Lock actuation system for aircraft

US10227143B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10227143-B2
Application numberUS-201414303443-A
CountryUS
Kind codeB2
Filing dateJun 12, 2014
Priority dateJun 12, 2014
Publication dateMar 12, 2019
Grant dateMar 12, 2019

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  5. First independent claim

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Abstract

Official abstract text for this publication.

Described herein is a system that includes an actuator with a movable input, a first summing mechanism with an input, a first output, and a second output. The input of the first summing mechanism is movably driven by the movable input of the actuator and the first output of the first summing mechanism is movably coupled to a first actuatable element. The system also includes an end mechanism with an input and a first output. The input of the end mechanism is movably driven by the second output and the first output of the end mechanism is movably coupled to a second actuatable element. The system further includes a sensor that senses a position of the rotational input of the actuator. A status of the first and second actuatable elements is based on a sensed position of the movable input of the actuator.

First claim

Opening claim text (preview).

What is claimed is: 1. A system, comprising: an actuator providing a movable input that drives a beginning of a main driveline; a first summing mechanism that unequally divides an input of the first summing mechanism proportionally between a first output that drives the main driveline, and a second output that drives a beginning of a first branch driveline, in response to differences between a first load and a second load applied respectively to the first output and to the second output, the input of the first summing mechanism being movably driven by the movable input of the actuator and the second output of the first summing mechanism being movably coupled to a first actuatable element at an end of the first branch driveline; an end mechanism at an end of the main driveline, with an input, and a first output, wherein the input of the end mechanism is movably driven by the first output of the first summing mechanism, and the first output of the end mechanism is movably coupled to a second actuatable element at an end of a second branch driveline; a sensor, disposed at a location of the main driveline between the actuator at the beginning of the main driveline and the first summing mechanism, that senses a position of the movable input of the actuator; and a controller that determines a jam status and a disconnect status of the first and second actuatable elements from the sensed position of the movable input of the actuator. 2. The system of claim 1 , further comprising a second summing mechanism with an input movably driven by the first output of the first summing mechanism, a second output coupled to a third actuatable element, and a first output movably coupled to the input of the end mechanism, the input of the end mechanism being movably driven by the first output of the first summing mechanism via the second summing mechanism, wherein the controller determines the status of the third actuatable element based on the sensed position of the input of the first summing mechanism. 3. The system of claim 1 , wherein the end mechanism comprises a second summing mechanism, the input of the end mechanism being an input of the second summing mechanism and the first output of the end mechanism being a first output of the second summing mechanism, wherein the second summing mechanism of the end mechanism further comprises a second output, and wherein the second output of the second summing mechanism is non-movably fixed relative to the input and first output of the second summing mechanism. 4. The system of claim 1 , wherein the movable input is a rotational input, the input of the first summing mechanism is rotatably driven by the rotational input of the actuator, the second output of the first summing mechanism is rotatably coupled to the first actuatable element, the input of the end mechanism is rotatably driven by the first output of the first summing mechanism, the first output of the end mechanism is rotatably coupled to the second actuatable element, the sensor senses an angular position of the rotational input of the actuator, and the controller determines the status of the first and second actuatable elements from a sensed angular position of the rotational input of the actuator. 5. The system of claim 4 , wherein at least one of the first summing mechanism and end mechanism comprises a differential. 6. The system of claim 1 , further comprising first and second latch pin assemblies, wherein each of the first and second actuatable elements comprises a lock of the first and second latch pin assemblies, respectively. 7. The system of claim 6 , wherein each latch pin assembly comprises a latch pin that is actuatable between first and second positions, and wherein the controller determines whether the latch pins of the latch pin assemblies are in the first or second positions based on the status of the locks. 8. The system of claim 1 , wherein the controller determines a first status of at least one of the first and second actuatable elements if the sensed position of the movable input is within a first positional range, and determines a second status of at least one of the first and second actuatable elements if the sensed position of the movable input is within a second positional range outside of the first positional range. 9. The system of claim 1 , further comprising first and second stop pairs, the first stop pair comprising two stops that limit a range-of-motion of the first actuatable element, and the second stop pair comprising two stops that limit a range-of-motion of the second actuatable element. 10. The system of claim 9 , wherein at least one stop of the first and second stop pairs is extendable to limit the range-of-motion of a respective one of the first and second actuatable elements, and retractable to not limit the range-of-motion of the respective one of the first and second actuatable elements. 11. A system, comprising: an actuator providing a rotational input that drives a beginning of a main driveline; a first summing mechanism that unequally divides an input of the first summing mechanism proportionally between a first output and a second output in response to differences between a first load and a second load applied respectively to the first output and to the second output, wherein the input of the first summing mechanism is rotatably driven by the rotational input of the actuator; a driveline mechanism selected from a group consisting of a second summing mechanism and a non-summing mechanism, the driveline mechanism having an input that is rotatably driven by the first output of the first summing mechanism, the driveline mechanism also having an output that rotatably drives a first actuatable element; a sensor, disposed at a location of the main driveline between the actuator at the beginning of the main driveline and the first summing mechanism, that senses an angular position of the rotational input of the actuator; and a controller that determines a jam status and a disconnect status of the first actuatable element from the sensed angular position of the rotational input of the actuator. 12. The system of claim 11 , wherein the second output of the first summing mechanism rotatably drives a second actuatable element, and wherein the controller determines a jam status and a disconnect status of the second actuatable element from the sensed angular position of the rotational input of the actuator. 13. The system of claim 12 , wherein the driveline mechanism selected is the second summing mechanism, the system further comprising a third summing mechanism with an input that is rotatably driven by an output of the second summing mechanism, the third summing mechanism rotatably driving a third actuatable element, and wherein the controller determines a jam status and a disconnect status of the third actuatable element from the sensed angular position of the rotational input of the actuator. 14. The system of claim 12 , wherein the first actuatable element and the second actuatable element are sequentially driven by the driveline mechanism and the first summing mechanism, respectively. 15. The system of claim 12 , further comprising first and second latch pin assemblies each having a latch pin actuatable between an engaged position and a non-engaged position, the latch pins of the first and second latch pin assemblies being co-axial, and wherein each of the first and second actuatable elements comprises a lock of the first and second latch pin assemblies, respectively. 16. The system of claim 11 , further comprising a third summing mechanism rotatably driven by the first summing mec

Assignees

Inventors

Classifications

  • Multiple controlled elements · CPC title

  • Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear · CPC title

  • Folding or collapsing to reduce overall dimensions of aircraft · CPC title

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What does patent US10227143B2 cover?
Described herein is a system that includes an actuator with a movable input, a first summing mechanism with an input, a first output, and a second output. The input of the first summing mechanism is movably driven by the movable input of the actuator and the first output of the first summing mechanism is movably coupled to a first actuatable element. The system also includes an end mechanism wi…
Who is the assignee on this patent?
Boeing Co
What technology area does this patent fall under?
Primary CPC classification B64D45/0005. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Mar 12 2019 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).