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公开(公告)号:US20230265702A1
公开(公告)日:2023-08-24
申请号:US17676537
申请日:2022-02-21
Applicant: Bell Textron Inc.
CPC classification number: E05F5/06 , E05D5/062 , E05D11/1085 , E05Y2900/531
Abstract: Disclosed is an assembly and a vehicle and apparatus including the assembly, for maintaining a vehicle door in an open position may include at least one rod member configured to connect at a first end to the door and at a second end to a vehicle frame. A tab may be connected to and extend in at least one direction from the rod member. A plunger may be configured to be anchored in the door and including a pin configured to extend from and retract into the plunger. The pin may be configured to engage the tab when extended and disengage from the tab when retracted.
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公开(公告)号:US11733714B2
公开(公告)日:2023-08-22
申请号:US17149445
申请日:2021-01-14
Applicant: Bell Textron Inc.
Inventor: Steven G. Hagerott , Jonathan Andrew Toth
CPC classification number: G05D1/0808 , B64C29/0033 , G05D1/0055 , B64C13/503
Abstract: There is disclosed in one example an inner loop controller for an aircraft flight computer, including: a stall protection circuit to compute, for an attitude angle θ, an attitude limit θmax as a function of a flight path angle (γ) and an angle of attack limit (αmax); a transfer function circuit to convert θ to an attitude rate {dot over (θ)}, wherein {dot over (θ)} is a time derivative of θ; and a load protector circuit to compute a limit on {dot over (θ)} ({dot over (θ)}max) as a function of a load factor limit (Nz,max) and a true airspeed (v).
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公开(公告)号:US11732747B2
公开(公告)日:2023-08-22
申请号:US17568820
申请日:2022-01-05
Applicant: Bell Textron Inc.
Inventor: Daniel P. Sottiaux , Marco A. Agredano , Frank B. Stamps
CPC classification number: F16C11/0614 , B64C27/001 , B64C27/39 , F16C27/06 , F16F1/40 , F16C2202/08 , F16C2208/10
Abstract: A laminated elastomeric journal bearing has an outer sleeve having an inner surface, at least a portion of each end of the inner surface being a concave surface of revolution, and an inner sleeve having an outer surface, at least a portion of each end of the outer surface being a convex surface of revolution. Alternating layers of elastomer and metal are located between the sleeves, with adjacent surfaces of the layers and the sleeves being adhered to each other.
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公开(公告)号:US11718397B2
公开(公告)日:2023-08-08
申请号:US17324184
申请日:2021-05-19
Applicant: Bell Textron Inc.
Inventor: Brent C. Ross , Kirk L. Groninga , Steven R. Ivans , Jason Paul Hurst
CPC classification number: B64C29/0033 , B64C13/24 , B64D27/24 , B64D35/04
Abstract: Embodiments include an aircraft comprising a fuselage; a wing connected to the fuselage; and first and second propulsion systems connected to the wing on opposite sides of the fuselage, wherein at least a portion of each of the first and second propulsion systems and at least a portion of the wing are tiltable between a first position in which the aircraft is in a hover mode and a second position in which the aircraft is in a cruise mode, wherein each of the propulsion systems includes pylon and a rotor assembly comprising a plurality of rotor blades.
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公开(公告)号:US11713804B2
公开(公告)日:2023-08-01
申请号:US17307142
申请日:2021-05-04
Applicant: Bell Textron Inc.
Inventor: Eric Stephen Olson , David Bockmiller
IPC: F16H57/04
CPC classification number: F16H57/0427 , F16H57/045 , F16H57/0482
Abstract: An exemplary passive oil system includes a reservoir housing configured in operation to rotate around a rotational axis, the reservoir housing defining a reservoir between a top wall, a bottom wall, innermost side, and an outer sidewall; and an outlet positioned adjacent the outer sidewall to discharge a lubrication fluid contained in the reservoir in response to the reservoir housing rotating around the rotational axis.
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公开(公告)号:US20230213059A1
公开(公告)日:2023-07-06
申请号:US17568820
申请日:2022-01-05
Applicant: Bell Textron Inc.
Inventor: Daniel P. Sottiaux , Marco A. Agredano , Frank B. Stamps
IPC: B64C27/35
CPC classification number: B64C27/35
Abstract: A laminated elastomeric journal bearing has an outer sleeve having an inner surface, at least a portion of each end of the inner surface being a concave surface of revolution, and an inner sleeve having an outer surface, at least a portion of each end of the outer surface being a convex surface of revolution. Alternating layers of elastomer and metal are located between the sleeves, with adjacent surfaces of the layers and the sleeves being adhered to each other.
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公开(公告)号:US11691720B2
公开(公告)日:2023-07-04
申请号:US17029569
申请日:2020-09-23
Applicant: Bell Textron inc.
Inventor: Gerard Michael Schneider , Lawrence Michael Petsch
Abstract: A pitch change link may include a shaft having a first end region and a second end region, and a bearing cartridge on at least one of the first end region and the second end region. The bearing cartridge may include a bearing and a bearing ring at least partially surrounding the bearing. The bearing ring may have a geometric symmetry and a cross section that is wider at a first end than at a second end, the first end may oppose the second end.
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公开(公告)号:US20230202321A1
公开(公告)日:2023-06-29
申请号:US17561900
申请日:2021-12-24
Applicant: Bell Textron Inc.
Inventor: Albert Mazzei , Michael R. Hull , Yue Fan
CPC classification number: B60L53/305 , B64C39/024 , B60L53/66 , B64C2201/042
Abstract: There is disclosed in one example, one or more tangible, non-transitory computer-readable storage media having stored thereon machine-executable instructions to: receive battery data from at least one sensor connected to a battery bank of an electric vertical takeoff and landing (eVTOL) aircraft, wherein the battery bank comprises a plurality of batteries; compute from the battery data an available flight time remaining for the eVTOL aircraft; compute a nominal flight time remaining, wherein the nominal flight time remaining excludes a reserve flight time; and display the nominal flight time remaining to a pilot in a human-readable format.
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公开(公告)号:US11685515B2
公开(公告)日:2023-06-27
申请号:US17069816
申请日:2020-10-13
Applicant: Bell Textron Inc.
Inventor: Luke Dafydd Gillett , James Rigsby , Jeffrey Kirkman , Craig Lovell , Andrew Carter , Aaron Alexander Acee
CPC classification number: B64C13/16 , B64C5/02 , B64C5/16 , B64C27/06 , B64C2027/8281
Abstract: A rotorcraft has a horizontal stabilizer movable about an axis of rotation and a horizontal stabilizer control system configured to control the horizontal stabilizer to at least one of move the rotorcraft into a minimum drag position, maintain the aircraft in a minimum drag position, efficiently achieve a maneuver, enter efficient autorotation, and maintain efficient autorotation.
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公开(公告)号:US11661172B2
公开(公告)日:2023-05-30
申请号:US17139049
申请日:2020-12-31
Applicant: Bell Textron Inc.
Inventor: Robert W. Roe , Mark L. Isaac
CPC classification number: B64C3/32 , B64C29/0033
Abstract: A wing for an aircraft includes a first end, a second end, and a skin extending longitudinally from the first end to the second end. The wing also includes at least one channel positioned within the skin and extending longitudinally between the first and second ends. The at least one channel defines a longitudinal translation path for translating at least one electrical power source longitudinally between the first and second ends.
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