USD920216S1 - Combined stator and spindle for a ducted rotor - Google Patents

Combined stator and spindle for a ducted rotor Download PDF

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Publication number
USD920216S1
USD920216S1 US29/719,446 US202029719446F USD920216S US D920216 S1 USD920216 S1 US D920216S1 US 202029719446 F US202029719446 F US 202029719446F US D920216 S USD920216 S US D920216S
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United States
Prior art keywords
spindle
ducted rotor
combined stator
stator
ducted
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
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US29/719,446
Inventor
Joseph Richard Carpenter
Steve Michael Loveland
Allen Brittain
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Bell Textron Inc
Original Assignee
Bell Textron Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Bell Textron Inc filed Critical Bell Textron Inc
Priority to US29/719,446 priority Critical patent/USD920216S1/en
Assigned to Bell Textron Inc. reassignment Bell Textron Inc. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: Brittain, Allen, CARPENTER, Joseph Richard, LOVELAND, Steve Michael
Application granted granted Critical
Publication of USD920216S1 publication Critical patent/USD920216S1/en
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FIG. 1 is a front plan view of our new design for a combined stator and spindle for a ducted rotor;
FIG. 2 is a side view in elevation of the stator and spindle as shown in FIG. 1;
FIG. 3 is a top plan view of the stator and spindle as shown in FIG. 1;
FIG. 4 is a front elevational view of the stator and spindle as shown in FIG. 1;
FIG. 5 is a bottom plan view of the stator and spindle as shown in FIG. 1;
FIG. 6 is a rear elevational view of the stator and spindle as shown in FIG. 1;
FIG. 7 is a front environmental perspective view of the stator and spindle as shown in FIG. 1; and,
FIG. 8 is a rear environmental perspective view of the stator and spindle as shown in FIG. 1.
The broken lines FIGS. 7 and 8 of the drawings are for the purpose of illustrating environmental structure and form no part of the claimed design.

Claims (1)

    CLAIM
  1. The ornamental design for a combined stator and spindle for a ducted rotor, substantially as shown and described.
US29/719,446 2020-01-03 2020-01-03 Combined stator and spindle for a ducted rotor Active USD920216S1 (en)

Priority Applications (1)

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US29/719,446 USD920216S1 (en) 2020-01-03 2020-01-03 Combined stator and spindle for a ducted rotor

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US29/719,446 USD920216S1 (en) 2020-01-03 2020-01-03 Combined stator and spindle for a ducted rotor

Publications (1)

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USD920216S1 true USD920216S1 (en) 2021-05-25

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US29/719,446 Active USD920216S1 (en) 2020-01-03 2020-01-03 Combined stator and spindle for a ducted rotor

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Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4432516A (en) * 1980-04-02 1984-02-21 Muscatell Ralph P Variable airfoil assembly
US5590854A (en) * 1994-11-02 1997-01-07 Shatz; Solomon Movable sheet for laminar flow and deicing
US20130089422A1 (en) * 2010-11-12 2013-04-11 Bell Helicopter Textron Inc. Adaptive twist system for a rotor blade
US20130233976A1 (en) * 2011-11-14 2013-09-12 Israel Aerospace Industries Ltd. Wing and devices therefor
US20160053742A1 (en) * 2014-08-20 2016-02-25 Don Allen Harwood Wing with slipstream turbine
US20180208305A1 (en) * 2016-10-31 2018-07-26 Bell Helicopter Textron Inc. Vertical Takeoff and Landing (VTOL) Aircraft
US20190084664A1 (en) * 2017-09-19 2019-03-21 The Boeing Company Methods and apparatus to align and secure aircraft
US20200017190A1 (en) * 2018-07-12 2020-01-16 Bell Helicopter Textron Inc. Multi-spar wing arrangements
USD887948S1 (en) * 2019-01-03 2020-06-23 Bell Helicopter Textron Inc. Aircraft
US20200239134A1 (en) * 2019-01-25 2020-07-30 Bell Helicopter Textron Inc. Hybrid-electric ducted fan transport
US20200239152A1 (en) * 2019-01-30 2020-07-30 Bell Helicopter Textron Inc. Thermal management system

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4432516A (en) * 1980-04-02 1984-02-21 Muscatell Ralph P Variable airfoil assembly
US5590854A (en) * 1994-11-02 1997-01-07 Shatz; Solomon Movable sheet for laminar flow and deicing
US20130089422A1 (en) * 2010-11-12 2013-04-11 Bell Helicopter Textron Inc. Adaptive twist system for a rotor blade
US20130233976A1 (en) * 2011-11-14 2013-09-12 Israel Aerospace Industries Ltd. Wing and devices therefor
US20160053742A1 (en) * 2014-08-20 2016-02-25 Don Allen Harwood Wing with slipstream turbine
US20180208305A1 (en) * 2016-10-31 2018-07-26 Bell Helicopter Textron Inc. Vertical Takeoff and Landing (VTOL) Aircraft
US20190084664A1 (en) * 2017-09-19 2019-03-21 The Boeing Company Methods and apparatus to align and secure aircraft
US20200017190A1 (en) * 2018-07-12 2020-01-16 Bell Helicopter Textron Inc. Multi-spar wing arrangements
USD887948S1 (en) * 2019-01-03 2020-06-23 Bell Helicopter Textron Inc. Aircraft
US20200239134A1 (en) * 2019-01-25 2020-07-30 Bell Helicopter Textron Inc. Hybrid-electric ducted fan transport
US20200239152A1 (en) * 2019-01-30 2020-07-30 Bell Helicopter Textron Inc. Thermal management system

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