Seal between the inner and outer casings of a turbojet section
The invention relates to a turbojet section comprising an external casing having a surface that extends radially inwards, an internal casing having an essentially axial wall that extends toward said surface, and a seal located between said wall and said surface to prevent communication between the h...
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| creator | LEJARS CLAUDE |
| description | The invention relates to a turbojet section comprising an external casing having a surface that extends radially inwards, an internal casing having an essentially axial wall that extends toward said surface, and a seal located between said wall and said surface to prevent communication between the high and low pressure regions situated on either side of said seal, in which said seal is made in the form of an annular sheet-metal ring comprising an essentially cylindrical first part fixed in a leaktight manner to one face of the axial wall and a second part continuing from said first part and situated in the space separating said axial wall from said radial surface, said second part exhibiting, in section on a radial plane containing the axis of the turbojet, a V-shaped profile and having an end portion in leaktight sliding contact with said radial surface. |
| format | Patent |
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that extends toward said surface, and a seal located between said wall and said surface to prevent communication between the high and low pressure regions situated on either side of said seal, in which said seal is made in the form of an annular sheet-metal ring comprising an essentially cylindrical first part fixed in a leaktight manner to one face of the axial wall and a second part continuing from said first part and situated in the space separating said axial wall from said radial surface, said second part exhibiting, in section on a radial plane containing the axis of the turbojet, a V-shaped profile and having an end portion in leaktight sliding contact with said radial surface.</description><edition>7</edition><language>eng</language><subject>BLASTING ; CYLINDERS ; ENGINE PLANTS IN GENERAL ; ENGINEERING ELEMENTS AND UNITS ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HEATING ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; NON-POSITIVE DISPLACEMENT PUMPS ; PISTONS ; POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS ; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS ; SEALINGS ; STEAM ENGINES ; THERMAL INSULATION IN GENERAL ; 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MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>NON-POSITIVE DISPLACEMENT PUMPS</topic><topic>PISTONS</topic><topic>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</topic><topic>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</topic><topic>SEALINGS</topic><topic>STEAM ENGINES</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>LEJARS CLAUDE</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LEJARS CLAUDE</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Seal between the inner and outer casings of a turbojet section</title><date>2005-11-03</date><risdate>2005</risdate><abstract>The invention relates to a turbojet section comprising an external casing having a surface that extends radially inwards, an internal casing having an essentially axial wall that extends toward said surface, and a seal located between said wall and said surface to prevent communication between the high and low pressure regions situated on either side of said seal, in which said seal is made in the form of an annular sheet-metal ring comprising an essentially cylindrical first part fixed in a leaktight manner to one face of the axial wall and a second part continuing from said first part and situated in the space separating said axial wall from said radial surface, said second part exhibiting, in section on a radial plane containing the axis of the turbojet, a V-shaped profile and having an end portion in leaktight sliding contact with said radial surface.</abstract><edition>7</edition><oa>free_for_read</oa></addata></record> |
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| language | eng |
| recordid | cdi_epo_espacenet_US2005242522A1 |
| source | esp@cenet |
| subjects | BLASTING CYLINDERS ENGINE PLANTS IN GENERAL ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES NON-POSITIVE DISPLACEMENT PUMPS PISTONS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS SEALINGS STEAM ENGINES THERMAL INSULATION IN GENERAL WEAPONS |
| title | Seal between the inner and outer casings of a turbojet section |
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