A connector assembly for mounting turbomachinery including a link connector to be coupled to a clevis. The clevis includes a pair of arms and an opening that extends therethrough. The link connector includes a first end that includes an elastomer portion that defines an opening. The connector assemb
A connector assembly for mounting turbomachinery including a link connector to be coupled to a clevis. The clevis includes a pair of arms and an opening that extends therethrough. The link connector includes a first end that includes an elastomer portion that defines an opening. The connector assembly further includes a support washer having an opening extending therethrough adjacent the link connector elastomer portion, and a fastener inserted through the clevis opening, the support washer opening, and the link connector elastomer opening to couple the link connector and the support washer to the clevis such that the link connector is coupled between the clevis arms by the fastener, and such that the support washer thermally insulates at least a portion of the link connector elastomer portion. At least a portion of the connector assembly being configured to shear when subjected to a predetermined load such that loading induced to the connector assembly is transmitted through the link connector elastomer portion.
대표청구항▼
A connector assembly for mounting turbomachinery including a link connector to be coupled to a clevis. The clevis includes a pair of arms and an opening that extends therethrough. The link connector includes a first end that includes an elastomer portion that defines an opening. The connector assemb
A connector assembly for mounting turbomachinery including a link connector to be coupled to a clevis. The clevis includes a pair of arms and an opening that extends therethrough. The link connector includes a first end that includes an elastomer portion that defines an opening. The connector assembly further includes a support washer having an opening extending therethrough adjacent the link connector elastomer portion, and a fastener inserted through the clevis opening, the support washer opening, and the link connector elastomer opening to couple the link connector and the support washer to the clevis such that the link connector is coupled between the clevis arms by the fastener, and such that the support washer thermally insulates at least a portion of the link connector elastomer portion. At least a portion of the connector assembly being configured to shear when subjected to a predetermined load such that loading induced to the connector assembly is transmitted through the link connector elastomer portion. tual sheets is a number of sheets or a level of sheets. 12. The method of claim 9, wherein said communicating steps comprise: simultaneously visualizing the maximum physical sheet capacity, the operational sheet capacity, and the measurement. 13. The method of claim 12, wherein the maximum physical sheet capacity, the operational sheet capacity, and the measurement are visualized relative to one another. 14. The method of claim 12, wherein the simultaneously visualizing step comprises: providing a graphical representation which communicates the maximum physical sheet capacity, the operational sheet capacity, and the measurement. 15. The method of claim 14, wherein the simultaneously visualizing step further comprises: providing a numerical readout of the measurement. 16. The method of claim 14, wherein the graphical representation in its entirety represents the maximum physical sheet capacity, said method comprising: visualizing a portion of the graphical representation which represents the operation sheet capacity in a first manner; and, visualizing a remainder of the graphical representation which represents a difference between the maximum physical sheet capacity and the operation sheet capacity in a second manner, said second manner being visibly distinguishable from the first manner. 17. A print engine having a maximum physical sheet capacity and being operable at an operational sheet capacity equal to or less than the maximum physical sheet capacity, said print engine comprising: a marking device which applies marks to sheets of media supplied thereto and outputs the same; a feeding device which supplies the sheets to the marking device; a finishing device which receives the sheets from the marking device; and, a user interface, said user interface including an indicator which communicates to an operator of the print engine: the maximum physical sheet capacity of the print engine; the operational sheet capacity at which the print engine is currently operating; and, a measurement of actual sheets which are at least one of contained in or received in a support device of the print engine, wherein said support device is the feeding device or the finishing device. 18. The print engine of claim 17, wherein said indicator comprises: a display which simultaneously visualizes the maximum physical sheet capacity, the operational sheet capacity, and the measurement relative to one another. 19. The print engine of claim 18, wherein the indicator provides a graphical representation which communicates the maximum physical sheet capacity, the operational sheet capacity, and the measurement. 20. The print engine of claim 19, wherein the graphical representation in its entirety represents the maximum physical sheet capacity and a portion thereof representing the operation sheet capacity is visualized differently from a remainder thereof representing a difference between the maximum physical sheet capacity and the operation sheet capacity.
연구과제 타임라인
LOADING...
LOADING...
LOADING...
LOADING...
LOADING...
이 특허에 인용된 특허 (16)
Seelen Laurence (Cincinnati OH) Joseph Thomas P. (West Chester OH) Spofford Hahn M. (West Chester OH) Orkiszewski Charles S. (Cincinnati OH), Aircraft engine forward mount.
Seelen Laurence (Cincinnati OH) Joseph Thomas P. (West Chester OH) Cencula James E. (Middletown OH) Bellia Donald L. (West Chester OH) Spofford Hahn M. (West Chester OH), Aircraft engine mount.
Spofford, Hahn M.; Wakeman, Thomas G.; Bellia, Donald L.; Joseph, Thomas P.; Wilson, Gregg H.; Cencula, James E.; Tegarden, Frederick W.; Schneider, Michael H., Aircraft engine thrust mount.
Halchak Kenneth L. (Wilmington NC) Schwarz Daniel C. (Hamilton OH) Birmingham Martin L. (West Chester OH), Method for assembling a turbine frame assembly.
Lippmeier William C. (Cincinnati OH) Wilkinson Todd T. (Chester OH) Ausdenmoore Robert M. (Chester OH), Support for a translating nozzle vectoring ring.
Cassagne, Jerome; Deforet, Thomas, Assembly comprising an articulation spindle supported by a clevis and immobilized in translation by a blocking device integrating a double anti-rotation system.
Cassagne, Jerome; Deforet, Thomas, Assembly comprising an articulation spindle supported by a clevis and immobilized in translation by a blocking device integrating a double anti-rotation system.
Godiot, Patrice; Bocoviz, Claude; Somson, Ludovic, Ball-joint mechanism between a clevis and a connecting rod, in particular for control apparatus of a rotorcraft.
Sheridan, William G.; McCune, Michael E.; Schwarz, Frederick M.; Kupratis, Daniel Bernard; Suciu, Gabriel L.; Ackermann, William K.; Husband, Jason, Fundamental gear system architecture.
McCune, Michael E.; Husband, Jason; Schwarz, Frederick M.; Kupratis, Daniel Bernard; Suciu, Gabriel L.; Ackermann, William K., Geared architecture for high speed and small volume fan drive turbine.
McCune, Michael E.; Husband, Jason; Schwarz, Frederick M.; Kupratis, Daniel Bernard; Suciu, Gabriel L.; Ackermann, William K., Geared architecture for high speed and small volume fan drive turbine.
McCune, Michael E.; Husband, Jason; Schwarz, Frederick M.; Kupratis, Daniel Bernard; Suciu, Gabriel L.; Ackermann, William K., Geared architecture for high speed and small volume fan drive turbine.
McCune, Michael E.; Husband, Jason; Schwarz, Frederick M.; Kupratis, Daniel Bernard; Suciu, Gabriel L.; Ackermann, William K., Geared architecture for high speed and small volume fan drive turbine.
Barber, Tim Daniel; Hindle, Timothy; Young, Ken; Davis, Torey, Launch lock assemblies including axial gap amplification devices and spacecraft isolation systems including the same.
Bellabal, Francois Robert; Seize, Guilhem; Vincent, Thomas Alain Christian, Link between the exhaust casing and a structural ring of the fan duct of a jet engine.
Young, Ken; Hindle, Timothy; Barber, Tim Daniel, Mounting systems for structural members, fastening assemblies thereof, and vibration isolation systems including the same.
Mahy, Frederic; Etoile, Gerard; Cortesi, Pierre; Delmon, Pierre; Mas, Jean, Shock absorber in elastomer material for a suspension connecting rod or other connecting component.
Miller, Brandon Wayne; Vondrell, Randy M.; Bradley, Donald Albert; Ertas, Bugra Han, Systems and methods for a gas turbine engine with combined multi-directional gearbox deflection limiters and dampers.
Schneider, Uwe, Tie bar for purposes of connecting equipment fitting of an equipment module, in particular an overhead compartment, to a structure fitting of a fuselage cell structure of an aeronautical vehicle.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.