blisks),[37] and the other two as variable stages >
A fixed stage and a blisk are not the same thing. A variable stage can have a blisk. Ref. 37 (Interavia 2003)needs rereading.
86.145.9.127 ( talk) 18:28, 2 June 2022 (UTC)
This is the
talk page for discussing improvements to the
Europrop TP400 article. This is not a forum for general discussion of the article's subject. |
Article policies
|
Find sources: Google ( books · news · scholar · free images · WP refs) · FENS · JSTOR · TWL |
![]() | This article is rated C-class on Wikipedia's
content assessment scale. It is of interest to the following WikiProjects: | |||||||||||||||||||
|
Image:Europrop.png is being used on this article. I notice the image page specifies that the image is being used under fair use but there is no explanation or rationale as to why its use in Wikipedia articles constitutes fair use. In addition to the boilerplate fair use template, you must also write out on the image description page a specific explanation or rationale for why using this image in each article is consistent with fair use.
Please go to the image description page and edit it to include a fair use rationale. Using one of the templates at Wikipedia:Fair use rationale guideline is an easy way to insure that your image is in compliance with Wikipedia policy, but remember that you must complete the template. Do not simply insert a blank template on an image page.
If there is other other fair use media, consider checking that you have specified the fair use rationale on the other images used on this page. Note that any fair use images uploaded after 4 May, 2006, and lacking such an explanation will be deleted one week after they have been uploaded, as described on criteria for speedy deletion. If you have any questions please ask them at the Media copyright questions page. Thank you. BetacommandBot 06:52, 4 June 2007 (UTC)
This was on a C-130K on December 17 2008, according to
http://www.amtonline.com/article/article.jsp?id=7012&siteSection=1
and ought to be mentioned.
86.181.119.232 ( talk) 11:36, 2 June 2011 (UTC)
It states: "...output can be up to 100 kNm (6840 Ft-Lb) of torque...". One of these numbers is wrong, 100 KNm = 73756 lb*ft and 6840 lb*ft = 9273 Nm.
I do not know which one of these is right so I will not correct the article. — Preceding unsigned comment added by 69.131.44.254 ( talk) 23:12, 11 November 2011 (UTC)
How can one have a turbine with an intermediate compressor but no low pressure compressor? The entire meaning of "intermediate" is that is'the stage between two other stages. If it was because it was pressuring air to a greater extent than a typical low-pressure compressor or less than a hi-pressure compressor, "medium" compressor would be more appropriate. But I don't believe that's why it's called that. I think someone decided to call it "intermediate pressure" because it happens to be on the same spool as the intermediate turbine. If it was a 3-spool turbofan, it would be completely correct to call it the "intermediate compressor", but it's not. The Low-pressure turbine is driving the prop, which doesn't count as a compression stage. So to be accurate, the intermediate turbine is driving the low-pressure compressor, and the hi-pressure turbine is driving the hi-pressure compressor. They don't need to correspont with their partners, the name is actually descriptive of what the the compressor (or turbine) actually IS. Calling it "intermediate" because it's on the same stage as the intermediate turbine is as bad as calling aftercoolers "intercoolers" (but in a different way)
Idumea47b (
talk)
06:04, 17 December 2018 (UTC)
https://www.wikiwand.com/en/Europrop_TP400 In wikiwand the heading "Specification" is coming after the contents of the section.Ahmed Afif Khan 14:49, 10 April 2020 (UTC) — Preceding unsigned comment added by Ahmedafifkhan ( talk • contribs)
< The HPC has six total stages, with four of them as fixed stages (blisks),[37] and the other two as variable stages >
A fixed stage and a blisk are not the same thing. A variable stage can have a blisk. Ref. 37 (Interavia 2003)needs rereading.
86.145.9.127 ( talk) 18:28, 2 June 2022 (UTC)