Guide vane assembly

• US 6,764,276 B2
• Filed: 07/24/2002
• Issued: 07/20/2004
• Est. Priority Date: 08/11/2001
• Status: Expired due to Term

• Current Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Inventors: Evans, Richard, Mulcaire, Thomas G, Holdsworth, Michael T
• Primary Examiner(s): Look, Edward K.
• Assistant Examiner(s): White, Dwayne J.
• Application Number:
  US10/201,195
• Publication Number:
  US 20030031556A1
• Time in Patent Office: 727 Days
• Field of Search: 415/9, 415/119, 415/173.1, 415/173.4, 415/196, 415/197, 415/200
• US Class Current: 415/119
• CPC Class Codes: F01D 5/00 Blades; Blade-carrying members nozzle boxes F01D9/02; Heating, heat-insulating, cooling or antivibration means on the blades or the members special arrangements in rotors dealing with breaking off of part thereof F01D21/045
• CPC Class Codes: F01D 9/041 using blades F01D5/148 takes precedence
• CPC Class Codes: F02C 7/045 having provisions for noise suppression
• CPC Class Codes: F02K 3/04 the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
• CPC Class Codes: F04D 29/667 by influencing the flow pattern, e.g. suppression of turbulence
• CPC Class Codes: F04D 29/681 especially adapted for elastic fluid pumps
• CPC Class Codes: F05D 2240/55 Seals
• CPC Class Codes: F05D 2250/191 perforated
• CPC Class Codes: F05D 2250/283 honeycomb
• CPC Class Codes: F05D 2260/96 Preventing, counteracting or reducing vibration or noise

Abstract

A fan outlet guide vane assembly (36) for a turbofan gas turbine engine (10) comprises a fan casing (32) and a plurality of circumferentially spaced radially extending fan outlet guide vanes (34). The fan outlet guide vanes (34) are secured at their radially outer ends to the fan casing (32). A plurality of panels (40) are secured to the fan casing (32). Each panel (40) is arranged between two adjacent fan outlet guide vanes (34) to define the flow path between the fan outlet guide vanes (34). Each panel (40) comprises a perforated skin (42) and a honeycomb structure (44) to form an acoustic treatment structure. The perforated skin (42) defines the flow path between the fan outlet guide vanes (34). The pressure equalization across the panels (40) minimises the possibility of the panels (40) being removed.

Claims

1. A guide vane assembly comprising a casing, a plurality of circumferentially spaced radially extending guide vanes, the guide vanes being secured at their radially outer ends to the casing, a plurality of panels being secured to the casing, each panel being arranged between two adjacent guide vanes to define the flow path between the guide vanes, at least one panel comprising a perforated skin and an acoustic treatment structure, the perforated skin defining the flow path between the guide vanes and with each panel being located circumferentially between two adjacent guide vanes.

2. A guide vane assembly as claimed in claim 1 wherein each panel comprises a perforated skin and an acoustic treatment structure, the perforated skin defining the flow path between the guide vanes.

3. A guide vane assembly as claimed in claim 1 wherein the at least one panel is secured to the casing by fasteners or by an adhesive bond and fasteners.

4. A guide vane assembly as claimed in claim 1 wherein the perforated skin of the at least one panel comprises a composite material.

5. A guide vane assembly as claimed in claim 1 wherein the guide vanes are secured to the casing by fasteners or by welded joints.

6. A guide vane assembly as claimed in claim 1 wherein the guide vanes are fan outlet guide vanes and the casing is a fan casing.

7. A guide vane assembly as claimed in claims 1 wherein the acoustic treatment is provided with drainage apertures to allow water and/or lubricant to flow generally axially and to prevent water or/lubricant flowing generally circumferentially between the panel and the casing between the two adjacent guide vanes.

8. A guide vane assembly as claimed in claim 1 wherein the acoustic treatment structure comprises a honeycomb structure.

9. A guide vane assembly as claimed in claim 8 wherein the honeycomb structure comprises a plurality of cells, each cell having eight sides or less.

10. A guide vane assembly as claimed in claim 9 wherein the honeycomb structure comprises an aluminium honeycomb, a composite material honeycomb or other suitable honeycomb.

11. A guide vane assembly as claimed in claim 1 wherein the perforated skin and the acoustic treatment structure are integral.

12. A guide vane assembly as claimed in claim 11 wherein the perforated skin and the acoustic treatment comprises a composite material or a metal.

13. A guide vane assembly as claimed in claim 12 wherein the perforated skin and the acoustic treatment comprises aluminium or glass fibre reinforced nylon.

14. A guide vane assembly comprising a casing, a plurality of circumferentially spaced radially extending guide vanes, the guide vanes being secured at their radially outer ends to the casing, a plurality of panels being secured to the casing, each panel being arranged between two adjacent guide vanes to define the flow path between the guide vanes, at least one panel comprising a perforated skin and an acoustic treatment structure, the perforated skin defining the flow path between the guide vanes wherein a flexible seal is arranged between the circumferential edges of the at least one panel and the two adjacent fan outlet guide vanes to seal the gaps between the circumferential edges of the at least one panel and the two adjacent fan outlet guide vanes.