公开(公告)号：DE2949156A1

公开(公告)日：1980-06-26

申请号：DE2949156

申请日：1979-12-06

Applicant: UNITED TECHNOLOGIES CORP

Inventor： FERRIS DONALD LEROY ,  OGLE PETER CHASE

IPC: B64C27/35 ,  B64C27/33 ,  B64C27/48

Abstract: A helicopter rotor having an even number of articulated blades wherein opposing blades are interconnected by a common spar passing across the rotor axis. Pitch change is introduced to the blade at the spar-blade attachment joint through a torque member connected at its outboard end to the blade joint and including a control horn at its inner end to receive pitch inputs. Drive for the rotor and support for each blade is provided by a spherical bearing directly connecting the torque member to the blade associated hub arm.

公开(公告)号：DE2927263A1

公开(公告)日：1980-01-24

申请号：DE2927263

申请日：1979-07-05

Applicant: UNITED TECHNOLOGIES CORP

Inventor： FERRIS DONALD LEROY ,  NOEHREN WILLIAM LAWRENCE ,  OGLE PETER CHASE

IPC: B64C27/33 ,  B64C27/32

公开(公告)号：NO792286A

公开(公告)日：1980-01-15

申请号：NO792286

申请日：1979-07-10

Applicant: UNITED TECHNOLOGIES CORP

Inventor： FERRIS DONALD LEROY ,  OGLE PETER CHASE ,  NOEHREN WILLIAM LAWRENCE

IPC: B64C27/33 ,  B64C

CPC classification number: B64C27/33

公开(公告)号：MY8600125A

公开(公告)日：1986-12-31

申请号：MY8600125

申请日：1986-12-30

Applicant: UNITED TECHNOLOGIES CORP USA D

Inventor： FERRIS DONALD LEROY ,  OGLE PETER CHASE

IPC: B64C27/00 ,  B64C27/32 ,  B64C27/48 ,  B64D45/00

Abstract: A helicopter rotor blade to hub arm attachment configured to react centrifugal loads from the blade through a blade cuff, spindle, and elastomeric bearings utilizes a pre-loaded bolt through the spindle for load sharing therewith and a spindle integrity monitoring indicator to provide a visual showing of a deviation from the normal load sharing proportion.

公开(公告)号：DE3068997D1

公开(公告)日：1984-09-27

申请号：DE3068997

申请日：1980-04-10

Applicant: UNITED TECHNOLOGIES CORP

Inventor： FERRIS DONALD LEROY ,  OGLE PETER CHASE

IPC: B64C27/32 ,  B64C27/35

公开(公告)号：CH637890A5

公开(公告)日：1983-08-31

申请号：CH638179

申请日：1979-07-09

Applicant: UNITED TECHNOLOGIES CORP

Inventor： FERRIS DONALD LEROY ,  NOEHREN WILLIAM LAWRENCE ,  OGLE PETER CHASE

IPC: B64C27/33 ,  B64C27/35

公开(公告)号：AU530102B2

公开(公告)日：1983-06-30

申请号：AU5731880

申请日：1980-04-10

Applicant: UNITED TECHNOLOGIES CORP

Inventor： FERRIS DONALD LEROY

IPC: B64C27/50 ,  B64C11/28

Abstract: In a fully articulated helicopter rotor head, utilizing an elastomeric bearing to support each rotor blade and react centrifugal flight loads, a blade restraint, effective in three axes is provided for use during blade folding for aircraft stowage purposes. The restraint allows the blade to be folded through a predetermined fold plane, and held there while preventing or minimizing deflection of the elastomeric bearing.

公开(公告)号：NO148144B

公开(公告)日：1983-05-09

申请号：NO803954

申请日：1980-12-30

Applicant: UNITED TECHNOLOGIES CORP

Inventor： FERRIS DONALD LEROY ,  OGLE PETER CHASE

IPC: B64C27/32 ,  B64C27/35 ,  B64C27/38

公开(公告)号：NO146273C

公开(公告)日：1982-09-01

申请号：NO792286

申请日：1979-07-10

Applicant: UNITED TECHNOLOGIES CORP

Inventor： FERRIS DONALD LEROY ,  NOEHREN WILLIAM LAWRENCE ,  OGLE PETER CHASE

IPC: B64C27/33 ,  B64C27/32

公开(公告)号：NO145830B

公开(公告)日：1982-03-01

申请号：NO792116

申请日：1979-06-25

Applicant: UNITED TECHNOLOGIES CORP

Inventor： FERRIS DONALD LEROY ,  HIBYAN EDWARD STANLEY ,  FAIZ ROBERT LEE

IPC: B64C27/32 ,  B64C27/35 ,  B64C27/48

Abstract: A helicopter rotor having one or more blades mounted for rotation with the rotor hub and each supported therefrom by an elastomeric bearing, and having a lead-lag damper connected to the blade and the hub and extending substantially parallel to the blade axis, and including the improvement of apparatus for preventing tension loading of the elastomeric bearing as the blade moves radially inwardly as a result of rotor braking.