FR1235694A - Seal structure resistant to high temperatures and fuels for jet engines and similar applications - Google Patents

Seal structure resistant to high temperatures and fuels for jet engines and similar applications

Info

Publication number
FR1235694A
FR1235694A FR801251A FR801251A FR1235694A FR 1235694 A FR1235694 A FR 1235694A FR 801251 A FR801251 A FR 801251A FR 801251 A FR801251 A FR 801251A FR 1235694 A FR1235694 A FR 1235694A
Authority
FR
France
Prior art keywords
fuels
high temperatures
seal structure
jet engines
similar applications
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
FR801251A
Other languages
French (fr)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Connecticut Hard Rubber Co
Original Assignee
Connecticut Hard Rubber Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Connecticut Hard Rubber Co filed Critical Connecticut Hard Rubber Co
Application granted granted Critical
Publication of FR1235694A publication Critical patent/FR1235694A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005—Sealing means between non relatively rotating elements
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
FR801251A 1958-07-28 1959-07-27 Seal structure resistant to high temperatures and fuels for jet engines and similar applications Expired FR1235694A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US1235694XA 1958-07-28 1958-07-28

Publications (1)

Publication Number Publication Date
FR1235694A true FR1235694A (en) 1960-07-08

Family

ID=22409453

Family Applications (1)

Application Number Title Priority Date Filing Date
FR801251A Expired FR1235694A (en) 1958-07-28 1959-07-27 Seal structure resistant to high temperatures and fuels for jet engines and similar applications

Country Status (1)

Country Link
FR (1) FR1235694A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0657624A1 (en) * 1993-12-08 1995-06-14 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Turbine housing containing a sealing body
EP2829689A1 (en) * 2013-07-23 2015-01-28 MTU Aero Engines GmbH Insulating structure for a thermal gas turbine, coresponding thermal gas turbine and method of manufacturing

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0657624A1 (en) * 1993-12-08 1995-06-14 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Turbine housing containing a sealing body
FR2713709A1 (en) * 1993-12-08 1995-06-16 Snecma Turbomachine wall comprising a sealing body.
EP2829689A1 (en) * 2013-07-23 2015-01-28 MTU Aero Engines GmbH Insulating structure for a thermal gas turbine, coresponding thermal gas turbine and method of manufacturing
US9771827B2 (en) 2013-07-23 2017-09-26 MTU Aero Engines AG Damping device for being situated between a housing wall and a casing ring of a housing of a thermal gas turbine

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