CFM56 (Chinese Wikipedia)

Analysis of information sources in references of the Wikipedia article "CFM56" in Chinese language version.

refsWebsite

Global rank Chinese rank

49web.archive.org

1^st place

17cfm56.com

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8flightglobal.com

223^rd place

398^th place

7ntsb.gov

1,153^rd place

2,151^st place

3aviationweek.com

1,181^st place

1,520^th place

2archives.gov

446^th place

1,043^rd place

1enginehistory.org

low place

1nasa.gov

75^th place

140^th place

1cfmaeroengines.com

low place

1news.google.com

59^th place

494^th place

1boeing.com

1,290^th place

821^st place

1sae.org

4,774^th place

5,919^th place

1ge.com

low place

9,106^th place

1webcitation.org

24^th place

29^th place

1safran-na.com

low place

1geae.com

low place

1cnki.net

3,420^th place

133^rd place

1uspto.gov

1,459^th place

1,685^th place

1pat2pdf.org

low place

1b737.org.uk

low place

1doi.org

2^nd place

23^rd place

1springerlink.com

2,569^th place

1,358^th place

1aaib.gov.uk

low place

1wired.com

193^rd place

421^st place

aaib.gov.uk

Report on the accident to Boeing 737-400, G-OBME, near Kegworth, Leicestershire on 8 January 1989. Report No: 4/1990. Air Investigations Branch. 1990-08-25 [2012-01-28]. （原始内容存档于2012-06-01）（英语）.

archives.gov

nixon.archives.gov

Henry A. Kissinger, GE-SNECMA Jet Engine Joint Venture (pdf), National Security Decision Memorandum 189 (The White House), 1972-09-19 [2012-01-27], （原始内容存档 (PDF)于2013-11-16）（英语）
Henry A. Kissinger, GE-SNECMA, CFM-56 Jet Engine Joint Development (pdf), National Security Decision Memorandum 220 (The White House), 1973-06-04 [2012-01-27], （原始内容存档 (PDF)于2013-11-16）（英语）

aviationweek.com

Swissair, AEA 'Agree To Pursue A Voluntary Program' On Passenger Rights | Aviation Week Network. aviationweek.com. [2022-12-27]. （原始内容存档于2022-12-27）.
Morris, John. "Son of CFM56" -- TECH56. Aviation Week's Show News Online. 2000-07-24 [2012-01-27]. （原始内容存档于2001-07-03）（英语）.
Norris, Guy. Airbus Weighs Modified CFM56-5 Upgrade Options. Aviation Week. 2010-05-12 [2012-01-27]. （原始内容存档于2020-03-05）（英语）.

b737.org.uk

Brady, Chris. The Boeing 737 Technical Guide. 2012-01-21 [2012-01-28]. （原始内容存档于2011-02-21）（英语）.

boeing.com

active.boeing.com

Boeing 737 Deliveries. The Boeing Company. [2012-01-27]. （原始内容存档于2018-11-21）（英语）.

cfm56.com

CFM delivers 20,000th engine. CFM International Website. CFM International. 2009-11-18 [2012-01-21]. （原始内容存档于2011-07-22）（英语）.
The CFM Timeline: Milestones in Aviation. CFM International Website. [2012-01-27]. （原始内容存档于2010-03-23）（英语）.
The CFM Work Split and Division of Labor. CFM International Website. [2012-01-27]. （原始内容存档于2010-05-19）（英语）.
CFM Certifies Tech Insertion Compressor Upgrade; Brings Lower Fuel Burn, Longer On-Wing Life to Mature Fleet. CFM International Website. 2008-07-14 [2012-01-27]. （原始内容存档于2012-03-12）（英语）.
CFM56-5B Technology. CFM International Website. [2012-01-28]. （原始内容存档于2010-03-07）（英语）.
CFM56-2 Technology. CFM International Website. [2012-01-28]. （原始内容存档于2010-05-30）（英语）.
CFM56-7: An In-Depth Look At The New Industry Leader. CFM International Website. 1996-06-12 [2012-01-27]. （原始内容存档于2010-04-12）（英语）.
CFM'S Advanced Double Annular Combustor Technology. CFM International Press Release. 1998-07-09 [2012-01-27]. （原始内容存档于2012-02-27）（英语）.
CFM56-5B/-7B Tech Insertion Package On Schedule For 2007 EIS. CFM International Website. 2006-06-13 [2012-01-27]. （原始内容存档于2012-03-12）（英语）.
CFM56-3 Technology. CFM International Website. [2012-01-27]. （原始内容存档于2008-09-20）（英语）.
"CFM56-5A History. CFM International Website. [2012-01-28]. （原始内容存档于2010-05-30）（英语）.
CFM56-5A Technology. CFM International Website. [2012-01-28]. （原始内容存档于2010-05-30）（英语）.
CFM56-5B History. CFM International Website. [2012-01-28]. （原始内容存档于2010-05-30）（英语）.
CFM56-5C Technology. CFM International Website. [2012-01-28]. （原始内容存档于2010-05-30）（英语）.
"CFM56-7B Technology. CFM International Website. [2012-01-28]. （原始内容存档于2012-02-29）（英语）.
CFM56-7B History. CFM International Website. [2012-01-28]. （原始内容存档于2012-02-29）（英语）.
CFM56 Turbofan Engine Reliability. CFM International Website. [2012-01-28]. （原始内容存档于2011-02-02）（英语）.

cfmaeroengines.com

CFM56 Engine Fleet Surpasses One Billion Engine Flight Hours (新闻稿). CFM international. 4 June 2019 [7 June 2019]. （原始内容存档于7 June 2019）.

cnki.net

mall.cnki.net

李杰. TAPS燃烧室燃油喷嘴设计特点分析. 航空发动机. 2010, (5) [2012-01-21]. （原始内容存档于2014-07-14）（中文（中国大陆））.

doi.org

dx.doi.org

Linke-Diesinger, Andreas. Chapter 8: Thrust Reverser Systems. Systems of Commercial Turbofan Engines: An Introduction to Systems Functions. Springer Berlin Heidelberg. 2008 [2012-01-28]. ISBN 978-3-540-73618-9. doi:10.1007/978-3-540-73619-6_8. （原始内容存档于2019-09-24）（英语）.

enginehistory.org

带冠叶片（Shrouded Blade）指叶片中部带有一块特别的突起物（Shroud）的叶片，各叶片的突起间互相衔接，形成一个环，通常用于抑制振动并发挥和翼尖小翼类似的作用。可参见这里（页面存档备份，存于互联网档案馆）的比较。

flightglobal.com

Norris, Guy. CFM56: Engine of Change. Flight International. 1999-05-25 [2012-01-27]. （原始内容存档于2016-03-05）（英语）.
Tooling up for Tiger. FLIGHT International. 1978-01-07: 8 [2012-01-27]. （原始内容存档于2016-12-27）（英语）.
Ostrower, Jon. CFM56-7BE achieves FAA and EASA certification. Air Transport Intelligence news. 2010-08-02 [2012-01-27]. （原始内容存档于2010-08-09）（英语）.
Max Kingsley-Jones. CFM brings elements of Evolution upgrade to A320 powerplant. Flightglobal. 2011-04-20 [2012-01-22]. （原始内容存档于2016-12-22）（英语）.
Velupillai, David. CFM56 Comes of Age. Flight International. 1981-04-18 [2012-01-27]. （原始内容存档于2016-03-05）（英语）.
Norris, Guy. CFMI details insertion plan for Tech 56. Flight International. 2004-08-03 [2012-01-27]. （原始内容存档于2019-09-24）（英语）.
CFM56 rises to challenge. Flight International. 1991-06-11 [2012-01-27]. （原始内容存档于2017-09-13）（英语）.
Derating Clears CFM56-3Cs to Fly. Flight International. 1989-07-01 [2012-01-28]. （原始内容存档于2015-12-22）（英语）.

ge.com

GE为南航提供CFM56-5B/3发动机 (PDF). GE在中国. 2008, 57 (3): 31 [2012-01-23]. （原始内容 (pdf)存档于2012-03-22）（中文（中国大陆））.

geae.com

CFM Launches CFM56-7B Evolution Engine Program to Power Enhanced Boeing Next-Generation 737. GE Aviation Press Release. 2009-04-28 [2012-01-27]. （原始内容存档于2010-12-11）（英语）.

nasa.gov

sti.nasa.gov

Chevron型尾喷管：一种锯齿型尾喷管，用于减小噪音。可参见这里（页面存档备份，存于互联网档案馆）的图片（请注意图中所示不是CFM56发动机）。

news.google.com

GE Gets OK To Build Jet Engine With French Firm. Daytona Beach Morning Journal. 1973-06-23: 4B [2012-01-24] （英语）.

ntsb.gov

NTSB No: DCA-06-MA-009. Section D.1.3 Thrust Reverser Description (pdf). National Transportation Safety Board. 2006-04-10 [2012-01-28]. （原始内容存档 (PDF)于2008-12-30）（英语）.
"Safety Recommendation A-05-19 and 20 (pdf). NTSB Recommendations. National Transportation Safety Board. 2005-08-31 [2012-01-28]. （原始内容存档 (PDF)于2011-06-04）（英语）.
NTSB Aviation Database. National Transportation Safety Board. [2012-01-14]. （原始内容存档于2015-02-08）（英语）.
NTSB Report: ENG09WA015. National Transportation Safety Board. [2012-01-14]. （原始内容存档于2012-09-26）（英语）.
NTSB Report: ENG09WA012. National Transportation Safety Board. [2012-01-14]. （原始内容存档于2012-09-26）（英语）.
NTSB Report: ENG11IA011. National Transportation Safety Board. [2012-01-14]. （原始内容存档于2012-10-17）（英语）.
NTSB Report: ENG11WA017. National Transportation Safety Board. [2012-01-14]. （原始内容存档于2012-10-17）（英语）.

pat2pdf.org

美国专利6360528 (PDF 版本)（于2002年03月26日注册）约翰·布劳施等——用于燃气涡轮发动机的Chevron型尾喷管。

sae.org

"Preparing for the future of aircraft engines - TECH56. Aerospace Engineering Online. [2012-01-27]. （原始内容存档于2012-09-29）（英语）.

safran-na.com

Angrand, A. Tech Insertion: Eternal youth for the CFM56 (PDF). SAFRAN magazine. 2007年11月: 26 [2012-01-27]. （原始内容 (pdf)存档于2010-04-09）（英语）.

springerlink.com

Linke-Diesinger, Andreas. Chapter 8: Thrust Reverser Systems. Systems of Commercial Turbofan Engines: An Introduction to Systems Functions. Springer Berlin Heidelberg. 2008 [2012-01-28]. ISBN 978-3-540-73618-9. doi:10.1007/978-3-540-73619-6_8. （原始内容存档于2019-09-24）（英语）.

uspto.gov

patft.uspto.gov

美国专利6360528 (PDF 版本)（于2002年03月26日注册）约翰·布劳施等——用于燃气涡轮发动机的Chevron型尾喷管。

web.archive.org

带冠叶片（Shrouded Blade）指叶片中部带有一块特别的突起物（Shroud）的叶片，各叶片的突起间互相衔接，形成一个环，通常用于抑制振动并发挥和翼尖小翼类似的作用。可参见这里（页面存档备份，存于互联网档案馆）的比较。
Chevron型尾喷管：一种锯齿型尾喷管，用于减小噪音。可参见这里（页面存档备份，存于互联网档案馆）的图片（请注意图中所示不是CFM56发动机）。
Swissair, AEA 'Agree To Pursue A Voluntary Program' On Passenger Rights | Aviation Week Network. aviationweek.com. [2022-12-27]. （原始内容存档于2022-12-27）.
CFM delivers 20,000th engine. CFM International Website. CFM International. 2009-11-18 [2012-01-21]. （原始内容存档于2011-07-22）（英语）.
CFM56 Engine Fleet Surpasses One Billion Engine Flight Hours (新闻稿). CFM international. 4 June 2019 [7 June 2019]. （原始内容存档于7 June 2019）.
Norris, Guy. CFM56: Engine of Change. Flight International. 1999-05-25 [2012-01-27]. （原始内容存档于2016-03-05）（英语）.
Henry A. Kissinger, GE-SNECMA Jet Engine Joint Venture (pdf), National Security Decision Memorandum 189 (The White House), 1972-09-19 [2012-01-27], （原始内容存档 (PDF)于2013-11-16）（英语）
Tooling up for Tiger. FLIGHT International. 1978-01-07: 8 [2012-01-27]. （原始内容存档于2016-12-27）（英语）.
Henry A. Kissinger, GE-SNECMA, CFM-56 Jet Engine Joint Development (pdf), National Security Decision Memorandum 220 (The White House), 1973-06-04 [2012-01-27], （原始内容存档 (PDF)于2013-11-16）（英语）
The CFM Timeline: Milestones in Aviation. CFM International Website. [2012-01-27]. （原始内容存档于2010-03-23）（英语）.
The CFM Work Split and Division of Labor. CFM International Website. [2012-01-27]. （原始内容存档于2010-05-19）（英语）.
Boeing 737 Deliveries. The Boeing Company. [2012-01-27]. （原始内容存档于2018-11-21）（英语）.
"Preparing for the future of aircraft engines - TECH56. Aerospace Engineering Online. [2012-01-27]. （原始内容存档于2012-09-29）（英语）.
Morris, John. "Son of CFM56" -- TECH56. Aviation Week's Show News Online. 2000-07-24 [2012-01-27]. （原始内容存档于2001-07-03）（英语）.
GE为南航提供CFM56-5B/3发动机 (PDF). GE在中国. 2008, 57 (3): 31 [2012-01-23]. （原始内容 (pdf)存档于2012-03-22）（中文（中国大陆））.
CFM Certifies Tech Insertion Compressor Upgrade; Brings Lower Fuel Burn, Longer On-Wing Life to Mature Fleet. CFM International Website. 2008-07-14 [2012-01-27]. （原始内容存档于2012-03-12）（英语）.
CFM Launches CFM56-7B Evolution Engine Program to Power Enhanced Boeing Next-Generation 737. GE Aviation Press Release. 2009-04-28 [2012-01-27]. （原始内容存档于2010-12-11）（英语）.
Norris, Guy. Airbus Weighs Modified CFM56-5 Upgrade Options. Aviation Week. 2010-05-12 [2012-01-27]. （原始内容存档于2020-03-05）（英语）.
Ostrower, Jon. CFM56-7BE achieves FAA and EASA certification. Air Transport Intelligence news. 2010-08-02 [2012-01-27]. （原始内容存档于2010-08-09）（英语）.
Max Kingsley-Jones. CFM brings elements of Evolution upgrade to A320 powerplant. Flightglobal. 2011-04-20 [2012-01-22]. （原始内容存档于2016-12-22）（英语）.
CFM56-5B Technology. CFM International Website. [2012-01-28]. （原始内容存档于2010-03-07）（英语）.
CFM56-2 Technology. CFM International Website. [2012-01-28]. （原始内容存档于2010-05-30）（英语）.
CFM56-7: An In-Depth Look At The New Industry Leader. CFM International Website. 1996-06-12 [2012-01-27]. （原始内容存档于2010-04-12）（英语）.
Velupillai, David. CFM56 Comes of Age. Flight International. 1981-04-18 [2012-01-27]. （原始内容存档于2016-03-05）（英语）.
Norris, Guy. CFMI details insertion plan for Tech 56. Flight International. 2004-08-03 [2012-01-27]. （原始内容存档于2019-09-24）（英语）.
CFM'S Advanced Double Annular Combustor Technology. CFM International Press Release. 1998-07-09 [2012-01-27]. （原始内容存档于2012-02-27）（英语）.
李杰. TAPS燃烧室燃油喷嘴设计特点分析. 航空发动机. 2010, (5) [2012-01-21]. （原始内容存档于2014-07-14）（中文（中国大陆））.
CFM56-5B/-7B Tech Insertion Package On Schedule For 2007 EIS. CFM International Website. 2006-06-13 [2012-01-27]. （原始内容存档于2012-03-12）（英语）.
CFM56 rises to challenge. Flight International. 1991-06-11 [2012-01-27]. （原始内容存档于2017-09-13）（英语）.
Brady, Chris. The Boeing 737 Technical Guide. 2012-01-21 [2012-01-28]. （原始内容存档于2011-02-21）（英语）.
NTSB No: DCA-06-MA-009. Section D.1.3 Thrust Reverser Description (pdf). National Transportation Safety Board. 2006-04-10 [2012-01-28]. （原始内容存档 (PDF)于2008-12-30）（英语）.
Linke-Diesinger, Andreas. Chapter 8: Thrust Reverser Systems. Systems of Commercial Turbofan Engines: An Introduction to Systems Functions. Springer Berlin Heidelberg. 2008 [2012-01-28]. ISBN 978-3-540-73618-9. doi:10.1007/978-3-540-73619-6_8. （原始内容存档于2019-09-24）（英语）.
CFM56-3 Technology. CFM International Website. [2012-01-27]. （原始内容存档于2008-09-20）（英语）.
"CFM56-5A History. CFM International Website. [2012-01-28]. （原始内容存档于2010-05-30）（英语）.
CFM56-5A Technology. CFM International Website. [2012-01-28]. （原始内容存档于2010-05-30）（英语）.
CFM56-5B History. CFM International Website. [2012-01-28]. （原始内容存档于2010-05-30）（英语）.
CFM56-5C Technology. CFM International Website. [2012-01-28]. （原始内容存档于2010-05-30）（英语）.
"CFM56-7B Technology. CFM International Website. [2012-01-28]. （原始内容存档于2012-02-29）（英语）.
CFM56-7B History. CFM International Website. [2012-01-28]. （原始内容存档于2012-02-29）（英语）.
CFM56 Turbofan Engine Reliability. CFM International Website. [2012-01-28]. （原始内容存档于2011-02-02）（英语）.
"Safety Recommendation A-05-19 and 20 (pdf). NTSB Recommendations. National Transportation Safety Board. 2005-08-31 [2012-01-28]. （原始内容存档 (PDF)于2011-06-04）（英语）.
Report on the accident to Boeing 737-400, G-OBME, near Kegworth, Leicestershire on 8 January 1989. Report No: 4/1990. Air Investigations Branch. 1990-08-25 [2012-01-28]. （原始内容存档于2012-06-01）（英语）.
Derating Clears CFM56-3Cs to Fly. Flight International. 1989-07-01 [2012-01-28]. （原始内容存档于2015-12-22）（英语）.
NTSB Aviation Database. National Transportation Safety Board. [2012-01-14]. （原始内容存档于2015-02-08）（英语）.
NTSB Report: ENG09WA015. National Transportation Safety Board. [2012-01-14]. （原始内容存档于2012-09-26）（英语）.
NTSB Report: ENG09WA012. National Transportation Safety Board. [2012-01-14]. （原始内容存档于2012-09-26）（英语）.
NTSB Report: ENG11IA011. National Transportation Safety Board. [2012-01-14]. （原始内容存档于2012-10-17）（英语）.
NTSB Report: ENG11WA017. National Transportation Safety Board. [2012-01-14]. （原始内容存档于2012-10-17）（英语）.
How Southwest Flight 1380'S Pilots Landee with a blown engine. Wired. [2018-04-18]. （原始内容存档于2018-04-18）（英语）.

webcitation.org

Angrand, A. Tech Insertion: Eternal youth for the CFM56 (PDF). SAFRAN magazine. 2007年11月: 26 [2012-01-27]. （原始内容 (pdf)存档于2010-04-09）（英语）.

wired.com

How Southwest Flight 1380'S Pilots Landee with a blown engine. Wired. [2018-04-18]. （原始内容存档于2018-04-18）（英语）.