US2476376A - Screw jack with a reversible motor and safety ejection means - Google Patents

Screw jack with a reversible motor and safety ejection means Download PDF

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Publication number
US2476376A
US2476376A US636A US63648A US2476376A US 2476376 A US2476376 A US 2476376A US 636 A US636 A US 636A US 63648 A US63648 A US 63648A US 2476376 A US2476376 A US 2476376A
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Prior art keywords
screw
jack
tube
rod
casing
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US636A
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Laraque Roland
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L AUXILIAIRE IND SA
L'AUXILIAIRE INDUSTRIELLE SA
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L AUXILIAIRE IND SA
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    • 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/02Undercarriages
    • B64C25/08Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/18Operating mechanisms
    • B64C25/24Operating mechanisms electric
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/02Undercarriages
    • B64C25/08Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/18Operating mechanisms
    • B64C25/26Control or locking systems therefor
    • B64C25/30Control or locking systems therefor emergency actuated
    • 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
    • F16H2025/2062Arrangements for driving the actuator
    • F16H2025/2071Disconnecting drive source from the actuator, e.g. using clutches for release of drive connection during manual control
    • 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
    • Y10T74/18592Auxiliary drive [e.g., fluid piston, etc.] for load

Definitions

  • the present invention has for its object to provide the new article of manufacture formed by a screw jack controlled by a reversible motor and provided with a safety device acting in a given direction of actuation (ejection of the jack-rod), said device being adapted.- to be actuated through a simple and fast actuating operation, in the event of non-operation or a check in the operation occurring for any reason and at any point of the stroke in said direction, of the motor which normally provides for such operation (such as an electric motor)
  • a jack of the above character is applicable, by way of example and not oflimitation, in connection with the retracting operation of an aircraft-undercarriage or landing gear which is normally effected, both for retracting and projecting the undercarriage, through the rotation of a reversible motor, and for which it is desired to avert the consequences arising from an impossibility of projecting the undercarriage in a normal manner at a desired time.
  • a detent percussion memer having a spring normally retained under tension, andthe release of which is operative to open the check valve of a tank containing a pressure fluid. This fluid, through a conduct, 11-. necting it with the jack,
  • Fig. 1 is a fragmentary longitudinal cross-section showing the drive portion and the safety ejection device for the rod. of the jack forming the subject of this invention.
  • Fig. 2 shows in fragmentary longitudinal cross-section the portion of the jack to which attached the retractable undercarriage.
  • F 3 is a fragmentary longitudinal cross-seetion on. line III-III 015 Fig. 2,
  • g. 4 is a cross-section showing the position occupied by certain elements of the jack; after admission of the pressure fluid into the safety device.
  • Fig. 5v shows the position occupied by said elements after the screW-and-nut assembly has been released from rigid connection with the engine controlled drive device.
  • Fig. 6 diagrammatically illustrates the jack in ejected position when the normal control device is being used.
  • Fig. '7 is a' diagram illustrating the jack in ejected position when thesafety device is being used.
  • Fig. 1 there has been illustrated the means used to drive the jack in its normal operation.
  • the drive is transmitted from a reversible motor I through a couple-limiting clutch means 2 (diagrammatically indicated in the drawing) to a speed reducing gearing controlled as, follows: the drive portion of the clutch 2 is rigid with the shaft 3 journalled in appropriate anti-friction bearings 4 mounted in the casing 5.
  • Said shaft has secured thereon a pinion 6 meshing with the larger diameter portion of a gear I provided with two sets of teeth, said gear being fitted with appropriate anti-friction bearings 8 supported on the fixed shaft 9 rigid with the casing 5.
  • the smaller diameter portion of the dual-toothed gear 1 meshes with a toothed gear l0 secured on a bushing H which rotates in appropriate anti-friction bearings 12 and I3 supported in the casing 5.
  • the bushing l I terminates in a cylindrical portion i l of enlarged diameter, the end face of which is adapted to engage through a claw-clutch means l5, the head iii of the jack-screw I! which is supported at one of its ends by its nut l8, and at the opposite end in a suitable bearing l9 (see Fig. 2).
  • said eye lindrical portion is formed with one or more recesses 20 the bottom or end-wall of which is formed by the periphery of a hollow piston 21 axially slidable within the cylindrical portion l4 of the bushing II but maintained in normal operative position of the device by means of a bias-.- ing spring 22; said spring engages at one end the end wall of the hollow piston 21 and at its other end the end wall of the cylindrical portion IA of the bushing I I.
  • each of said recesses 20 is arranged a ball 3 en a ing said recess so as to be more than 3 half embedded therein and which rests against the peripheral surface of the hollow piston 2i (Fig. 1).
  • the ball is retained in its recess (irrespective of the attitude of the aircraft in flight) by means of a retaining socket 24.
  • the other portion of the ball 23 engages the bottom of an annular groove 25 of trapezoidal cross-section formed in the head I 6 of the screw I I.
  • the above-described ball-and-groove locking device acts to prevent any lateral displacement of of the screw I! together with the interiorly threaded member 58 which controls the helical movement of the screw II through the'agency of the clutch claws I5, the head It of the screw I1 with the end face of the cylindrical portion [4 of the bushing II.
  • the nut I8 is blocked against rotation through a telescopic tube 26 with which it is rigidly connected, said tube in turn being made rigid with the tubular extension 21 (see Figs. 2 and 3) of a fork member 28 through a pin 29 on'which is mounted a key 30 for sliding displacement in a slot 3i formed in said tubular extension 27.
  • the fork 28 carries a pin 32 (a screw-threaded end of which is provided with a nut 83) which makes is possible to immobilize the pin 34 to which is attached the retractable undercarriage, not shown.
  • the just described assembly thus provides a universal or Cardan joint.
  • the casing 5 is extended on the side of the telescopic tube 26 by a guiding tube 35 terminating in a bearing or journal housing 36.
  • the casing 5 is at its opposite end pivoted through a universal joint to the body of the aircraft through the use of a pivotal fork 31.
  • the reversible rho-- tor l transmits its drive through a reducing gearing and through the bushing III4 to the screw H which then shifts its nut I8 along the tube 25.
  • Said nut in its displacement carries With it in either one or the other direction the telescopic tube 26 with which it is rigid.
  • the relative movement between the telescopic tube 26 and the slotted fork element 21 gives rise at the start of each stroke in either direction, to an initial lost motion phase for the tube 26 and the pin 29 rigid therewith, prior to exerting any action upon the undercarriage itself. This lost motion serves to control the levers (not shown herein) which cause the unlatching of the undercarriage when in projected position or the release of the undercarriage when in retracted condition.
  • the telescopic tube 26 causes the retractible undercarriage attached to the jack shaft 34 (see Fig. 6), respectively to be raised when moving in one direction and to be lowered when moving in the opposite direction.
  • the raisin of the undercarriage is shown to be effected upon contraction of the jack and the lowering of the undercarriage upon expansion of the jack.
  • the safety lowering device As may be ascertained from Fig. 1 this device is of highly simple construction and operation and offers a minimum overall size or bulk, since it occupies the central portion of the jack according to the invention.
  • Said safety lowering device is controlled by the hollow piston 2
  • Said hollow piston carries a push rod 39 which at its opposite end extends through an extension 40 of the factelescopic tube, the fork member ing 5, slightly projecting outwardly thereof.
  • the push-rod 39 is separated from the extension 43 of the casing 5 by an annular duct or channel 4 I.
  • a cap 42 threadedly engaging the extension 40 of the casing 5 protects from any extraneous action the end of the push-rod 39 (projecting out of the casing 5) and seals the end of the annular duct 4
  • a certain amount of clearance is provided between the central portion of the push-rod 39 and the internal portion of the bush H, so as thereby to define a sort of annular channel 43.
  • is peripherally formed with an annular groove 45 of trapezoidal cross-section.
  • a screw-threaded aperture 46 adapted to receive for instance the threaded connection of the flexible pipe communicating with the above-mentioned pressure fluid tank.
  • Rotary joints 4! and 48 mounted on the bushing I I and the cylindrical portion I4 as well as the slidable joint 49 provided on the nut I8 ensure fluid-tightness of the device.
  • the chamber of variable volume clefined by the tube 26 and the nut I8, the tube 35 and the bearing 36 serves as a pneumatic damper for the safety ejection of the tube, through the provision of the tight seals 49 (on the nut I3) and 52 (on the bearing 26), as well as the vent outlets 53 formed in the bearing 36 and which if desired may be provided adjustable through screws or loaded by an adjustable spring-biassed checkvalve, not shown herein.
  • the percussion member of the safety tank is first cocked, the effect of this being to allow the check valve of the tank to drop back upon its seating and to vent the jack to atmosphere. Then the undercarriage and the jack are disconnected.
  • Thetelescopid tube 26 is then reinserted into the tube 35 after having pressed the push-rod- 39; in the first pl-aceso asto uncover the port fifi and thuszto -al-low' escape ofthefluid from tube 35; and in the'second placeto allow the balls: 23.-.
  • the jack according to the invention couldbe applied to the control of a device other thanv a retractable aircraft undercarriage.
  • a screw-jack device comprising'in combination a casinghaving an-elongated tubular portion, a tube telescopabl'e within said tubular portion in coaxial spaced relationtherewith slidable in the outer end'of' saidtubular portion; a structure to be-operatedby said device-attached to the outerendof said'tube, a-nut member at the inner end of said tubenon-rotatably sealingly slidable in saidtubu-larportion, a screw-rod engaging said nut and extending in coaxial relation with both said tubular portion and said tube, said screwrod when rotated causing said nut-and-tube assembly to move axially between a retracted and a projected position with respect to said casing, a reversible power-means outside said tubular casing, a drive connection extending from said power-means'to a drive member in said casing opposite the inner end of said screw-rod, co-operating clutch means in said drive member and in said inner end of said inner end
  • a screw-jack device as claimed in claim I wherein said drive-member has a cavity with cylindrical walls directed towards said screwrod, said screw-rod has a cavity with cylindrical walls directed towardssaid member adapted to surround said first-mentioned cylindrical walls; annularly arranged clutch teeth at the endof said walls of said member and complementary clutch-teeth in the-bottom'of said cavity in said head-, adapted to c'o-operate in rotational driving engagement witheach other when saidscrewrod is in said normal retracted position, circumferentially-spaced recesses in theinner peripheral surface of said' cylindricalwall's of said screw-head and correspondingly-arranged apertures throughsaid cylindrical walls of said member, a latching ball adapted to be seated partly in each of said recesses and partly in the related aperture in saidnormal retracted position of said screw-rod;- apiston sea-lingly slid able in said cavity of said member between a retracted latching position and a projected unlatching position with respect there
  • a screw-jack device comprising in combination a casing having an elongated tubular portion, a tube telescopable within said portion in coaxial spaced relationship therewith slidably sealed in the outer end of said portion, a structure to be operated by said device attached to the outer end of said tube, a nut member at the inner end of said tube sealingly non-rotatably slidable in said tubular portion, and defining with the inner end of said casing a sealed enclosure, a screw-rod engaging said nut and extending coaxially to said tubular portion and said tube, a reversible power-means outside said casing, a drive member in said casing opposite the inner end of said rod and a drive connection extending from said power-means to said drivemember, a cavity with a cylindrical wall extending from said member towards said rod and a cavity with a cylindrical wall extending from the inner end of said rod towards said member surrounding said first caVity-Wall, clutch-teeth on the end of said first cavity-wall and clutch
  • a push-rod extending from said piston axially and projecting from out of said casing to allow said piston to be manually actuated after said piston has operated in an emergency, both to uncover said port and thus allow the fluid in said enclosure to be vented, and to allow retraction of said balls to thus enable said screw to return to the normal retracted position thereof.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Transmission Devices (AREA)

Description

July 19, 1949. R. LARAQUE SCREW 'JACK WITH A REVERSIBLE MOTOR AND SAFETY EJECTION MEANS Filed Jan. 5, 1948 4 Sheets-Sheet l July 19, 1949. LARAQUE 7 2,476,376
SCREW JACK WITH A REVERSIBLE MOTOR AND SAFETY EJECTIONMEANS Filed Jan. 5, 1948 4 Sheets-Sheet 2 July 19, 1949. R. LARAQUE 2,476,376
scREw JACK WITH A REVERSIBLE MOTOR AND SAFETY EJECTION MEANS Filed Jan. 5,1948 4 Sheets-Sheet 5 r LO R. LARAQUE SCREW JACK WITH A REVERSIBL July 19, 1949.
E MOTOR AND SAFETY EJECTION MEANS Filed Jan. 5, 1948 4 Sheets-Sheet 4 Patented July 19, 1949 SCREW JACK WITH A REVERS'IBLEMOTOR ANDSAFETY EJEGTION MEAN S1 Roland Laraque, Paris, France, assignor to Societe An'onyrne LAuxiliaire Industrielle', Paris,
France, a corporation of France Application January 5, 1948, Serial No. 63.6 In France August; 9., 1.947
8 Claims.
The present invention has for its object to provide the new article of manufacture formed by a screw jack controlled by a reversible motor and provided with a safety device acting in a given direction of actuation (ejection of the jack-rod), said device being adapted.- to be actuated through a simple and fast actuating operation, in the event of non-operation or a check in the operation occurring for any reason and at any point of the stroke in said direction, of the motor which normally provides for such operation (such as an electric motor) A jack of the above character is applicable, by way of example and not oflimitation, in connection with the retracting operation of an aircraft-undercarriage or landing gear which is normally effected, both for retracting and projecting the undercarriage, through the rotation of a reversible motor, and for which it is desired to avert the consequences arising from an impossibility of projecting the undercarriage in a normal manner at a desired time.
To actuate said safety device, it is simply necessary to release, under the action of a very slight actuating stress, a detent percussion memer, having a spring normally retained under tension, andthe release of which is operative to open the check valve of a tank containing a pressure fluid. This fluid, through a conduct, 11-. necting it with the jack,
then penetrates into the safety device, first uncouples the rigid connection between the control screw and the drive system connected with the motor, then directly acts upon the screw-and-nut assembly of the jack causing this assembly to move in the manner of a piston within its cylinder and causing ac.- cordingly an ejection of the rod :and also, in the exemplary application mentioned above, the ejection of the undercarriage rigidly coupled with the end of said assembly.
Further characteristics and features of the in! vention wil1 appear from the ensuing disclosure relating to a preferred embodiment of the re versible motor and safety ejection jack, illustrated by way of indication and not of limitation in the accompanying drawing wherein:
Fig. 1 is a fragmentary longitudinal cross-section showing the drive portion and the safety ejection device for the rod. of the jack forming the subject of this invention.
Fig. 2 shows in fragmentary longitudinal cross-section the portion of the jack to which attached the retractable undercarriage.
F 3 is a fragmentary longitudinal cross-seetion on. line III-III 015 Fig. 2,
g. 4 is a cross-section showing the position occupied by certain elements of the jack; after admission of the pressure fluid into the safety device.
Fig. 5v shows the position occupied by said elements after the screW-and-nut assembly has been released from rigid connection with the engine controlled drive device.
Fig. 6 diagrammatically illustrates the jack in ejected position when the normal control device is being used.
Fig. '7 is a' diagram illustrating the jack in ejected position when thesafety device is being used.
In Fig. 1 there has been illustrated the means used to drive the jack in its normal operation. In this case, the drive is transmitted from a reversible motor I through a couple-limiting clutch means 2 (diagrammatically indicated in the drawing) to a speed reducing gearing controlled as, follows: the drive portion of the clutch 2 is rigid with the shaft 3 journalled in appropriate anti-friction bearings 4 mounted in the casing 5.. Said shaft has secured thereon a pinion 6 meshing with the larger diameter portion of a gear I provided with two sets of teeth, said gear being fitted with appropriate anti-friction bearings 8 supported on the fixed shaft 9 rigid with the casing 5. The smaller diameter portion of the dual-toothed gear 1 meshes with a toothed gear l0 secured on a bushing H which rotates in appropriate anti-friction bearings 12 and I3 supported in the casing 5.
The bushing l I terminates in a cylindrical portion i l of enlarged diameter, the end face of which is adapted to engage through a claw-clutch means l5, the head iii of the jack-screw I! which is supported at one of its ends by its nut l8, and at the opposite end in a suitable bearing l9 (see Fig. 2).
In order to prevent the head I6 of the jack screw H from becoming uncoupled from the cylindrical portion 14 of the bushing H, said eye lindrical portion is formed with one or more recesses 20 the bottom or end-wall of which is formed by the periphery of a hollow piston 21 axially slidable within the cylindrical portion l4 of the bushing II but maintained in normal operative position of the device by means of a bias-.- ing spring 22; said spring engages at one end the end wall of the hollow piston 21 and at its other end the end wall of the cylindrical portion IA of the bushing I I.
In each of said recesses 20 is arranged a ball 3 en a ing said recess so as to be more than 3 half embedded therein and which rests against the peripheral surface of the hollow piston 2i (Fig. 1). The ball is retained in its recess (irrespective of the attitude of the aircraft in flight) by means of a retaining socket 24. The other portion of the ball 23 engages the bottom of an annular groove 25 of trapezoidal cross-section formed in the head I 6 of the screw I I. The above-described ball-and-groove locking device acts to prevent any lateral displacement of of the screw I! together with the interiorly threaded member 58 which controls the helical movement of the screw II through the'agency of the clutch claws I5, the head It of the screw I1 with the end face of the cylindrical portion [4 of the bushing II.
The nut I8 is blocked against rotation through a telescopic tube 26 with which it is rigidly connected, said tube in turn being made rigid with the tubular extension 21 (see Figs. 2 and 3) of a fork member 28 through a pin 29 on'which is mounted a key 30 for sliding displacement in a slot 3i formed in said tubular extension 27. The fork 28 carries a pin 32 (a screw-threaded end of which is provided with a nut 83) which makes is possible to immobilize the pin 34 to which is attached the retractable undercarriage, not shown. The just described assembly thus provides a universal or Cardan joint. On the other hand the casing 5 is extended on the side of the telescopic tube 26 by a guiding tube 35 terminating in a bearing or journal housing 36. The casing 5 is at its opposite end pivoted through a universal joint to the body of the aircraft through the use of a pivotal fork 31.
In normal operation of the screw jack forming the subject of this invention, the reversible rho-- tor l transmits its drive through a reducing gearing and through the bushing III4 to the screw H which then shifts its nut I8 along the tube 25. Said nut in its displacement carries With it in either one or the other direction the telescopic tube 26 with which it is rigid. The relative movement between the telescopic tube 26 and the slotted fork element 21 gives rise at the start of each stroke in either direction, to an initial lost motion phase for the tube 26 and the pin 29 rigid therewith, prior to exerting any action upon the undercarriage itself. This lost motion serves to control the levers (not shown herein) which cause the unlatching of the undercarriage when in projected position or the release of the undercarriage when in retracted condition.
After the key 30 has engaged either one of the end walls of the slot 3I, the telescopic tube 26 causes the retractible undercarriage attached to the jack shaft 34 (see Fig. 6), respectively to be raised when moving in one direction and to be lowered when moving in the opposite direction. In the accompanying drawing the raisin of the undercarriage is shown to be effected upon contraction of the jack and the lowering of the undercarriage upon expansion of the jack.
Within the jack driving device which has just been described is accommodated the safety lowering device. As may be ascertained from Fig. 1 this device is of highly simple construction and operation and offers a minimum overall size or bulk, since it occupies the central portion of the jack according to the invention. Said safety lowering device is controlled by the hollow piston 2| mentioned above and on the face of which initially acts the pressure medium. Said hollow piston carries a push rod 39 which at its opposite end extends through an extension 40 of the factelescopic tube, the fork member ing 5, slightly projecting outwardly thereof. The push-rod 39 is separated from the extension 43 of the casing 5 by an annular duct or channel 4 I. A cap 42 threadedly engaging the extension 40 of the casing 5 protects from any extraneous action the end of the push-rod 39 (projecting out of the casing 5) and seals the end of the annular duct 4|. A certain amount of clearance is provided between the central portion of the push-rod 39 and the internal portion of the bush H, so as thereby to define a sort of annular channel 43. There is similarly provided at 44 a certain spacing between the end face of the bush II and the casing 5, for purposes to be described later. The hollow piston 2| is peripherally formed with an annular groove 45 of trapezoidal cross-section.
There is formed in the casing 5 a screw-threaded aperture 46 adapted to receive for instance the threaded connection of the flexible pipe communicating with the above-mentioned pressure fluid tank.
Rotary joints 4! and 48 mounted on the bushing I I and the cylindrical portion I4 as well as the slidable joint 49 provided on the nut I8 ensure fluid-tightness of the device.
Finally, the chamber of variable volume clefined by the tube 26 and the nut I8, the tube 35 and the bearing 36, serves as a pneumatic damper for the safety ejection of the tube, through the provision of the tight seals 49 (on the nut I3) and 52 (on the bearing 26), as well as the vent outlets 53 formed in the bearing 36 and which if desired may be provided adjustable through screws or loaded by an adjustable spring-biassed checkvalve, not shown herein.
Should for any reason and at any point of its downward (jack expanding) stroke, the motor I break down, or should for any accidental cause such as an abnormally tough area, the reaction be greater than the maximum permissible sliding value for the stress-limiting clutch 2, the pilot would then release the percussion member of the safety tank. The pressure medium flows into the safety device, the result of this being to displace the hollow piston 2| until it engages the end face of the cylindrical portion I4 (Fig. 4) while compressing its spring 22, blocking it by pressure action in its new position and uncovering the port 50 formed in the cylindrical portion I4 of enlarged diameter in the bushing II, and through which the pressure fluid penetrates into the expansion chamber 5!. Under the effect of the pressure exerted by the nut I 8, the balls 23 are projected into the annular groove 45 and release the head I6 of the screw I1, which is thus disconnected from the cylindrical portion I4 of the bush II. The fluid pressure continuing to further act upon the surface of the nut I8, pushes the nut I8 and the screw I1 through the tube 35, after the manner of a piston in its cylinder (see Figs. 5 and '7). The nut and its screw in turn carry with them in their displacement, through the agency of the 28 (see Figs. 2 and 3) with which the retractible undercarriage (not shown) is rigid, thus enabling the latter to be lowered.
After landing has been effected, in order to recondition or recock the safety device of the jack according to the invention, the percussion member of the safety tank is first cocked, the effect of this being to allow the check valve of the tank to drop back upon its seating and to vent the jack to atmosphere. Then the undercarriage and the jack are disconnected. For
camera this purpose it is necessary to extract the pin 32 from:- the fork: 28hy loosening theanllt 33 (see Figs. 2 and: 3): therrvthe capi 42i's .un-.: screwed (Fig. 1-)-. Since pressure :iszreli'eved from the face. of the hollow piston 2t" the latter will have been restored to its. initial position (as shown in Fig. I) by the action of the biasing spring 22. Thetelescopid tube 26 is then reinserted into the tube 35 after having pressed the push-rod- 39; in the first pl-aceso asto uncover the port fifi and thuszto -al-low' escape ofthefluid from tube 35; and in the'second placeto allow the balls: 23.-. to be retracted so as to enable the head- It of the screw Hi to return to'its' place; After the annular groove 25 0f the head 16* comes i ntoregister with the recesses 2-0 for the balls 23; the application of pressure is discontinued on the push-rod 39-; the'balls 2'3-then rideup alongthe cam-surf ace of the annular "groove 45, and, while thus retnrni-ngtotheir place, they'latchingl'yconnect the head [B -of thescrew H'- with the engine controlled driving device. The safety deviceis then: cocked and in a condition toresume its iii-notion;
It will of course be understood that the exernplary embodiment described above and illustrated in the accompanying drawings is given merely by way of indication and not of limitation, and it maybe possibleto provide any modiflcations in the jack with a safetyrod-ejecting device according to theinvention, and to replace therein certain elements" by equivalent ones without departing from thespirit' of the invention.
Thus for} example the jack according to the invention couldbe applied to the control of a device other thanv a retractable aircraft undercarriage.
': What: is: claimed is:
l. A screw-jack device comprising'in combination a casinghaving an-elongated tubular portion, a tube telescopabl'e within said tubular portion in coaxial spaced relationtherewith slidable in the outer end'of' saidtubular portion; a structure to be-operatedby said device-attached to the outerendof said'tube, a-nut member at the inner end of said tubenon-rotatably sealingly slidable in saidtubu-larportion, a screw-rod engaging said nut and extending in coaxial relation with both said tubular portion and said tube, said screwrod when rotated causing said nut-and-tube assembly to move axially between a retracted and a projected position with respect to said casing, a reversible power-means outside said tubular casing, a drive connection extending from said power-means'to a drive member in said casing opposite the inner end of said screw-rod, co-operating clutch means in said drive member and in said inner end of said rod adapted to drivingly couple said rod and said member in rotation when said rod is in said retracted condition, means to latch and unlatch said member and said inner end of said rod with respect to each other when so coupled, pressure-fluid actuated means in said tubular casing, means to admit pressure fluid from an external source to one side of said lastmentioned means, said means being operative, when so actuated, to first unlatch said drive-coupling between said rod and said member and then to cause said fluid pressure to act upon said nut to impart a bodily axial displacement to said nutand-tube assembly together with said screw-rod from said retracted to said projected position thereof, thereby operating said structure accordingly.
2. A screw-jack device as claimed in claim 1 6 wherein said latching: means comprises in combination: a head at thei-inner end-Jr of said screw; a pair of complementary generally interesting cylindrical surfaces in: said; drive member and said head. respectively; circumferentially spaced recesses in the outer one of? said surfacesand correspondingly disposed-L apertures through the inner one of. said surfaces, and alatching ball adapted tobe. housed partly in each: one of said recesses and partly in -the-related aperture, said pressure actuated means'being' operative, when unactuated, to retain: said balls in such position and when actuated, to allow said balls-to drop through said apertures completely out of the related recesses;
3. A screw-jack device as claimed in claim I wherein said drive-member has a cavity with cylindrical walls directed towards said screwrod, said screw-rod has a cavity with cylindrical walls directed towardssaid member adapted to surround said first-mentioned cylindrical walls; annularly arranged clutch teeth at the endof said walls of said member and complementary clutch-teeth in the-bottom'of said cavity in said head-, adapted to c'o-operate in rotational driving engagement witheach other when saidscrewrod is in said normal retracted position, circumferentially-spaced recesses in theinner peripheral surface of said' cylindricalwall's of said screw-head and correspondingly-arranged apertures throughsaid cylindrical walls of said member, a latching ball adapted to be seated partly in each of said recesses and partly in the related aperture in saidnormal retracted position of said screw-rod;- apiston sea-lingly slid able in said cavity of said member between a retracted latching position and a projected unlatching position with respect thereto, and having a peripheral-annular groove arranged'to'regrister with said annular apertures only for said projected position of said piston to then allow said balls to drop into said groove, spring-means urging said piston to said retracted position thereof, and said pressure-fluid when admitted urging said piston towards said projected unlatching position thereof.
4; Ina-screw-jack'device as claimed in claim 1 wherein the innersurfa'ce of said' nut defines a fluid-tight enclosure with said casing, a hollow cylindrical portion on said member and a hollow cylindrical portion on the inner end of said screw-rod surrounding said first-mentioned portion, complementary pairs of annularly arranged recesses in the cylindrical walls of said portions respectively and a set of balls each movable between a latching position wherein said ball partly engages each one of said complementary pair of recesses in said cylindrical walls respectively and an unlatching position wherein said ball is retracted out of the recess in said cylindrical wall of said screw-rod cavity, a piston formed with a peripheral groove sealingly slidable in said member cavity, spring means urging said piston to a position wherein said periphery thereof retains said balls in said latching position thereof, means to admit said pressure fluid into the chamber defined between the inner walls of said member cavity and the adjacent side of said piston to thereby urge said piston to an unlatching position wherein said groove therein allows said balls to drop to said retracted condition thereof, a port through the cylindrical wall of said member cavity arranged to be uncovered by said piston when urged to said unlatching position, said port providing communication from said chamber to said enclosure to thereby cause said pressure-fluid to first positively force said balls to said retracted position thereof, and then to drive said nut together with said screw and said tube to said projected position thereof out of said tubular casing.
5. A screw-jack device as in claim 1 wherein said power-means comprises a reversible electric motor secured outside of said tubular casing and said drive connection includes a torquelimiting device on the shaft of said motor and a reducing gearing from said device to said drivemember.
6. A screw-jack device as in claim 1 wherein said tubular casing portion, said nut, said tube and said slidable seal between said tube and said portion define a substantially air-tight enclosure forming a pneumatic damping means for the emergency-projecting movement of said assembly, and an adjustable vent aperture is provided for said enclosure to adjust the damping action thereof.
7. A screw-jack device comprising in combination a casing having an elongated tubular portion, a tube telescopable within said portion in coaxial spaced relationship therewith slidably sealed in the outer end of said portion, a structure to be operated by said device attached to the outer end of said tube, a nut member at the inner end of said tube sealingly non-rotatably slidable in said tubular portion, and defining with the inner end of said casing a sealed enclosure, a screw-rod engaging said nut and extending coaxially to said tubular portion and said tube, a reversible power-means outside said casing, a drive member in said casing opposite the inner end of said rod and a drive connection extending from said power-means to said drivemember, a cavity with a cylindrical wall extending from said member towards said rod and a cavity with a cylindrical wall extending from the inner end of said rod towards said member surrounding said first caVity-Wall, clutch-teeth on the end of said first cavity-wall and clutch-teeth in the end-wall of said second cavity drivingly cooperating therewith when said rod is retracted within said casing for normal operation, annularly-spaced recesses in the inner-cylindrical surface of said second cavity-wall and complementary apertures through said first cavity wall, a ball each adapted when in a latching position, to be partly seated in each of said recesses and partly seated in a related one of said apertures, a piston sealingly slidable in said first cavity defining a chamber with the end-wall thereof, a peripheral groove around said piston, spring means urging said piston to a position wherein the periphery thereof retains said balls in said latching position thereof, a supply of pressure fluid outside said casing, means to admit pressure fluid in an emergency from said supply to said chamber to thereby urge said piston to an unlatching position wherein said groove allows said balls to be retracted from out of said respective recesses, a port through the cylindrical Wall of said first cavity arranged to be uncovered by said piston only as said piston is urged to said unlatching position to provide communication from said chamber through said port to said enclosure, whereby said fiuid acts in said enclosure first to force said balls to said retracted position thereof and then to drive said nut, tube and screw assembly outwardly of said casing.
8. In a screw-jack as claimed in claim 7, a push-rod extending from said piston axially and projecting from out of said casing to allow said piston to be manually actuated after said piston has operated in an emergency, both to uncover said port and thus allow the fluid in said enclosure to be vented, and to allow retraction of said balls to thus enable said screw to return to the normal retracted position thereof.
-ROLAND LARAQUE.
REFERENCES CITED The following references file of this patent:
UNITED STATES PATENTS are of record in the
US636A 1947-08-09 1948-01-05 Screw jack with a reversible motor and safety ejection means Expired - Lifetime US2476376A (en)

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US2660027A (en) * 1952-12-05 1953-11-24 Gen Motors Corp Dual drive actuator
US2660026A (en) * 1952-12-05 1953-11-24 Gen Motors Corp Dual drive actuator
US2688227A (en) * 1952-07-01 1954-09-07 Gen Motors Corp Dual drive actuator
US2810256A (en) * 1954-02-17 1957-10-22 Gen Motors Corp Actuator with electric motor drive and means for controlling the degree of motor energization
US2875980A (en) * 1954-06-25 1959-03-03 Grace Karl Truck raising and supporting mechanism
US2891380A (en) * 1954-09-13 1959-06-23 Gen Motors Corp Dual drive actuator and control means therefor
US2905015A (en) * 1956-11-20 1959-09-22 Buhr Machine Tool Company Lead screw unit
US2949742A (en) * 1957-12-02 1960-08-23 Nat Res Dev Servo-controlled drives
US3031397A (en) * 1958-08-07 1962-04-24 Fortescue Peter Reactor control
US3139721A (en) * 1962-03-16 1964-07-07 Richard P Daubenspeck Canopy actuator and ejector device
US4790201A (en) * 1987-01-21 1988-12-13 Iveco Fiat S.P.A. Electromechanical linear actuator for tipping the driver's cab of a commercial vehicle
US20030233896A1 (en) * 2002-06-24 2003-12-25 Smc Kabushiki Kaisha Electric actuator
US6928894B2 (en) * 2001-02-26 2005-08-16 Societe Eca Compensated actuator with optimized power
US20090044645A1 (en) * 2007-08-14 2009-02-19 Hans-Joachim Buescher Motor driven linear actuator
EP2107273A2 (en) * 2008-04-03 2009-10-07 Goodrich Actuation Systems Limited Actuator
US20090260462A1 (en) * 2008-04-21 2009-10-22 Messier - Bugatti actuator with a main rod and an auxiliary rod
US20100071490A1 (en) * 2008-09-25 2010-03-25 Messier-Bugatti Telescopic actuator with a main rod and an auxiliary rod
ITGE20080085A1 (en) * 2008-10-17 2010-04-18 Ultraflex Control Systems Srl ELECTROMECHANICAL LINEAR ACTUATOR WITH EMERGENCY OPERATION
US20140238168A1 (en) * 2011-11-16 2014-08-28 Ntn Corporation Electric Linear Actuator
US20140245848A1 (en) * 2011-11-11 2014-09-04 Ntn Corporation Electric Linear Actuator
KR20150035812A (en) * 2012-06-04 2015-04-07 에어로 컨트롤렉스 그룹 인코포레이티드 Blow down actuator assembly
EP2896564A1 (en) * 2014-01-21 2015-07-22 CESA, Compania Espanola de Sistemas Aeronauticos, S.A. Linear electromechanical actuator and anti-jamming device
EP2902315A1 (en) * 2014-02-04 2015-08-05 General Atomics Aeronautical Systems, Inc. Landing gear deployment systems and methods
EP3473550A1 (en) * 2017-10-17 2019-04-24 CESA, Compania Espanola de Sistemas Aeronauticos, S.A. Electrical telescopic strut construction
US10683880B2 (en) 2012-06-04 2020-06-16 Aero Controlex Group Inc. Blow down actuator assembly having a drag brake
FR3089950A1 (en) * 2018-12-18 2020-06-19 Safran Landing Systems Method of protection against impacts which may affect an aircraft undercarriage
EP3672868A4 (en) * 2017-08-25 2020-08-26 Marine Canada Acquisition Inc. Electric actuator for a marine steering system

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Cited By (42)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2688227A (en) * 1952-07-01 1954-09-07 Gen Motors Corp Dual drive actuator
US2660027A (en) * 1952-12-05 1953-11-24 Gen Motors Corp Dual drive actuator
US2660026A (en) * 1952-12-05 1953-11-24 Gen Motors Corp Dual drive actuator
US2810256A (en) * 1954-02-17 1957-10-22 Gen Motors Corp Actuator with electric motor drive and means for controlling the degree of motor energization
US2875980A (en) * 1954-06-25 1959-03-03 Grace Karl Truck raising and supporting mechanism
US2891380A (en) * 1954-09-13 1959-06-23 Gen Motors Corp Dual drive actuator and control means therefor
US2905015A (en) * 1956-11-20 1959-09-22 Buhr Machine Tool Company Lead screw unit
US2949742A (en) * 1957-12-02 1960-08-23 Nat Res Dev Servo-controlled drives
US3031397A (en) * 1958-08-07 1962-04-24 Fortescue Peter Reactor control
US3139721A (en) * 1962-03-16 1964-07-07 Richard P Daubenspeck Canopy actuator and ejector device
US4790201A (en) * 1987-01-21 1988-12-13 Iveco Fiat S.P.A. Electromechanical linear actuator for tipping the driver's cab of a commercial vehicle
US6928894B2 (en) * 2001-02-26 2005-08-16 Societe Eca Compensated actuator with optimized power
US20030233896A1 (en) * 2002-06-24 2003-12-25 Smc Kabushiki Kaisha Electric actuator
US7159482B2 (en) * 2002-06-24 2007-01-09 Smc Kabushiki Kaisha Electric actuator
US20090044645A1 (en) * 2007-08-14 2009-02-19 Hans-Joachim Buescher Motor driven linear actuator
EP2107273A3 (en) * 2008-04-03 2011-02-16 Goodrich Actuation Systems Limited Actuator
US20090250552A1 (en) * 2008-04-03 2009-10-08 Goodrich Actuation Systems Limited Actuator
EP2107273A2 (en) * 2008-04-03 2009-10-07 Goodrich Actuation Systems Limited Actuator
US8272285B2 (en) 2008-04-03 2012-09-25 Goodrich Actuation Systems Limited Failsafe actuator
US20090260462A1 (en) * 2008-04-21 2009-10-22 Messier - Bugatti actuator with a main rod and an auxiliary rod
US8286520B2 (en) * 2008-04-21 2012-10-16 Messier-Bugatti-Dowty Actuator with a main rod and an auxiliary rod
US20100071490A1 (en) * 2008-09-25 2010-03-25 Messier-Bugatti Telescopic actuator with a main rod and an auxiliary rod
ITGE20080085A1 (en) * 2008-10-17 2010-04-18 Ultraflex Control Systems Srl ELECTROMECHANICAL LINEAR ACTUATOR WITH EMERGENCY OPERATION
US9353838B2 (en) * 2011-11-11 2016-05-31 Ntn Corporation Electric linear actuator
US20140245848A1 (en) * 2011-11-11 2014-09-04 Ntn Corporation Electric Linear Actuator
US20140238168A1 (en) * 2011-11-16 2014-08-28 Ntn Corporation Electric Linear Actuator
US9631712B2 (en) * 2011-11-16 2017-04-25 Ntn Corporation Electric linear actuator
KR20150035812A (en) * 2012-06-04 2015-04-07 에어로 컨트롤렉스 그룹 인코포레이티드 Blow down actuator assembly
US10920801B2 (en) 2012-06-04 2021-02-16 Aerocontrolex Group Inc. Blow down actuator assembly
US10683880B2 (en) 2012-06-04 2020-06-16 Aero Controlex Group Inc. Blow down actuator assembly having a drag brake
KR102105220B1 (en) 2012-06-04 2020-04-28 에어로 컨트롤렉스 그룹 인코포레이티드 Blow down actuator assembly
US10458442B2 (en) 2012-06-04 2019-10-29 Aero Controlex Group Inc. Blow down actuator assembly
US9845853B2 (en) 2014-01-21 2017-12-19 CESA, Compania Espanola de Sistemas Aeronauticos, S.A. Linear electromechanical actuator and anti-jamming device
EP2896564A1 (en) * 2014-01-21 2015-07-22 CESA, Compania Espanola de Sistemas Aeronauticos, S.A. Linear electromechanical actuator and anti-jamming device
US9988143B2 (en) 2014-02-04 2018-06-05 General Atomics Aeronautical Systems, Inc. Landing gear deployment systems and methods
EP2902315A1 (en) * 2014-02-04 2015-08-05 General Atomics Aeronautical Systems, Inc. Landing gear deployment systems and methods
EP3672868A4 (en) * 2017-08-25 2020-08-26 Marine Canada Acquisition Inc. Electric actuator for a marine steering system
US10981638B2 (en) 2017-08-25 2021-04-20 Marine Canada Acquisition Inc. Electric actuator for a marine steering system
EP3473550A1 (en) * 2017-10-17 2019-04-24 CESA, Compania Espanola de Sistemas Aeronauticos, S.A. Electrical telescopic strut construction
US10837529B2 (en) 2017-10-17 2020-11-17 CESA, Compania Espanola de Sistemas Aeronauticos, S.A. Electrical telescopic strut construction
EP3670964A1 (en) * 2018-12-18 2020-06-24 Safran Landing Systems Method for protecting against impacts that could affect an aircraft landing gear
FR3089950A1 (en) * 2018-12-18 2020-06-19 Safran Landing Systems Method of protection against impacts which may affect an aircraft undercarriage

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