US2935950A - Release mechanism - Google Patents

Release mechanism Download PDF

Info

Publication number
US2935950A
US2935950A US535527A US53552744A US2935950A US 2935950 A US2935950 A US 2935950A US 535527 A US535527 A US 535527A US 53552744 A US53552744 A US 53552744A US 2935950 A US2935950 A US 2935950A
Authority
US
United States
Prior art keywords
rotor
shaft
detent
projectile
mass
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.)
Expired - Lifetime
Application number
US535527A
Inventor
William B Mclean
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to US535527A priority Critical patent/US2935950A/en
Application granted granted Critical
Publication of US2935950A publication Critical patent/US2935950A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C11/00Electric fuzes
    • F42C11/04Electric fuzes with current induction
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K7/00Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
    • H02K7/10Structural association with clutches, brakes, gears, pulleys or mechanical starters
    • H02K7/102Structural association with clutches, brakes, gears, pulleys or mechanical starters with friction brakes
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K7/00Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
    • H02K7/18Structural association of electric generators with mechanical driving motors, e.g. with turbines
    • H02K7/1807Rotary generators
    • H02K7/1823Rotary generators structurally associated with turbines or similar engines

Definitions

  • Another object is to provide agenera'tor lock which, when released, is positively secured in such manner that it cannot again interfere 'with'rotation of the generator rotor.
  • the generator is therefore positively locked until 'the projectile is. fired, andreleased with equal positiveness 4 upon firing.
  • V A 1 4 The invention herein described may be manufactured and used by or for the Government of the United States of America for governmental purposes without the. payment of'any royalties thereon or therefor.
  • Fig. 1 is a' part-sectional diametric elevational view of a generator and a housing therefor, showin'g'my im-' proved setback-operated mechanism-in locked position.
  • Fig. 2 is a view similar to Fig.1 but showing the locking mechanism released.
  • Fig. 3 is a cross section taken substantially on the line 3-3 of Fig. 1, and looking in the direction of the arrows.
  • rotor l' is fastened to shaft 2, which may be driven by any suitable means (not shown but which may comprise a wind-driven impeller).
  • Field coils 3, shown diagrammatically, are mounted in casing 6 in operative relationship to the rotor.
  • Shaft 2 rotates in bearings 4 and 5 fixed in casing 6.
  • Disc 7 is screwed or otherwise fastened to the lower face of rotor 1, and carries pins 8 positioned as best shown in plan in Fig. 3.
  • Pins 8 normally extend downwardly beside arms 9, 12.
  • Arms 9 are integral with a tapped cylindrical hub 10, threaded upon the axial bushing 5 upstanding from the bottom of the casing andwhich forms the lower bearing for the rotor.
  • hub 11 is downwardly slidable on the outside surface of hub 10 and carries arms 12 which normally block pins 8 and therefore prevent rotor 1 from being turned.
  • Arms 12 are vertically slidable between and prevented from rotating byposts 13 fixed to the bottom of casing 6.
  • Compression spring 14 urges the arm and hub assembly 11, 12 upwardly.
  • the generator and its release mechanism are installed in the projectile or other vehicle with the axis of shaft 2 parallel to the line of I. set-back, compressing spring 14. This action brings locking arms 12 below pins 8 which are then rapidly revolved with rotor 1 by the driving means (unshown) attached to shaft 2.
  • the direction of such rotation is ing a detent normally in operative blocking engagement with said rotorbut movable away from” such engagement under the influence of set back, spring means forv urging said detent in such operative blockingengagement, means for holding [said detent out of such' blocking engagement, and means for rotating said rotor rela'tive to said stator substantially immediately upon release of said rotor by said releasable locking means.
  • An electrical generator having rotor and stator means adapted for installation in a projectile or the like, set-back releasable locking means for said rotor including a detent normally in operative blocking engagement v with said rotor but movable away from such engagement under the influence of set-back, means for holding said detent out of such blocking engagement, said electrical generator being adapted for installation in a projectile with the axis of rotation of the rotor substantially parallel to the line of flight of the projectile, said locking means including a spring-held mass movable rearwardly with respect to the direction of flight during set-back, and said holding means including a hold-down nut actuatable by the rotor.
  • An electrical generator having rotor and stator means adapted for installation in a projectile or the like, setback releasable locking means for said rotor including a detent normally in operative blocking engagement with said rotor but movable away from such engagement under the.
  • said generator including a shaft supporting said rotor concentric with said stator means, the said stator means being adapted for installation in a projectile with the shaft substantially parallel to the line of flight of the projectile, said detent including a mass mounted concentrically with respect to and movable longitudinally of the shaft, spring means surrounding the shaft and urging said mass toward the rotor, and interengageable abutment portions carried by 1 said rotor and mass and separable when said detent moves detent normally in operative blocking engagement with said rotor but movable away from such engagement under the influence of set-back, means for holding said detent out of such blocking engagement, said generator including a shaft supporting said rotor concentric with said stator means, the said stator means being adapted for installation in a projectile with the shaft substantially parallel to the line of flight of the projectile, said detent including a mass mounted concentrically with respect to and movable longitudinally of the shaft, spring means surrounding the shaft and
  • An electrical generator having rotor and stator means adapted for installation in a projectile or the like, setback releasable locking means for said rotor including a detent normally in operative blocking engagement with said rotor but movable away from such engagement under the influence of'set back, means for holding said detent out of such blocking engagement, said generator including a shaft supporting said rotor concentric with said stator means, the said stator means being adapted for installation in a projectile with the shaft substantially parallel to the line of flight of the projectile, said detent including a mass mounted concentrically with respect to and movable longitudinally of the shaft, spring means surrounding the shaft and urging said mass toward the rotor, interengageable abutment portions carried by said rotor and mass and separable when said detent moves away, said holding means including a hold-down nut also surrounding said shaft and drivable by the rotor, after release of said locking means, to a position in which it prevents reengagement of said abutment portions
  • An electrical generator having rotor and stator means adapted for installation in a projectile or the like, setback releasable locking means for said rotor including a detent normally in operative blocking engagement with said rotor but movable away from such engagement under the influence of set-back, means for holding said detent out of such blocking engagement, said generator including a shaft supporting said rotor concentric with said stator means, the said stator means being adapted for installation in a projectile with the shaft substantially parallel to the line of flight of the projectile, said detent including a mass mounted concentrically with respect to and movable longitudinally of the shaft, spring means surrounding the shaft and urging said mass toward the rotor, pins projecting longitudinally from the rotor and into driving engagement with said mass, said holding means including a hold-down nut also surrounding said shaft and engageable with and adapted to be driven by said pins, said nut being movable by said pins to a position in which .it prevents reengagement of said mass with the pins.

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Iron Core Of Rotating Electric Machines (AREA)

Description

May 10, 1960 w. B. MCLEAN 2,935,950 7 RELEASE MECHANISM Filed May 13, 1944 WILLIAM B. MGLEAN AORNEY 910 4 2 I3 Fl6.l'
United St T 2,935,950 RELEASE MECHANISM William B. McLeanywashington, l).C.,- assignor to the United States of America as represented by the Secre tary of the Navy "Application'May 13,1944,'SerialNo. 535,527
6 Claims. Cl. 102-701 7 (Granted under Title :35, 'U.S.'C0de (1952), sec. 266) .simple construction,adapted to prevent the rotor from turning until after setback and which cannot be released by accelerations of short duration.
Another object is to provide agenera'tor lock which, when released, is positively secured in such manner that it cannot again interfere 'with'rotation of the generator rotor.
"F65. Pe 9 Patented May 10, 1960,
such as to screw sleeve 10 down on the sleevesi'j The momentum of the nut assembly 9, 10, iniconjufnction with reverse acceleration, is sutficient to insure that arms 9 will be carried below the ends of pins 8. R otor l is thus left free to revolve under the influence of its drivingmeans.
When the setback ceases, arms 1 2 remain fastened their depressed, releasing position, being'held securely against the pressure of spring 14 by'means ofthe nut assembly 9, 10. I I
It is, of course, essential that setback endure art sufficient period to let the propeller turn enough 'revol u- Spin m l o below the pins 8.; Itjhajs been 1 foundthat this action is easily attainable with projectiles and generatordrivingmeans of known varieties. Y
The generator is therefore positively locked until 'the projectile is. fired, andreleased with equal positiveness 4 upon firing. V A 1 4 The invention herein described may be manufactured and used by or for the Government of the United States of America for governmental purposes without the. payment of'any royalties thereon or therefor.
1 claim: I I v 1."An electrical generator having rotor "and stator means adapted for installation in a projectile or thelike,
set-back releasable locking "means for said rotor includ- Other objects will be apparentupon consideration of p 'the 'presentdisclosure in its entirety.
In the drawings: Fig. 1 is a' part-sectional diametric elevational view of a generator and a housing therefor, showin'g'my im-' proved setback-operated mechanism-in locked position. Fig. 2 is a view similar to Fig.1 but showing the locking mechanism released.
Fig. 3 is a cross section taken substantially on the line 3-3 of Fig. 1, and looking in the direction of the arrows.
. Referring now to the drawings, rotor l'is fastened to shaft 2, which may be driven by any suitable means (not shown but which may comprise a wind-driven impeller). Field coils 3, shown diagrammatically, are mounted in casing 6 in operative relationship to the rotor. Shaft 2 rotates in bearings 4 and 5 fixed in casing 6. Disc 7 is screwed or otherwise fastened to the lower face of rotor 1, and carries pins 8 positioned as best shown in plan in Fig. 3. Pins 8 normally extend downwardly beside arms 9, 12. Arms 9 are integral with a tapped cylindrical hub 10, threaded upon the axial bushing 5 upstanding from the bottom of the casing andwhich forms the lower bearing for the rotor. An additional. hub 11is downwardly slidable on the outside surface of hub 10 and carries arms 12 which normally block pins 8 and therefore prevent rotor 1 from being turned. Arms 12 are vertically slidable between and prevented from rotating byposts 13 fixed to the bottom of casing 6. Compression spring 14 urges the arm and hub assembly 11, 12 upwardly.
. It will be understood that the generator and its release mechanism are installed in the projectile or other vehicle with the axis of shaft 2 parallel to the line of I. set-back, compressing spring 14. This action brings locking arms 12 below pins 8 which are then rapidly revolved with rotor 1 by the driving means (unshown) attached to shaft 2. The direction of such rotation is ing a detent normally in operative blocking engagement with said rotorbut movable away from" such engagement under the influence of set back, spring means forv urging said detent in such operative blockingengagement, means for holding [said detent out of such' blocking engagement, and means for rotating said rotor rela'tive to said stator substantially immediately upon release of said rotor by said releasable locking means.
2. An electrical generator having rotor and stator means adapted for installation in a projectile or the like, set-back releasable locking means for said rotor including a detent normally in operative blocking engagement v with said rotor but movable away from such engagement under the influence of set-back, means for holding said detent out of such blocking engagement, said electrical generator being adapted for installation in a projectile with the axis of rotation of the rotor substantially parallel to the line of flight of the projectile, said locking means including a spring-held mass movable rearwardly with respect to the direction of flight during set-back, and said holding means including a hold-down nut actuatable by the rotor. I
3. An electrical generator having rotor and stator means adapted for installation in a projectile or the like, setback releasable locking means for said rotor including a detent normally in operative blocking engagement with said rotor but movable away from such engagement under the. influence of set-back, means for holding said detent out of such blocking engagement, said generator including a shaft supporting said rotor concentric with said stator means, the said stator means being adapted for installation in a projectile with the shaft substantially parallel to the line of flight of the projectile, said detent including a mass mounted concentrically with respect to and movable longitudinally of the shaft, spring means surrounding the shaft and urging said mass toward the rotor, and interengageable abutment portions carried by 1 said rotor and mass and separable when said detent moves detent normally in operative blocking engagement with said rotor but movable away from such engagement under the influence of set-back, means for holding said detent out of such blocking engagement, said generator including a shaft supporting said rotor concentric with said stator means, the said stator means being adapted for installation in a projectile with the shaft substantially parallel to the line of flight of the projectile, said detent including a mass mounted concentrically with respect to and movable longitudinally of the shaft, spring means surrounding the shaft and urging said mass toward the rotor, interengageable abutment portions carried by said rotor and mass and separable when said detent moves away, said holding means including a hold-down nut also surrounding the shaft anddrivable by the rotor, after release of said locking means, to a position in which it prevents reengagement of said abutment portions.v
V 5'. An electrical generator having rotor and stator means adapted for installation in a projectile or the like, setback releasable locking means for said rotor including a detent normally in operative blocking engagement with said rotor but movable away from such engagement under the influence of'set back, means for holding said detent out of such blocking engagement, said generator including a shaft supporting said rotor concentric with said stator means, the said stator means being adapted for installation in a projectile with the shaft substantially parallel to the line of flight of the projectile, said detent including a mass mounted concentrically with respect to and movable longitudinally of the shaft, spring means surrounding the shaft and urging said mass toward the rotor, interengageable abutment portions carried by said rotor and mass and separable when said detent moves away, said holding means including a hold-down nut also surrounding said shaft and drivable by the rotor, after release of said locking means, to a position in which it prevents reengagement of said abutment portions, said nut being arranged between the mass and the rotor and 4 f being of sufficient mass to coast to and hold the mass in a position in which said abutment portions are clear of one another.
6. An electrical generator having rotor and stator means adapted for installation in a projectile or the like, setback releasable locking means for said rotor including a detent normally in operative blocking engagement with said rotor but movable away from such engagement under the influence of set-back, means for holding said detent out of such blocking engagement, said generator including a shaft supporting said rotor concentric with said stator means, the said stator means being adapted for installation in a projectile with the shaft substantially parallel to the line of flight of the projectile, said detent including a mass mounted concentrically with respect to and movable longitudinally of the shaft, spring means surrounding the shaft and urging said mass toward the rotor, pins projecting longitudinally from the rotor and into driving engagement with said mass, said holding means including a hold-down nut also surrounding said shaft and engageable with and adapted to be driven by said pins, said nut being movable by said pins to a position in which .it prevents reengagement of said mass with the pins. 1 V 7 References Cited in the file of this patent UNITED STATES PATENTS 865,732 Vandervell et al. Sept. 10, 1907 984,607 Von Risch Feb. 21, 1911 1,568,527 Pearson Jan. 5, 1926 2,192,542 Benedetti Mar. 5, 1940 FOREIGN PATENTS 6,757 Great Britain Mar. 13, 1913
US535527A 1944-05-13 1944-05-13 Release mechanism Expired - Lifetime US2935950A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US535527A US2935950A (en) 1944-05-13 1944-05-13 Release mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US535527A US2935950A (en) 1944-05-13 1944-05-13 Release mechanism

Publications (1)

Publication Number Publication Date
US2935950A true US2935950A (en) 1960-05-10

Family

ID=24134631

Family Applications (1)

Application Number Title Priority Date Filing Date
US535527A Expired - Lifetime US2935950A (en) 1944-05-13 1944-05-13 Release mechanism

Country Status (1)

Country Link
US (1) US2935950A (en)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US865732A (en) * 1905-03-06 1907-09-10 Charles Anthony Vandervell Dynamo or the like.
US984607A (en) * 1910-08-23 1911-02-21 Isidor Theodor Von Risch Fuse for ordnance-shells.
US1568527A (en) * 1925-01-14 1926-01-05 Charles H Pearson Safety-clutch mechanism
US2192542A (en) * 1936-06-03 1940-03-05 Benedetti Giacomo De Electric detonator

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US865732A (en) * 1905-03-06 1907-09-10 Charles Anthony Vandervell Dynamo or the like.
US984607A (en) * 1910-08-23 1911-02-21 Isidor Theodor Von Risch Fuse for ordnance-shells.
US1568527A (en) * 1925-01-14 1926-01-05 Charles H Pearson Safety-clutch mechanism
US2192542A (en) * 1936-06-03 1940-03-05 Benedetti Giacomo De Electric detonator

Similar Documents

Publication Publication Date Title
US2511872A (en) Electric fuse
GB1213865A (en) Projectile fuze with improved time delay and self-destroying mechanism
US3611943A (en) Bombs fuses coupled axial impeller and generator rotor jointly shiftable rearwardly during launching to prevent rotation thereof
US2978982A (en) Magnetically delayed arming device for a fuze
US3861312A (en) Ignition device having an ignition sequence including fuse elements for preventing an unintentional release
US2935950A (en) Release mechanism
US2938461A (en) Free-flight arming device
US3326132A (en) Delay fuze for spinning projectiles
US2834292A (en) Intermittent action ball cam rotor
US2750888A (en) Long delay bomb tail fuze
US2789508A (en) Safety and arming mechanism
US1203528A (en) Starting device for explosion-engines.
US3772992A (en) Turbine alternator utilizing fluid bearings
US3093076A (en) Spring-started generator
US2748708A (en) Bomb fuze, centrifugal-inertia type
US3768415A (en) Fuze arming device
US3140661A (en) Generator-powered fuze
US3329014A (en) Drop and spin test apparatus
US3653325A (en) Delayed arming device for the proximity fuse of a bomb
GB1348756A (en) Mechanically operated fuse for gyratory missiles
US2680407A (en) Arming system
US3699892A (en) Controlled variable time radio proximity fuze
US2920570A (en) Safety and delay arming device
US2990776A (en) Wind driven generator
US2681008A (en) Fuse