Patent search ap:("UNITED TECHNOLOGIES CORP") AND inv:"FARRELL MARVIN D" Page 2

11.

发明专利
未知

公开(公告)号：DE69318713D1

公开(公告)日：1998-06-25

申请号：DE69318713

申请日：1993-06-18

Applicant: UNITED TECHNOLOGIES CORP

Inventor： CYPON JAMES P , HUNTER DAVID H , KOHLHEPP FRED W , KRAUSS TIMOTHY A , MILLEA VINCENT F , FURNES KENNETH M , FARRELL MARVIN D , SANDY DAVID F , BEATTY ROBERT D , HANSEN BRUCE D

IPC: B64C27/10 , B64C27/12 , B64C27/14 , B64C27/20 , B64C27/33 , B64C27/46 , B64C27/473 , B64C27/605 , B64C29/00 , B64C39/02 , B64C39/06 , F02B75/02 , F16C11/06 , F16D1/02 , F16D1/05 , F16D1/06 , F16D3/06 , F16D3/18 , F16D41/07 , F16F15/10 , F16H1/14 , F16H1/22

12.

发明专利
A drive train assembly for an unmanned aerial vehicle having ducted, coaxial counter-rotating rotors 未知

公开(公告)号：AU667650B2

公开(公告)日：1996-03-28

申请号：AU1017895

申请日：1995-01-13

Applicant: UNITED TECHNOLOGIES CORP

Inventor： CYPON JAMES P , HUNTER DAVID H , KOHLHEPP FRED W , KRAUSS TIMOTHY A , MILLEA VINCENT F , FURNES KENNETH M , FARRELL MARVIN D , SANDY DAVID F , BEATTY ROBERT D , HANSEN BRUCE D

IPC: B64C27/10 , B64C27/12 , B64C27/14 , B64C27/20 , B64C27/33 , B64C27/46 , B64C27/473 , B64C27/605 , B64C29/00 , B64C39/02 , B64C39/06 , F02B75/02 , F16C11/06 , F16D1/02 , F16D1/05 , F16D1/06 , F16D3/06 , F16D3/18 , F16D41/07 , F16F15/10 , F16H1/14 , F16H1/22 , B64D35/06

13.

发明专利
An integrated spline/cone seat subassembly for the rotor assembly of an unmanned aerial vehicle having ducted, coaxial counter-rotating rotors 未知

公开(公告)号：AU1018095A

公开(公告)日：1995-03-09

申请号：AU1018095

申请日：1995-01-13

Applicant: UNITED TECHNOLOGIES CORP

Inventor： CYPON JAMES P , HUNTER DAVID H , KOHLHEPP FRED W , KRAUSS TIMOTHY A , MILLEA VINCENT F , FURNES KENNETH M , FARRELL MARVIN D , SANDY DAVID F , BEATTY ROBERT D , HANSEN BRUCE D

IPC: B64C27/10 , B64C27/12 , B64C27/14 , B64C27/20 , B64C27/33 , B64C27/46 , B64C27/473 , B64C27/605 , B64C29/00 , B64C39/02 , B64C39/06 , F02B75/02 , F16C11/06 , F16D1/02 , F16D1/05 , F16D1/06 , F16D3/06 , F16D3/18 , F16D41/07 , F16F15/10 , F16H1/14 , F16H1/22 , B64D35/06 , B64C27/32

Abstract: An integrated spline/cone seat subassembly (190) for an unmanned aerial vehicle (10) having a rotor assembly (100) that includes ducted, counter-rotating rotors (200, 202), comprising:a rotor shaft (128R or 130R) having an axis, said rotor shaft (128R or 130R) includinga primary shaft portion (192) having a first diameter (D 1 ),an end shaft portion (194) having a second diameter (D 2 ) and having a plurality of shaft splines (198) extending radially outwardly therefrom, anda conic transition portion (196) intermediate said primary and end shaft portions (192, 194), said conic transition portion (196) making a predetermined angle (β) with respect to said axis of said rotor shaft (128R or 130R); anda rotor hub (204) having a centerline (212), said rotor hub (204) having a shaft aperture (206) having a plurality of hub splines (208) extending radially inwardly therefrom;said plurality of hub splines (208) and said plurality of shaft splines (198) being interleaved in combination to provide a rotational interlock between said rotor hub (204) and said rotor shaft (128R or 130R) in the rotor assembly (100); characterized in thateach of said hub splines (208) having an outwardly tapered lower portion (210) that makes a predetermined angle (θ) with respect to said centerline (212); andsaid predetermined angle (θ) of said outwardly tapered lower portions (210) of said hub splines (208) being equal to said predetermined angle (β) of said conic transition portion (196) of said rotor shaft (128R or 130R) wherein said tapered lower portions (210) of said hub splines (208) abuttingly engage and are mechanically supported by said conic transition portion (196) of said rotor shaft (128R or 130R) in the rotor assembly (100).

14.

发明专利
A coaxial transmission/center hub subassembly for the rotor assembly of an unmanned aerial vehicle having ducted, coaxial counter-rotating rotors 未知

公开(公告)号：AU1017995A

公开(公告)日：1995-03-09

申请号：AU1017995

申请日：1995-01-13

Applicant: UNITED TECHNOLOGIES CORP

Inventor： CYPON JAMES P , HUNTER DAVID H , KOHLHEPP FRED W , KRAUSS TIMOTHY A , MILLEA VINCENT F , FURNES KENNETH M , FARRELL MARVIN D , SANDY DAVID F , BEATTY ROBERT D , HANSEN BRUCE D

IPC: B64C27/10 , B64C27/12 , B64C27/14 , B64C27/20 , B64C27/33 , B64C27/46 , B64C27/473 , B64C27/605 , B64C29/00 , B64C39/02 , B64C39/06 , F02B75/02 , F16C11/06 , F16D1/02 , F16D1/05 , F16D1/06 , F16D3/06 , F16D3/18 , F16D41/07 , F16F15/10 , F16H1/14 , F16H1/22 , B64C11/02 , B64C27/32 , B64D35/06

Abstract: An integrated spline/cone seat subassembly (190) for an unmanned aerial vehicle (10) having a rotor assembly (100) that includes ducted, counter-rotating rotors (200, 202), comprising:a rotor shaft (128R or 130R) having an axis, said rotor shaft (128R or 130R) includinga primary shaft portion (192) having a first diameter (D 1 ),an end shaft portion (194) having a second diameter (D 2 ) and having a plurality of shaft splines (198) extending radially outwardly therefrom, anda conic transition portion (196) intermediate said primary and end shaft portions (192, 194), said conic transition portion (196) making a predetermined angle (β) with respect to said axis of said rotor shaft (128R or 130R); anda rotor hub (204) having a centerline (212), said rotor hub (204) having a shaft aperture (206) having a plurality of hub splines (208) extending radially inwardly therefrom;said plurality of hub splines (208) and said plurality of shaft splines (198) being interleaved in combination to provide a rotational interlock between said rotor hub (204) and said rotor shaft (128R or 130R) in the rotor assembly (100); characterized in thateach of said hub splines (208) having an outwardly tapered lower portion (210) that makes a predetermined angle (θ) with respect to said centerline (212); andsaid predetermined angle (θ) of said outwardly tapered lower portions (210) of said hub splines (208) being equal to said predetermined angle (β) of said conic transition portion (196) of said rotor shaft (128R or 130R) wherein said tapered lower portions (210) of said hub splines (208) abuttingly engage and are mechanically supported by said conic transition portion (196) of said rotor shaft (128R or 130R) in the rotor assembly (100).

15.

发明专利
A drive train assembly for an unmanned aerial vehicle having ducted, coaxial counter-rotating rotors 未知

公开(公告)号：AU1017895A

公开(公告)日：1995-03-09

申请号：AU1017895

申请日：1995-01-13

Applicant: UNITED TECHNOLOGIES CORP

Inventor： CYPON JAMES P , HUNTER DAVID H , KOHLHEPP FRED W , KRAUSS TIMOTHY A , MILLEA VINCENT F , FURNES KENNETH M , FARRELL MARVIN D , SANDY DAVID F , BEATTY ROBERT D , HANSEN BRUCE D

IPC: B64C27/10 , B64C27/12 , B64C27/14 , B64C27/20 , B64C27/33 , B64C27/46 , B64C27/473 , B64C27/605 , B64C29/00 , B64C39/02 , B64C39/06 , F02B75/02 , F16C11/06 , F16D1/02 , F16D1/05 , F16D1/06 , F16D3/06 , F16D3/18 , F16D41/07 , F16F15/10 , F16H1/14 , F16H1/22 , B64D35/06

Abstract: An integrated spline/cone seat subassembly (190) for an unmanned aerial vehicle (10) having a rotor assembly (100) that includes ducted, counter-rotating rotors (200, 202), comprising:a rotor shaft (128R or 130R) having an axis, said rotor shaft (128R or 130R) includinga primary shaft portion (192) having a first diameter (D 1 ),an end shaft portion (194) having a second diameter (D 2 ) and having a plurality of shaft splines (198) extending radially outwardly therefrom, anda conic transition portion (196) intermediate said primary and end shaft portions (192, 194), said conic transition portion (196) making a predetermined angle (β) with respect to said axis of said rotor shaft (128R or 130R); anda rotor hub (204) having a centerline (212), said rotor hub (204) having a shaft aperture (206) having a plurality of hub splines (208) extending radially inwardly therefrom;said plurality of hub splines (208) and said plurality of shaft splines (198) being interleaved in combination to provide a rotational interlock between said rotor hub (204) and said rotor shaft (128R or 130R) in the rotor assembly (100); characterized in thateach of said hub splines (208) having an outwardly tapered lower portion (210) that makes a predetermined angle (θ) with respect to said centerline (212); andsaid predetermined angle (θ) of said outwardly tapered lower portions (210) of said hub splines (208) being equal to said predetermined angle (β) of said conic transition portion (196) of said rotor shaft (128R or 130R) wherein said tapered lower portions (210) of said hub splines (208) abuttingly engage and are mechanically supported by said conic transition portion (196) of said rotor shaft (128R or 130R) in the rotor assembly (100).

16.

发明专利
DAMPENING UNIT FOR MAIN ROTORS OF UNMANNED FLYING VEHICLES 未知

公开(公告)号：RU2117604C1

公开(公告)日：1998-08-20

申请号：RU95106357

申请日：1993-06-18

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SAJKON DZHEJMS P , KHANTER DEHVID KH , KOL KHEPP FRED V , KRAUSS TIMOTI A , MILLEA VINSENT F , FERNESS KENNET M , FARRELL MARVIN D , SANDI DEHVID F , BITTI ROBERT D , KHANSEN BRJUS D

IPC: B64C27/46 , B64C27/20 , B64C27/33 , B64C27/605 , B64C39/02 , F02B75/02

Abstract: FIELD: aircraft manufacture; designing of dampening units for main rotors of unmanned flying vehicles. SUBSTANCE: dampening unit includes main rotor hub, torsion tubes and flexible beams; each torsion tube is connected with respective flexible beam its inner end with the aid of holder fitted with spherical bearing. Main rotor hub is connected with main rotor shaft and is provided with many outer radial panels having attachment units for securing the hub to inner ends of flexible beams and units for mounting the holders with their spherical bearings in hub. Assembly of each holder with its spherical bearing is located inside outer end of one of outer radial panels and inner end of respective flexible beam. According to invention, members for securing the outer radial panels of hub to inner ends of flexible beams are made in form of forks. Each unit for mounting the holder with spherical bearing on respective outer panel of main rotor hub includes near and far partitions and bearing bolt. Partitions bound bearing cavity and inner cavity of hub; bearing bolt is connected with each partition and spherical bearing for turn of holder in bearing cavity. EFFECT: optimization of construction and ease in maintenance. 3 cl, 32 dwg