Unlock instant, AI-driven research and patent intelligence for your innovation.

Reinforced shaped composite shell

A technology of composite materials and shells, which is applied in liquid fuel engines, components of pumping devices for elastic fluids, machines/engines, etc., can solve problems that are not conducive to the total weight of the shell, the overall size and weight of the shell, Shell manufacturing and installation equipment and other issues

Active Publication Date: 2021-08-10
SAFRAN AIRCRAFT ENGINES SAS
View PDF12 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, this solution leads to a substantial increase in the overall size and weight of the housing
Furthermore, due to the complex omega-shape of the housing, it was found difficult to manufacture and install equipment (e.g. acoustic panels, wearable boxes) on this type of housing
Finally, the cavity formed by the Ω-shaped part requires filling material, further detrimental to the overall weight of the case

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Reinforced shaped composite shell
  • Reinforced shaped composite shell
  • Reinforced shaped composite shell

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0035] The invention is generally applicable to any gas turbine casing made of composite material.

[0036] The invention is described below in the context of its application to a fan casing of a gas turbine aeroengine.

[0037] Such as figure 1 As schematically shown in , this engine includes, from upstream to downstream along the flow direction of the airflow: a fan 1 arranged at the inlet of the engine; a compressor 2; a combustion chamber 3; a high-pressure turbine 4; and a low-pressure turbine 5.

[0038] The engine is housed within a housing comprising a number of sections corresponding to the different elements of the engine. The fan 1 is thus surrounded by an axisymmetric fan housing 10 .

[0039] figure 2 The profile of the fan housing 10 is shown, which is parallel to the axis A of the housing 10 10 The radial direction D A and by the radial direction DR Sections in defined planes correspond to . In this example, the housing 10 is made of an organic matrix com...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

PropertyMeasurementUnit
radiusaaaaaaaaaa
radiusaaaaaaaaaa
Login to View More

Abstract

A gas turbine casing (10) made of composite material, said casing having an axisymmetric shape and comprising, along an axial direction (DA): an upstream flange (14); a holding area (15), said holding the thickness of the zone is greater than the rest of the shell; and the downstream flange (16). Housing (10) in the axial direction (D A ) and the radial direction (D R ) has a profile in section on a plane defined, said profile comprising at least first and second sloped portions (17, 18), said first and second sloped portions (17, 18) relative to each other and relative to Axis of the housing (A 10 )tilt. The first and second sloping portions meet at a point (S10) between the retaining area (15) and one of the flanges (16, 14), which is connected to the first and second sloping portions (17, 18). ) corresponding to the vertex (19) of the angle (β1) formed. Angle (β 1 ) vertex (19) and the average radius of the shell (Rm 10 ) between the distance (d 19 ) within the range of 1.5% and 4% of said mean radius of the shell.

Description

technical field [0001] The present invention relates to gas turbine casings, and more particularly, but not exclusively, to gas turbine fan casings for aircraft engines. Background technique [0002] In gas turbine aero-engines, the fan casing performs several functions. In particular, it defines an air inlet passage into the engine, which optionally supports abradable material facing the tips of the fan blades and / or a sound absorber structure for acoustic treatment at the engine inlet, which incorporates or supports a retaining shroud . [0003] Housings, such as fan housings, used to be made of metallic materials, but are now made of composite materials, i.e. fiber preforms of composite materials densified with an organic matrix, enabling the manufacture of components that, when they When made of metallic material, the part has a lower overall weight than the same part, while also having at least equal, if not greater, mechanical strength. A fan housing made of organic...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Patents(China)
IPC IPC(8): F04D29/52
CPCF04D29/522F05D2300/601F05D2300/603F01D25/24F05D2220/36F01D25/243F05D2240/14Y02T50/60B29B11/16B29C70/24B29L2031/7504F05D2260/96F05D2300/6033
Inventor 塞德里克·扎卡蒂玛蒂尔德·安内尔·梅丽西亚·索拉特
Owner SAFRAN AIRCRAFT ENGINES SAS