US20040065522A1 - Force-limiting rotary lock - Google Patents

Force-limiting rotary lock Download PDF

Info

Publication number
US20040065522A1
US20040065522A1 US10/266,710 US26671002A US2004065522A1 US 20040065522 A1 US20040065522 A1 US 20040065522A1 US 26671002 A US26671002 A US 26671002A US 2004065522 A1 US2004065522 A1 US 2004065522A1
Authority
US
United States
Prior art keywords
shaft
pawl
housing
angular direction
rotary lock
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.)
Granted
Application number
US10/266,710
Other versions
US6722485B1 (en
Inventor
Seth Gitnes
William House
Kenneth Nakashima
Eric Polcuch
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.)
Moog Inc
Original Assignee
Moog 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 Moog Inc filed Critical Moog Inc
Assigned to MOOG INC. reassignment MOOG INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: HOUSE, WILLIAM H., POLCUCH, ERIC A., GITNES, SETH E., NAKASHIMA, KENNETH K.
Priority to US10/266,710 priority Critical patent/US6722485B1/en
Assigned to HSBC BANK USA, AS AGENT reassignment HSBC BANK USA, AS AGENT SECURITY AGREEMENT Assignors: MOOG INC.
Priority to CA2444404A priority patent/CA2444404C/en
Priority to JP2003383127A priority patent/JP3856785B2/en
Priority to DE60301467T priority patent/DE60301467T2/en
Priority to EP03256303A priority patent/EP1411272B1/en
Priority to ES03256303T priority patent/ES2244898T3/en
Publication of US20040065522A1 publication Critical patent/US20040065522A1/en
Publication of US6722485B1 publication Critical patent/US6722485B1/en
Application granted granted Critical
Adjusted expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H25/00Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms
    • F16H25/18Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms for conveying or interconverting oscillating or reciprocating motions
    • F16H25/20Screw mechanisms
    • F16H25/2021Screw mechanisms with means for avoiding overloading
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00Machine element or mechanism
    • Y10T74/18Mechanical movements
    • Y10T74/18568Reciprocating or oscillating to or from alternating rotary
    • Y10T74/18576Reciprocating or oscillating to or from alternating rotary including screw and nut
    • Y10T74/18704Means to selectively lock or retard screw or nut

Definitions

  • the present invention relates generally to force limiters, and, more particularly, to an improved force-limiting rotary lock that is particularly adapted to be utilized on an aircraft between a driving shaft and one or more airfoil surfaces, such as flaps, slats and the like.
  • flaps are used to redefine the contour of the wing during takeoff and landing.
  • a ball screw actuator is used to drive a rotary shaft that controls movement of a plurality of individual flaps that are spaced along the wing. It is generally desirable to provide a force limiter to prevent damage to the actuator structure in the event that an overload condition is sensed.
  • the present invention provides an improved force-limiting rotary lock ( 20 ) for a shaft ( 21 ) mounted in a housing ( 22 ) for rotational movement about an axis (x-x).
  • the shaft is also axially movable relative to the housing, and is biased (via Belleville spring stacks 33 , 34 ) to move toward a predetermined axial position relative to the housing.
  • the improved rotary lock broadly comprises: at least one member ( 28 ) provided on one of the shaft and housing; a pawl ( 51 ) mounted on the other of the shaft and housing, the pawl being movable relative to the member ( 28 ) between first and second positions; wherein the pawl is operatively arranged to engage the member when the pawl is in the first position (e.g., as shown in FIG. 3) to prevent further rotation of the shaft in one angular direction, and is operatively arranged to be disengaged from the member when the pawl is in the second position (e.g., as shown in FIG.
  • each member ( 28 ) is a lug or dog that extends outwardly from the shaft.
  • such members be they dogs, lugs or otherwise
  • the device is shown as having a single pawl ( 51 ) which is operatively mounted for selective movement between any one of three spring-biased positions: a first position (e.g., as shown in FIG. 3) in which the pawl ( 51 ) engages a member ( 28 ) to prevent rotation of the shaft in one angular direction, a second position (e.g., as shown in FIG. 2) in which the pawl is disengaged from such member and permits rotation of the shaft in either angular direction, and a third position in which the pawl engages a member ( 28 ) and prevents further rotation in the opposite angular direction.
  • a first position e.g., as shown in FIG. 3
  • a second position e.g., as shown in FIG. 2
  • the pawl is disengaged from such member and permits rotation of the shaft in either angular direction
  • a third position in which the pawl engages a member ( 28 ) and prevents further rotation in the opposite angular direction
  • the shaft When the shaft is prevented from rotating in one angular direction, the shaft is not prevented from rotating in the opposite angular direction. Moreover, when the shaft is prevented from rotating in the one angular direction, the pawl is retained in its position independently of the axial position of the shaft. When the pawl is in its first or locked position (i.e., to prevent further rotation in the one angular direction), and the shaft is rotated in the opposite angular direction, even when the shaft is not axially displaced, the pawl will be moved from its locked or first position to its unlocked or second position.
  • the general object of the invention is to provide an improved force-limiting rotary lock.
  • Another object is to provide a force-limiting rotary lock for use in controlling airfoil surfaces, such as flaps, slats and the like.
  • FIG. 1 is a perspective cutaway view of the improved force-limiting rotary lock, this view showing the shaft, the housing, the lug-like members, and the pawl.
  • FIG. 2 is a fragmentary vertical sectional view thereof, taken generally on line 2 - 2 of FIG. 1, showing the pawl as being in its disengaged or second position.
  • FIG. 3 is a view generally similar to FIG. 2, but showing the pawl as having been moved from its unlocked or second position to its first or locked position, and further showing the pawl as operatively engaging one of the lug-like members to prevent further rotation of the shaft in a counterclockwise direction.
  • the terms “horizontal”, “vertical”, “left”, “right”, “up” and “down”, as well as adjectival and adverbial derivatives thereof simply refer to the orientation of the illustrated structure as the particular drawing figure faces the reader.
  • the terms “inwardly” and “outwardly” generally refer to the orientation of a surface relative to its axis of elongation, or axis of rotation, as appropriate.
  • the present invention broadly provides an improved force-limiting rotary lock, of which the presently-preferred embodiment is schematically indicated at 20 .
  • This embodiment broadly includes a horizontally-elongated shaft, generally indicated at 21 , which is operatively mounted within a housing, generally indicated at 22 . More particularly, shaft 21 is mounted for both rotational and axial movement relative to the housing.
  • the shaft is shown as having a generally horizontal axis x-x.
  • the shaft has an external screw thread, schematically indicated at 23 , at its left marginal end portion; a collar portion 24 spaced rightwardly from the screw thread; a plurality of cam members, severally indicated at 25 , extending outwardly from a portion of the shaft; an annular disk-like member 26 provided with four circumferentially-spaced dog- or lug-like members 28 extending radially outwardly therefrom; and a series of splined teeth 29 operatively engaging a mating set of splined teeth on a driving member 30 .
  • Member 30 is arranged-to be rotated about axis x-x by a suitable mechanism (not shown). Because of the splined connection, shaft 21 is constrained to rotate with member 30 , but is permitted to move axially relative to driving member 30 and housing 22 .
  • Screw thread 23 at the left end of the shaft is operatively connected to a screw-and-nut mechanism (not shown) for driving another member or element (not shown).
  • a screw-and-nut mechanism for driving another member or element (not shown).
  • the housing is shown as being a horizontally-elongated specially-configured tubular member that is penetrated by the shaft.
  • the housing has a leftward portion 31 of reduced diameter, and a rightward portion 32 of enlarged diameter.
  • the housing leftward portion 31 has two axially-spaced chambers 33 , 34 separated by an inwardly-extending annular portion 35 .
  • a Belleville spring stack 36 is arranged in left chamber 35
  • another Belleville spring stack 38 is arranged in right chamber 34 .
  • These two Belleville spring stacks act via preload-adjusting shims 39 , 40 on shaft collar portion 24 , and urge the shaft to move toward a predetermined axial position relative to the housing.
  • Shims 39 and 40 are selected to provide the desired preload on the respective springs, and need not be of the same axial thickness. Indeed, they may be of different axial thicknesses, depending on the particular application.
  • the housing enlarged-diameter portion 32 is shown as having (from left to right in FIG. 1): a rightwardly-facing annular vertical wall 41 , an inwardly-facing horizontal cylindrical wall 42 extending rightwardly therefrom, a leftwardly-facing annular vertical surface 43 , an inwardly-facing horizontal cylindrical surface 44 , a rightwardly-facing annular vertical surface 45 , an inwardly-facing horizontal cylindrical surface 46 , and an leftwardly-facing annular vertical surface 48 .
  • the cam members 25 are arranged in two axially-spaced groups of four each, with the cam members of each group being spaced equidistantly about the shaft axis by intervals of about 90 degrees.
  • Disk member 26 is arranged in the housing recess defined between surfaces 45 , 46 and 48 .
  • member 26 is an annular disk-like member from which four lug-like members 28 extend radially outwardly. These four members are spaced equidistantly about the outer cylindrical surface of disk member 26 .
  • Cam follower 49 is mounted on the left marginal end portion of a rod 50 that is pivotally mounted in a hole that extends between housing surfaces 43 and 45 .
  • follower 49 is mounted on one end of rod 50
  • a pawl 51 is mounted on the other end of this rod.
  • follower 49 has a inner portion 52 that is normally arranged to be axially positioned between the axially-spaced cams 25 , 25 .
  • the pawl is a specially-configured member having three concave recesses 53 , 54 and 55 , respectively.
  • a ball 56 is mounted on the housing and is biased by a spring 58 to move toward the pawl and to snap into one of recesses 53 , 54 or 55 .
  • FIGS. 1 - 3 the design shown in FIGS. 1 - 3 is capable of locking the shaft against further rotation in the event of a overload, in either angular direction, with the shaft in all cases being free to be moved in opposite angular direction so as to selectively unlock the mechanism.
  • the invention provides an improved force-limiting rotary lock for a shaft mounted on a housing.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Braking Arrangements (AREA)
  • Chairs For Special Purposes, Such As Reclining Chairs (AREA)
  • Transmission Devices (AREA)
  • Pivots And Pivotal Connections (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)

Abstract

A force-limiting rotary lock (20) for a shaft (21) mounted on a housing (22) for rotational and axial movement relative thereto, broadly includes a lug member (28) provided on the shaft, and a pawl (51) mounted on the housing. The pawl is movable relative to the housing between first and second positions. The pawl is operatively arranged to engage the lug when the pawl is in its first position (shown in FIG. 3) to prevent further rotation of the shaft in one angular direction, and to be disengaged from the lug when the pawl is in its second position (shown in FIG. 2) to permit rotation of the shaft in either angular direction. A cam (25) is mounted on the shaft, and a follower (49) is mounted on the housing for selectively moving the pawl between the first and second positions when the shaft is axially displaced from its predetermined position. When the shaft is axially displaced from its predetermined position and the pawl engages the lug, the shaft will be prevented from rotating further in the one angular direction.

Description

    TECHNICAL FIELD
  • The present invention relates generally to force limiters, and, more particularly, to an improved force-limiting rotary lock that is particularly adapted to be utilized on an aircraft between a driving shaft and one or more airfoil surfaces, such as flaps, slats and the like. [0001]
  • BACKGROUND ART
  • In fixed wing aircraft, flaps are used to redefine the contour of the wing during takeoff and landing. In some cases, a ball screw actuator is used to drive a rotary shaft that controls movement of a plurality of individual flaps that are spaced along the wing. It is generally desirable to provide a force limiter to prevent damage to the actuator structure in the event that an overload condition is sensed. [0002]
  • Various types of rotary locking mechanisms are shown and described in U.S. patent application Ser. No. 09/778,600, filed Feb. 7, 2001, which is assigned to the assignee of the present application, and in U.S. Pat. Nos. 6,109,415, 4,697,672, 4,579, 201, 3,898,817 and 5,582,390. The aggregate disclosures of this application and these patents are hereby incorporated by reference. [0003]
  • DISCLOSURE OF THE INVENTION
  • With parenthetical reference to the corresponding parts, portions or surfaces of the disclosed embodiment, merely for purposes of illustration and not by way of limitation, the present invention provides an improved force-limiting rotary lock ([0004] 20) for a shaft (21) mounted in a housing (22) for rotational movement about an axis (x-x). The shaft is also axially movable relative to the housing, and is biased (via Belleville spring stacks 33, 34) to move toward a predetermined axial position relative to the housing. The improved rotary lock broadly comprises: at least one member (28) provided on one of the shaft and housing; a pawl (51) mounted on the other of the shaft and housing, the pawl being movable relative to the member (28) between first and second positions; wherein the pawl is operatively arranged to engage the member when the pawl is in the first position (e.g., as shown in FIG. 3) to prevent further rotation of the shaft in one angular direction, and is operatively arranged to be disengaged from the member when the pawl is in the second position (e.g., as shown in FIG. 2) to permit rotation of the shaft in either angular direction; a cam (25) mounted on one of the shaft and housing; a follower (49) associated with the pawl for selectively moving the pawl between the first and second positions, and operatively arranged to engage the cam when the shaft is axially displaced from the predetermined position such that when the shaft is axially displaced from the predetermined position and the pawl (51) engages the member (28), the shaft will be prevented from rotating further in the one angular direction.
  • In the illustrated embodiment, each member ([0005] 28) is a lug or dog that extends outwardly from the shaft. However, in an alternative arrangement, such members (be they dogs, lugs or otherwise) could be mounted on the housing.
  • Also, in the preferred embodiment, the device is shown as having a single pawl ([0006] 51) which is operatively mounted for selective movement between any one of three spring-biased positions: a first position (e.g., as shown in FIG. 3) in which the pawl (51) engages a member (28) to prevent rotation of the shaft in one angular direction, a second position (e.g., as shown in FIG. 2) in which the pawl is disengaged from such member and permits rotation of the shaft in either angular direction, and a third position in which the pawl engages a member (28) and prevents further rotation in the opposite angular direction. However, in an alternative embodiment, multiple pawls could be provided.
  • When the shaft is prevented from rotating in one angular direction, the shaft is not prevented from rotating in the opposite angular direction. Moreover, when the shaft is prevented from rotating in the one angular direction, the pawl is retained in its position independently of the axial position of the shaft. When the pawl is in its first or locked position (i.e., to prevent further rotation in the one angular direction), and the shaft is rotated in the opposite angular direction, even when the shaft is not axially displaced, the pawl will be moved from its locked or first position to its unlocked or second position. [0007]
  • Accordingly, the general object of the invention is to provide an improved force-limiting rotary lock. [0008]
  • Another object is to provide a force-limiting rotary lock for use in controlling airfoil surfaces, such as flaps, slats and the like. [0009]
  • These and other objects and advantages will become apparent from the foregoing and ongoing written specification, the drawings, and the appended claims.[0010]
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIG. 1 is a perspective cutaway view of the improved force-limiting rotary lock, this view showing the shaft, the housing, the lug-like members, and the pawl. [0011]
  • FIG. 2 is a fragmentary vertical sectional view thereof, taken generally on line [0012] 2-2 of FIG. 1, showing the pawl as being in its disengaged or second position.
  • FIG. 3 is a view generally similar to FIG. 2, but showing the pawl as having been moved from its unlocked or second position to its first or locked position, and further showing the pawl as operatively engaging one of the lug-like members to prevent further rotation of the shaft in a counterclockwise direction.[0013]
  • DESCRIPTION OF THE PREFERRED EMBODIMENTS
  • At the outset, it should be clearly understood that like reference numerals are intended to identify the same structural elements, portions or surfaces, consistently throughout the several drawing figures, as such elements, portions or surfaces may be further described or explained by the entire written specification, of which this detailed description is an integral part. Unless otherwise indicated, the drawings are intended to be read (e.g., cross-hatching, arrangement of parts, proportion, degree, etc.) together with the specification, and are to be considered a portion of the entire written description of this invention. As used in the following description, the terms “horizontal”, “vertical”, “left”, “right”, “up” and “down”, as well as adjectival and adverbial derivatives thereof (e.g., “horizontally”, “rightwardly”, “upwardly”, etc.), simply refer to the orientation of the illustrated structure as the particular drawing figure faces the reader. Similarly, the terms “inwardly” and “outwardly” generally refer to the orientation of a surface relative to its axis of elongation, or axis of rotation, as appropriate. [0014]
  • Referring now to the drawings, and, more particularly, to FIG. 1 thereof, the present invention broadly provides an improved force-limiting rotary lock, of which the presently-preferred embodiment is schematically indicated at [0015] 20. This embodiment broadly includes a horizontally-elongated shaft, generally indicated at 21, which is operatively mounted within a housing, generally indicated at 22. More particularly, shaft 21 is mounted for both rotational and axial movement relative to the housing.
  • The shaft is shown as having a generally horizontal axis x-x. The shaft has an external screw thread, schematically indicated at [0016] 23, at its left marginal end portion; a collar portion 24 spaced rightwardly from the screw thread; a plurality of cam members, severally indicated at 25, extending outwardly from a portion of the shaft; an annular disk-like member 26 provided with four circumferentially-spaced dog- or lug-like members 28 extending radially outwardly therefrom; and a series of splined teeth 29 operatively engaging a mating set of splined teeth on a driving member 30. Member 30 is arranged-to be rotated about axis x-x by a suitable mechanism (not shown). Because of the splined connection, shaft 21 is constrained to rotate with member 30, but is permitted to move axially relative to driving member 30 and housing 22.
  • Screw [0017] thread 23 at the left end of the shaft is operatively connected to a screw-and-nut mechanism (not shown) for driving another member or element (not shown). As long as the reaction force from the screw-and-nut mechanism is less than the preload on Belleville springs 36 or 38 (as described in detail below), there will be no discernable axial movement of the shaft relative to the housing. However, should such driven member lock up for any reason, then continued rotation of shaft 21 will produce a reaction force in excess of the preload, and thus cause axial movement of shaft 21 relative to housing 22.
  • The housing is shown as being a horizontally-elongated specially-configured tubular member that is penetrated by the shaft. The housing has a [0018] leftward portion 31 of reduced diameter, and a rightward portion 32 of enlarged diameter. The housing leftward portion 31 has two axially- spaced chambers 33, 34 separated by an inwardly-extending annular portion 35. A Belleville spring stack 36 is arranged in left chamber 35, and another Belleville spring stack 38 is arranged in right chamber 34. These two Belleville spring stacks act via preload-adjusting shims 39, 40 on shaft collar portion 24, and urge the shaft to move toward a predetermined axial position relative to the housing. Shims 39 and 40 are selected to provide the desired preload on the respective springs, and need not be of the same axial thickness. Indeed, they may be of different axial thicknesses, depending on the particular application.
  • The housing enlarged-[0019] diameter portion 32 is shown as having (from left to right in FIG. 1): a rightwardly-facing annular vertical wall 41, an inwardly-facing horizontal cylindrical wall 42 extending rightwardly therefrom, a leftwardly-facing annular vertical surface 43, an inwardly-facing horizontal cylindrical surface 44, a rightwardly-facing annular vertical surface 45, an inwardly-facing horizontal cylindrical surface 46, and an leftwardly-facing annular vertical surface 48. The cam members 25 are arranged in two axially-spaced groups of four each, with the cam members of each group being spaced equidistantly about the shaft axis by intervals of about 90 degrees. Thus, there are a total of eight cam members 25, and these extend outwardly so as to face toward housing surface 44. Disk member 26 is arranged in the housing recess defined between surfaces 45, 46 and 48. As previously indicated, member 26 is an annular disk-like member from which four lug-like members 28 extend radially outwardly. These four members are spaced equidistantly about the outer cylindrical surface of disk member 26.
  • [0020] Cam follower 49 is mounted on the left marginal end portion of a rod 50 that is pivotally mounted in a hole that extends between housing surfaces 43 and 45. Follower 49 is mounted on one end of rod 50, and a pawl 51 is mounted on the other end of this rod. Follower 49 has a inner portion 52 that is normally arranged to be axially positioned between the axially-spaced cams 25, 25. Thus, when the shaft is in its predetermined axial position relative to the housing and driving member 30 is rotated, shaft 21 will rotate and will cause the desired movement of the flap. In other words, during normal operation, the shaft will rotate in response to an input from driving member 30, but will not move axially relative to the housing.
  • However, in the event that the flap drive becomes jammed, such impeded movement of the drive will be transmitted back through [0021] screw thread 23 and will cause axial shifting of shaft 21. As this occurs, the inner end of follower 49 will be engaged by one of the cams 25. Continued rotation of the shaft will cause follower 49 to pivot about the axis of rod 50, and will cause pawl 51 to move from its second or unlocked position (as shown in FIG. 2)to its first or biased locked position (as shown in FIG. 3).
  • As best shown in FIGS. 2 and 3, the pawl is a specially-configured member having three [0022] concave recesses 53, 54 and 55, respectively. A ball 56 is mounted on the housing and is biased by a spring 58 to move toward the pawl and to snap into one of recesses 53, 54 or 55.
  • When the shaft is in its predetermined axial position relative to the housing, normal rotational movement of the shaft does not cause any movement of [0023] pawl 51. Thus, the pawl is normally retained in its unlocked or second position, as shown in FIG. 2. However, should the shaft move in either axial direction, as by a flap being overloaded or locked up and the threaded connection causing axial shifting of the shaft within the housing, follower 49 will engage the cams 25 on the axially-shifted shaft and will pivot the pawl from its unlocked position (shown in FIG. 2) to its alternative locked position (shown in FIG. 3). In this condition, the locked position of the pawl will preclude further rotation of the shaft in the same direction by blocking one of the lugs 28 on disk 26, this being shown as being counter-clockwise in FIG. 3.
  • However, even when locked against further rotation in one angular direction, the shaft is free to rotate in the opposite (i.e., clockwise) angular direction. As this occurs, the advancing lug will then engage the off-center pawl and return it from its locked position back to its normal position. [0024]
  • It should be noted that the design shown in FIGS. [0025] 1-3 is capable of locking the shaft against further rotation in the event of a overload, in either angular direction, with the shaft in all cases being free to be moved in opposite angular direction so as to selectively unlock the mechanism.
  • Thus, the invention provides an improved force-limiting rotary lock for a shaft mounted on a housing. [0026]
  • Modifications [0027]
  • As indicated above, many changes and modifications may be made. For example, the form illustrated in the drawings is intended to be viewed as a schematic. The actual implementation of this schematic may take varied and other forms. While it is presently preferred to use opposed Belleville spring stacks with preload-adjusting shims, other types of centering devices may be used. Similarly, other types of cams and followers may be used. The pawl may be mounted on either the shaft or the housing, with the lugs being mounted on the other of the shaft and housing. Connections other than the splined connection may be substituted therefor. [0028]
  • Therefore, while the presently preferred form of the improved force-limiting rotary lock has been shown and described, and certain changes and modifications thereof discussed, persons skilled in this art will readily appreciate that various additional changes and modifications may be made without departing from the spirit of the invention, as defined and differentiated by the following claims. [0029]

Claims (4)

What is claimed is:
1. A rotary lock for a shaft mounted in a housing for rotational movement about an axis, said shaft being axially movable relative to said housing and being biased to move toward a predetermined axial position, comprising:
at least one member provided on one of said shaft and housing;
a pawl mounted on the other of said shaft and housing, said pawl being movable relative to said other of said shaft and housing between first and second positions;
wherein said pawl is operatively arranged to engage said member when said pawl is in said first position to prevent further rotation of said shaft in one angular direction, and to be disengaged from said member when said pawl is in said second position to permit rotation of said shaft in either angular direction;
a cam mounted on one of said shaft and housing;
a follower operatively arranged to engage said cam as said shaft is rotated when said shaft is axially displaced from said predetermined position to selectively move said pawl between said first and second positions and;
such that when said shaft is axially displaced from said predetermined position and said pawl engages said member, said shaft will be prevented from rotating further in said one angular direction.
2. A rotary lock as set forth in claim 1 wherein, when said shaft is prevented from rotating in said one angular direction, said shaft is not prevented from rotating in the opposite angular direction.
3. A rotary lock as set forth in claim 2 wherein, when said shaft is prevented from rotating in said one angular direction, said pawl is retained in said first position independently of the axial position of said shaft.
4. A rotary lock as set forth in claim 2 wherein, as said shaft is rotated in said opposite angular direction and said shaft is not axially displaced, said pawl will be moved from said first position to said second position.
US10/266,710 2002-10-08 2002-10-08 Force-limiting rotary lock Expired - Lifetime US6722485B1 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
US10/266,710 US6722485B1 (en) 2002-10-08 2002-10-08 Force-limiting rotary lock
CA2444404A CA2444404C (en) 2002-10-08 2003-10-06 Force-limiting rotary lock
ES03256303T ES2244898T3 (en) 2002-10-08 2003-10-07 FORCE LIMIT ROTATING LOCK.
DE60301467T DE60301467T2 (en) 2002-10-08 2003-10-07 Force limiter by blocking a rotary movement
JP2003383127A JP3856785B2 (en) 2002-10-08 2003-10-07 Force-limiting rotary locking device
EP03256303A EP1411272B1 (en) 2002-10-08 2003-10-07 Force-limiting rotary lock

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/266,710 US6722485B1 (en) 2002-10-08 2002-10-08 Force-limiting rotary lock

Publications (2)

Publication Number Publication Date
US20040065522A1 true US20040065522A1 (en) 2004-04-08
US6722485B1 US6722485B1 (en) 2004-04-20

Family

ID=32042711

Family Applications (1)

Application Number Title Priority Date Filing Date
US10/266,710 Expired - Lifetime US6722485B1 (en) 2002-10-08 2002-10-08 Force-limiting rotary lock

Country Status (6)

Country Link
US (1) US6722485B1 (en)
EP (1) EP1411272B1 (en)
JP (1) JP3856785B2 (en)
CA (1) CA2444404C (en)
DE (1) DE60301467T2 (en)
ES (1) ES2244898T3 (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100096152A1 (en) * 2008-10-16 2010-04-22 Top Gearbox Industry Co., Ltd. Lever type output shaft locking device
CN102927093A (en) * 2012-10-23 2013-02-13 中国船舶重工集团公司第七一○研究所 March fixing device with state sampling function
CN104859842A (en) * 2015-06-11 2015-08-26 贵州华烽电器有限公司 Longitudinal angular displacement tooling structure
WO2016115062A1 (en) * 2015-01-13 2016-07-21 Moog Inc. Travel limiting stop module for a rotational drive system
US20160369877A1 (en) * 2015-06-17 2016-12-22 Moog Inc. No-back brake functionality monitor
US20180087637A1 (en) * 2016-09-28 2018-03-29 Linear Transfer Automation Ball screw locking apparatus
US11781625B2 (en) 2019-02-25 2023-10-10 Moog Inc. Single-use non-jamming stop module for rotary drive actuator

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007089275A (en) * 2005-09-21 2007-04-05 Smc Corp Electric cylinder
JP5243018B2 (en) * 2007-12-27 2013-07-24 Ntn株式会社 Electric linear actuator
EP2285673B1 (en) * 2008-06-13 2014-05-21 Moog Inc. Method for determining the apparent operational integrity of a no-back device
US8844389B2 (en) * 2011-12-14 2014-09-30 Woodward Hrt, Inc. Automatically locking linear actuator
GB201121604D0 (en) 2011-12-15 2012-01-25 Airbus Uk Ltd A shaft locking device
JP3186045U (en) * 2013-03-11 2013-09-19 秋夫 松井 The present invention relates to a wedge-shaped biting brake device for an elevator (elevator).
US9470272B2 (en) 2013-07-09 2016-10-18 Moog Inc. Torque limiter responsive to output torque
CN203702759U (en) * 2014-01-20 2014-07-09 思博特有限公司 Portable rotating self-locking type quick-disassembly lock catch device
US10473554B2 (en) * 2016-02-02 2019-11-12 Moog Inc. Gearbox torque measurement system
EP3232078B1 (en) 2016-04-15 2020-06-03 UTC Aerospace Systems Wroclaw Sp. z o.o. No-back device with energy-dispersing springs
CN110422129B (en) * 2019-07-28 2020-05-26 南京视莱尔汽车电子有限公司 Automobile electronic module monitoring system
US11873092B2 (en) * 2020-12-16 2024-01-16 The Boeing Company Trim actuators for horizontal stabilizers and methods of controlling horizontal stabilizers
EP4186788A1 (en) * 2021-11-25 2023-05-31 Goodrich Actuation Systems SAS Electromechanical actuator
EP4209415B1 (en) * 2022-01-06 2024-09-18 Goodrich Actuation Systems SAS Electromechanical actuator

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2393120A (en) * 1943-05-27 1946-01-15 Perman Per Emil Safety device in screw hoisting blocks
US2854113A (en) * 1957-02-06 1958-09-30 Barber Colman Co Actuator and limit means therefor
US3898817A (en) * 1973-02-20 1975-08-12 Lucas Industries Ltd Actuator with a torque limiting device
US4459867A (en) * 1981-12-28 1984-07-17 Sundstrand Corporation Resettable force limiting device
US4579201A (en) * 1983-05-16 1986-04-01 Curtiss Wright Flight Systems, Inc. Bidirectional, torque-limiting, no-back clutch mechanism
US4697672A (en) * 1985-03-25 1987-10-06 Sundstrand Corporation Bi-directional force limiting no-back mechanism
US5582390A (en) * 1994-11-17 1996-12-10 Sundstrand Corporation Drive apparatus with primary and secondary no-back features
US5655636A (en) * 1995-06-02 1997-08-12 Sundstrand Corporation Compact actuator including resettable force limiting and anti-backdrive devices
US6109415A (en) * 1998-05-29 2000-08-29 The Boeing Company Bi-directional ballscrew no-back device
US6467363B2 (en) * 2001-02-07 2002-10-22 Moog Inc. Ball screw actuator locking mechanism

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4318304A (en) * 1980-04-11 1982-03-09 Sundstrand Corporation Force limiting device

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2393120A (en) * 1943-05-27 1946-01-15 Perman Per Emil Safety device in screw hoisting blocks
US2854113A (en) * 1957-02-06 1958-09-30 Barber Colman Co Actuator and limit means therefor
US3898817A (en) * 1973-02-20 1975-08-12 Lucas Industries Ltd Actuator with a torque limiting device
US4459867A (en) * 1981-12-28 1984-07-17 Sundstrand Corporation Resettable force limiting device
US4579201A (en) * 1983-05-16 1986-04-01 Curtiss Wright Flight Systems, Inc. Bidirectional, torque-limiting, no-back clutch mechanism
US4697672A (en) * 1985-03-25 1987-10-06 Sundstrand Corporation Bi-directional force limiting no-back mechanism
US5582390A (en) * 1994-11-17 1996-12-10 Sundstrand Corporation Drive apparatus with primary and secondary no-back features
US5655636A (en) * 1995-06-02 1997-08-12 Sundstrand Corporation Compact actuator including resettable force limiting and anti-backdrive devices
US6109415A (en) * 1998-05-29 2000-08-29 The Boeing Company Bi-directional ballscrew no-back device
US6467363B2 (en) * 2001-02-07 2002-10-22 Moog Inc. Ball screw actuator locking mechanism

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100096152A1 (en) * 2008-10-16 2010-04-22 Top Gearbox Industry Co., Ltd. Lever type output shaft locking device
CN102927093A (en) * 2012-10-23 2013-02-13 中国船舶重工集团公司第七一○研究所 March fixing device with state sampling function
WO2016115062A1 (en) * 2015-01-13 2016-07-21 Moog Inc. Travel limiting stop module for a rotational drive system
US9670999B2 (en) 2015-01-13 2017-06-06 Moog Inc. Low friction travel limiting stop module for a rotational drive system
CN104859842A (en) * 2015-06-11 2015-08-26 贵州华烽电器有限公司 Longitudinal angular displacement tooling structure
US20160369877A1 (en) * 2015-06-17 2016-12-22 Moog Inc. No-back brake functionality monitor
US20180087637A1 (en) * 2016-09-28 2018-03-29 Linear Transfer Automation Ball screw locking apparatus
US10663046B2 (en) * 2016-09-28 2020-05-26 Linear Transfer Automation Ball screw locking apparatus
US11781625B2 (en) 2019-02-25 2023-10-10 Moog Inc. Single-use non-jamming stop module for rotary drive actuator

Also Published As

Publication number Publication date
JP3856785B2 (en) 2006-12-13
DE60301467T2 (en) 2006-01-19
EP1411272A3 (en) 2004-05-06
ES2244898T3 (en) 2005-12-16
EP1411272B1 (en) 2005-08-31
DE60301467D1 (en) 2005-10-06
CA2444404A1 (en) 2004-04-08
JP2004162919A (en) 2004-06-10
EP1411272A2 (en) 2004-04-21
US6722485B1 (en) 2004-04-20
CA2444404C (en) 2011-04-19

Similar Documents

Publication Publication Date Title
US6722485B1 (en) Force-limiting rotary lock
US6202803B1 (en) Output load limiter
US5983743A (en) Actuator assembly
US6467363B2 (en) Ball screw actuator locking mechanism
US5655636A (en) Compact actuator including resettable force limiting and anti-backdrive devices
US5916325A (en) Actuator assembly and torque limiting system for same
JP6244021B2 (en) Torque limiter that can respond to output torque
US6766709B1 (en) Universal gear self-locking/unlocking mechanism
US9863515B2 (en) Self-locking no-back actuator
US4795110A (en) Flight control surface actuation lock system
US20120111993A1 (en) Rotational lock mechanism for actuator
CA2700572C (en) Motorized spindle drive with overload protection
US4628752A (en) Actuators and actuator assemblies
US20140135132A1 (en) Non-chattering ball detent torque limiter
US10859123B2 (en) Torque-limiting device
US6237433B1 (en) Electromechanical actuator of the type having a screw-and-nut system
EP0404772B1 (en) Non-jamming rotary mechanical actuator
US5383818A (en) Overload clutch for limiting a torque moment
EP1321359B1 (en) Differential torque limiter
DE69419144T2 (en) SAFETY DEVICE AGAINST INTERFERENCE FOR FLIGHT CONTROL SYSTEM
US6196361B1 (en) Compact electric asymmetry brake
US9039538B2 (en) Non-chattering ball detent torque limiter
US20060070827A1 (en) Screw actuator
JPS62202217A (en) Overfeed stopper for rotating shaft
US6471028B1 (en) Mechanical module with variable characteristic set by the act of installation

Legal Events

Date Code Title Description
AS Assignment

Owner name: MOOG INC., NEW YORK

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:GITNES, SETH E.;HOUSE, WILLIAM H.;NAKASHIMA, KENNETH K.;AND OTHERS;REEL/FRAME:013375/0858;SIGNING DATES FROM 20020925 TO 20020927

AS Assignment

Owner name: HSBC BANK USA, AS AGENT, NEW YORK

Free format text: SECURITY AGREEMENT;ASSIGNOR:MOOG INC.;REEL/FRAME:013782/0738

Effective date: 20030303

STCF Information on status: patent grant

Free format text: PATENTED CASE

FPAY Fee payment

Year of fee payment: 4

REMI Maintenance fee reminder mailed
FPAY Fee payment

Year of fee payment: 8

FPAY Fee payment

Year of fee payment: 12