FR1267419A - Air deoiling installation in aircraft compressors or the like - Google Patents

Air deoiling installation in aircraft compressors or the like

Info

Publication number
FR1267419A
FR1267419A FR838089A FR838089A FR1267419A FR 1267419 A FR1267419 A FR 1267419A FR 838089 A FR838089 A FR 838089A FR 838089 A FR838089 A FR 838089A FR 1267419 A FR1267419 A FR 1267419A
Authority
FR
France
Prior art keywords
installation
air deoiling
compressors
aircraft
aircraft compressors
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
FR838089A
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.)
ENTWICKLUNGSBAU PIRNA VEB
Original Assignee
ENTWICKLUNGSBAU PIRNA VEB
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 ENTWICKLUNGSBAU PIRNA VEB filed Critical ENTWICKLUNGSBAU PIRNA VEB
Priority to FR838089A priority Critical patent/FR1267419A/en
Application granted granted Critical
Publication of FR1267419A publication Critical patent/FR1267419A/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
    • F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
    • F01D11/04—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type using sealing fluid, e.g. steam

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR838089A 1960-09-08 1960-09-08 Air deoiling installation in aircraft compressors or the like Expired FR1267419A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR838089A FR1267419A (en) 1960-09-08 1960-09-08 Air deoiling installation in aircraft compressors or the like

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR838089A FR1267419A (en) 1960-09-08 1960-09-08 Air deoiling installation in aircraft compressors or the like

Publications (1)

Publication Number Publication Date
FR1267419A true FR1267419A (en) 1961-07-21

Family

ID=8738675

Family Applications (1)

Application Number Title Priority Date Filing Date
FR838089A Expired FR1267419A (en) 1960-09-08 1960-09-08 Air deoiling installation in aircraft compressors or the like

Country Status (1)

Country Link
FR (1) FR1267419A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114704386A (en) * 2022-04-24 2022-07-05 中国航发沈阳发动机研究所 Sealing method and structure for turbine engine fulcrum of hypersonic vehicle

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114704386A (en) * 2022-04-24 2022-07-05 中国航发沈阳发动机研究所 Sealing method and structure for turbine engine fulcrum of hypersonic vehicle
CN114704386B (en) * 2022-04-24 2024-03-19 中国航发沈阳发动机研究所 Sealing method and structure for turbine engine pivot of hypersonic vehicle

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