US2274755A - Fuse - Google Patents

Fuse Download PDF

Info

Publication number
US2274755A
US2274755A US200333A US20033338A US2274755A US 2274755 A US2274755 A US 2274755A US 200333 A US200333 A US 200333A US 20033338 A US20033338 A US 20033338A US 2274755 A US2274755 A US 2274755A
Authority
US
United States
Prior art keywords
cap
base
fuse
groove
ring
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
US200333A
Inventor
Harold G Towner
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 US200333A priority Critical patent/US2274755A/en
Application granted granted Critical
Publication of US2274755A publication Critical patent/US2274755A/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
    • F42C19/00Details of fuzes
    • F42C19/02Fuze bodies; Fuze housings

Definitions

  • Patented Mar. 3, 1942 STATES PATENT OFFIQE (Granted under the act of March 3, 1883, as amended April 30, 1928; 370 0. G. 757) 1. Claim.
  • This invention relates in general to a fuse and more particularly it has reference to means for rotatably connecting the base and setting cap of a time fuse.
  • the purpose of this invention is to provide a simple and effective connection which will permit relative rotation of the cap and base to set the timing mechanism of the fuse and which will prevent their derangement under the infiuence of centrifugal force during flight.
  • the invention consists in the construction, arrangement and combination of elements described hereinafter and pointed out in the claim forming a part of this specification.
  • Fig. 1 is a longitudinal sectional view of a fuse casing whose units are held in assembly by the improved coupling means;
  • Fig. 2 is a sectional view on the line 22 of Fig. 1;
  • Fig. 3 is an enlarged sectional view on the line 3-3 of Fig. 2.
  • a fuse casing of generally circular shape in horizontal cross section comprising a base 5 and a rotatable setting cap 6.
  • the base is formed with a reduced upper part 1 for receiving the lower end of the cap which rests upon an annular seat 8 established in the base.
  • the lower end of the cap is provided internally with a radial inwardly opening circumferential or annular groove 9 of generally U-shape in cross-section which, when the cap is resting on the seat, registers with a circumferential orannular groove l0 provided externally on the reduced part I of the base.
  • the groove 10 has beveled or outwardly diverging side walls
  • the ring I3 is housed completely within the groove 9. If the ring should protrude from the groove 9 during this operation, the lower beveled edge l2 will engage the upper part 1 of the base and be forced outwardly into the groove 9.
  • a plurality of screws l4 are applied in threaded apertures of the cap and act on the ring I3 to move it inwardly until the beveled inner portion of the ring enters the groove ll] and engages the surfaces of the groove to interlock the base and cap against aixal separation.
  • the amount of pressure applied to the ring through the screws regulates the frictional contact between the ring and base and determines the resistance to rotation of the parts.
  • An adjustment is made which will permit rotation of the cap to set the timing mechanism of the fuse and which will prevent relative movement of the parts under the influence of centrifugal force during flight.
  • a fuse casing of generally circular shape in horizontal cross section including an annular groove having outwardly diverging upper and lower side walls, a setting cap mounted on the base for rotatable movement relative thereto and provided with a radial inwardly opening annular groove of generally U-shape in cross section and having upper and lower walls adapted to be registered with the outer termini of said diverging upper and lower side walls, respectively, a split ring of generally rectangular shape in cross section having radial inwardly converging upper and lower corners adapted to engage said diverging upper and lower side walls, respectively, inserted in said U-shape groove and adjustable means on said setting cap adapted to circumferentially contract the split ring to a position where its converging corners engage both of said diverging walls; whereby the setting cap and base are interlocked against axial separation and the frictional engagement between said diverging walls and converging corners may be regulated.

Description

' March 3, 1942. TOWNER 2,274,755
'.FUSE
Filed April 6,4938
Inventor Harald G-'Tmwnar may E'Mh, @M
Patented Mar. 3, 1942 STATES PATENT OFFIQE (Granted under the act of March 3, 1883, as amended April 30, 1928; 370 0. G. 757) 1. Claim.
The invention described herein may be manufactured and used by or for the Government for governmental purposes, without the payment to me of any royalty thereon.
This invention relates in general to a fuse and more particularly it has reference to means for rotatably connecting the base and setting cap of a time fuse.
In fuses wherein the cap is to be rotatable with respect to the base it has been the usual practice to connect these units by some form of coupling ring.
The purpose of this invention is to provide a simple and effective connection which will permit relative rotation of the cap and base to set the timing mechanism of the fuse and which will prevent their derangement under the infiuence of centrifugal force during flight.
To these and other ends, the invention consists in the construction, arrangement and combination of elements described hereinafter and pointed out in the claim forming a part of this specification.
A practical embodiment of the invention is illustrated in the accompanying drawing, wherein:
Fig. 1 is a longitudinal sectional view of a fuse casing whose units are held in assembly by the improved coupling means;
Fig. 2 is a sectional view on the line 22 of Fig. 1;
Fig. 3 is an enlarged sectional view on the line 3-3 of Fig. 2.
Referring to the drawing by characters of reference there is shown a fuse casing of generally circular shape in horizontal cross section comprising a base 5 and a rotatable setting cap 6. The base is formed with a reduced upper part 1 for receiving the lower end of the cap which rests upon an annular seat 8 established in the base.
The lower end of the cap is provided internally with a radial inwardly opening circumferential or annular groove 9 of generally U-shape in cross-section which, when the cap is resting on the seat, registers with a circumferential orannular groove l0 provided externally on the reduced part I of the base. The groove 10 has beveled or outwardly diverging side walls |l--ll for engagement by correspondingly beveled or converging inner edges |2--l2 of a split coupling ring l3 and the outer termini of the diverging side walls coincide or register with the corresponding termini of the side walls of the U- shape groove when the two grooves are in normal registration.
For the purpose of assembly of the casing the ring I3 is housed completely within the groove 9. If the ring should protrude from the groove 9 during this operation, the lower beveled edge l2 will engage the upper part 1 of the base and be forced outwardly into the groove 9. When the cap and the base are brought into final position a plurality of screws l4 are applied in threaded apertures of the cap and act on the ring I3 to move it inwardly until the beveled inner portion of the ring enters the groove ll] and engages the surfaces of the groove to interlock the base and cap against aixal separation. The amount of pressure applied to the ring through the screws regulates the frictional contact between the ring and base and determines the resistance to rotation of the parts. An adjustment is made which will permit rotation of the cap to set the timing mechanism of the fuse and which will prevent relative movement of the parts under the influence of centrifugal force during flight.
I claim:
A fuse casing of generally circular shape in horizontal cross section including an annular groove having outwardly diverging upper and lower side walls, a setting cap mounted on the base for rotatable movement relative thereto and provided with a radial inwardly opening annular groove of generally U-shape in cross section and having upper and lower walls adapted to be registered with the outer termini of said diverging upper and lower side walls, respectively, a split ring of generally rectangular shape in cross section having radial inwardly converging upper and lower corners adapted to engage said diverging upper and lower side walls, respectively, inserted in said U-shape groove and adjustable means on said setting cap adapted to circumferentially contract the split ring to a position where its converging corners engage both of said diverging walls; whereby the setting cap and base are interlocked against axial separation and the frictional engagement between said diverging walls and converging corners may be regulated.
HAROLD G. TOWNER.
US200333A 1938-04-06 1938-04-06 Fuse Expired - Lifetime US2274755A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US200333A US2274755A (en) 1938-04-06 1938-04-06 Fuse

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US200333A US2274755A (en) 1938-04-06 1938-04-06 Fuse

Publications (1)

Publication Number Publication Date
US2274755A true US2274755A (en) 1942-03-03

Family

ID=22741269

Family Applications (1)

Application Number Title Priority Date Filing Date
US200333A Expired - Lifetime US2274755A (en) 1938-04-06 1938-04-06 Fuse

Country Status (1)

Country Link
US (1) US2274755A (en)

Similar Documents

Publication Publication Date Title
US2309281A (en) Rod end connection
US2469637A (en) Umbrella frame
US2345910A (en) Connection for elements of rotatable units
US1289867A (en) Cotter-pin.
US2749162A (en) Non-rotatable retaining ring
US2723876A (en) Parachute release
US2274755A (en) Fuse
US2273920A (en) Universal joint
US2262068A (en) Fuse
US2494756A (en) Balance assembly for propeller blades
US1786330A (en) Valve device
US3467419A (en) Means for securing a rotor on a shaft
US2328898A (en) Rotary joint
KR890000805A (en) Joint device
US2548874A (en) Retaining device
US660559A (en) Expansion-bolt.
US3007747A (en) Universal bearing
US977458A (en) Roller-bearing having grooved rolls and tension-band.
US2330490A (en) Hand grenade
US2297506A (en) Elastic mounting
US1792631A (en) Fuse for projectiles
US1707414A (en) Fuse
US2201209A (en) Fuse
US1834521A (en) Shaft coupling
US2709963A (en) Variable torque mechanical time fuse