公开(公告)号：FR2572358B1

公开(公告)日：1987-01-30

申请号：FR8510757

申请日：1985-07-12

Applicant: UNITED TECHNOLOGIES CORP

Inventor： CARTER DONALD R ,  KRAUSS TIMOTHY A ,  SEDLAK MATTHEW

IPC: B64C27/46 ,  B64C27/32 ,  B64C27/467 ,  B64C27/72 ,  B64C27/22 ,  B64C21/04

Abstract: A circulation control aircraft rotor blade having a spanwise Coanda surface 16 and a plurality of spanwise extending flexible composite material panels 18 cooperating with the surface to define slots for the discharge of compressed air from within the blade with each panel having first flexure means 60 associated with screw adjustments 36 for establishing a slot opening preload and second flexure means 62 associated with screw adjustments 38 for establishing a slot maximum opening.

公开(公告)号：DE3524483A1

公开(公告)日：1986-05-07

申请号：DE3524483

申请日：1985-07-09

Applicant: UNITED TECHNOLOGIES CORP

Inventor： CARTER DONALD R ,  KRAUSS TIMOTHY A ,  SEDLAK MATTHEW

IPC: B64C27/46 ,  B64C27/32 ,  B64C27/467 ,  B64C27/18

Abstract: A circulation control aircraft rotor blade having a spanwise Coanda surface 16 and a plurality of spanwise extending flexible composite material panels 18 cooperating with the surface to define slots for the discharge of compressed air from within the blade with each panel having first flexure means 60 associated with screw adjustments 36 for establishing a slot opening preload and second flexure means 62 associated with screw adjustments 38 for establishing a slot maximum opening.

公开(公告)号：FR2572358A1

公开(公告)日：1986-05-02

申请号：FR8510757

申请日：1985-07-12

Applicant: UNITED TECHNOLOGIES CORP

Inventor： CARTER DONALD R ,  KRAUSS TIMOTHY A ,  SEDLAK MATTHEW

IPC: B64C27/46 ,  B64C27/32 ,  B64C27/467 ,  B64C27/72 ,  B64C27/22 ,  B64C21/04

Abstract: A circulation control aircraft rotor blade having a spanwise Coanda surface 16 and a plurality of spanwise extending flexible composite material panels 18 cooperating with the surface to define slots for the discharge of compressed air from within the blade with each panel having first flexure means 60 associated with screw adjustments 36 for establishing a slot opening preload and second flexure means 62 associated with screw adjustments 38 for establishing a slot maximum opening.

公开(公告)号：GB2166104A

公开(公告)日：1986-04-30

申请号：GB8516708

申请日：1985-07-02

Applicant: UNITED TECHNOLOGIES CORP

Inventor： CARTER DONALD R ,  KRAUSS TIMOTHY A ,  SEDLAK MATTHEW

IPC: B64C27/46 ,  B64C27/32 ,  B64C27/467 ,  B64C21/08

Abstract: A circulation control aircraft rotor blade having a spanwise Coanda surface 16 and a plurality of spanwise extending flexible composite material panels 18 cooperating with the surface to define slots for the discharge of compressed air from within the blade with each panel having first flexure means 60 associated with screw adjustments 36 for establishing a slot opening preload and second flexure means 62 associated with screw adjustments 38 for establishing a slot maximum opening.