CASELESS AMMUNITION FOR FIREARM AND THE MECHANISM FOR THE EXTRACTION OF CASELESS AMMUNITION

Abstract

A mechanism for extraction caseless ammunition, the mechanism for extraction including a receiver (84) interacting with the lid of the receiver (85); lock frame (86) which interacts with the lid of the receiver; bolt (88) made in the lock frame; a conical bushing (93) installed inside the bolt through the firing pin (89); an extractor (95), wherein lock frame is made with a front ledge (87); on the front end of the firing pin the conical part (90) is made; conical bushing (93) is made with interior ledges (94); a shaft (103) with a circular groove (104); the rear part (102) passes into the lower ledge (106) which has a front inclined area (107) and a rear horizontal area (108) and the lower ledge (106) passes into the upper ledge (109) which has a front inclined area (110), an upper horizontal area (111) and a rear inclined area (112).

Claims

1. The mechanism for extraction careless ammunition, that comprises a shell, the propellant (solid, liquid, gas) of flammable material which is placed in the shell chamber, and an igniter block, wherein the shell body is made with a cylindrical part (25), which passes into an inclined surface (26) of the leading cylindrical part (29), which passes into the rear cylindrical part (30), herewith: said inclined surface (26) is made at an angle (d27) 30°-45° to the longitudinal axis (28)of the shell body; said leading cylindrical part (29) is made with a wall thickness (T29), the thickness (T29) of the leading cylindrical part (29) is 0.1.22D, where D-outside diameter of the ammunition; said rear cylindrical part (30) is made with smaller diameter than the diameter of the leading cylindrical part (29): between the leading cylindrical part (29) and the rear cylindrical part (30) the ledge (31) is made; rear cylindrical part (30) ends with a chamfer (32); the inlet interior cylindrical hole (33) is made in the body of the shell, into which an miter block (4) or (5) or (22) is installed, and the mechanism for extraction comprises the receiver (84) interacting with the lid of the receiver (85) which is made with possibility to make in and out movement; lock frame (86) which is made with possibility to make in and out movement and interacts with the lid of the receiver (85); the bolt (88) is made in the lock frame 1), and installed with possibility to make in and out movement a conical. bushing (93) is installed inside the bolt (88) through the firing pin (89); an extractor (95) which is made with possibility to rotate on the shaft (103) in the receiver (84), which is characterized in that lock frame (86) is made with a front ledge (87); on the front end of the firing pin (89) the conical part (90) is made, which passes into a cylindrical section of smaller diameter (91), herewith at the juncture of the conical section (90) and cylindrical section of smaller diameter (91) inclined ledge (92) is formed; conical bushing (93) is made with interior ledges (94); an extractor (95) is made with a. ledge (96) with a semicircular hollow (97) which passes into an upper ledge (98) which has a front inclined area (99) and a rear inclined area (100) and the upper ledge (98) passes into the fore-part (101) which passes into the rear part (102); a shaft (103) with a circular groove (104) which is placed on the contact point of the forepart (101) and the rear part (102), herewith the rear part (102) passes into the lower ledge (106) which has a front inclined area (10) and a rear horizontal area (108) and the lower ledge (106) passes into the upper ledge (109) which has a front inclined area (110), an upper horizontal area (111) and a rear inclined area (112).

2. The mechanism for the extraction of caseless ammunition according to claim 1, wherein the angle (d92) of inclined ledge (92) about the axis of the firing pin (89) is 30-45 degrees.

3. The mechanism for the extraction of caseless ammunition according to claim 1, wherein between the end face of conical section (90) of the firing pin (89) and a primer with an anvil (67) of igniter block (4,5) of the caseless ammunition a gap (114) is made.

4. The mechanism for the extraction of caseless ammunition according to claim 3, wherein the thickness (T114) of the gap (114) is 0.03-0.05D, wherein D-outside diameter of the ammunition.

5. The mechanism for the extraction of caseless ammunition according to claim 1, wherein the conical bushing (93) on the bolt (88) forms a gap (115) with the rear end of the ammunition.

6. The mechanism for the extraction of caseless ammunition according to claim 5, wherein the thickness (T115) of the gap (115) is equal to 0.2D, wherein D-outside diameter of the ammunition.

7. The mechanism for the extraction of caseless ammunition according to claim 1, wherein the mechanism works only with hand reloading.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0084] FIG. 1. Acute caseless ammunition, hereafter caseless ammunition 1 (side view).

[0085] FIG. 2. Blunt-ended caseless ammunition, hereafter—caseless ammunition 6 (side view).

[0086] FIG. 3. Armor-piercing caseless ammunition, hereafter—caseless ammunition 8 (side view).

[0087] FIG. 4. Enhanced armor-piercing caseless ammunition, hereafter—caseless ammunition 10 (side view).

[0088] FIG. 5. Tracer caseless ammunition, hereafter—caseless ammunition 12 (side view).

[0089] FIG. 6. Acute caseless :ammunition for noiseless timeless shooting, hereafter—caseless ammunition 16 (side view).

[0090] FIG. 7. Blunt-ended caseless ammunition for noiseless flameless shooting, hereafter—caseless ammunition 18 (side view).

[0091] Training caseless ammunition, hereafter—caseless ammunition 20 (side view).

[0092] FIG. 9. Caseless ammunition 1, detail design (side view).

[0093] FIG. 10. Caseless ammunition 6, detail design (side view).

[0094] FIG. 11. Caseless .ammunition 8, detail design (side view).

[0095] FIG. 12. Caseless ammunition 10, detail design (side view).

[0096] FIG. 13. Caseless ammunition 12, detail design (side view).

[0097] FIG. 14. Caseless ammunition 16, detail design (side view).

[0098] FIG. 15. Caseless ammunition 18, detail design (side view).

[0099] FIG. 16. Caseless ammunition 20, detail design (side view).

[0100] FIG. 17. Acute shell, hereafter—shell 2 (side view).

[0101] FIG. 18. Blunt-ended shell, hereafter—shell 7 (side view).

[0102] FIG. 19. Acute shell, hereafter—shell 9 (side view).

[0103] FIG. 20. Shell 9, detail design (side view).

[0104] FIG. 21. Acute shell, hereafter—shell 11 (side view).

[0105] FIG. 22. Shell 11, detail design (side view).

[0106] FIG. 23. Body 41 (side view).

[0107] FIG. 24. Amor-piercing tip 42 (side view).

[0108] FIG. 25. Body 43 (side view).

[0109] FIG. 26. Amor-piercing core tip 44 (side view).

[0110] FIG. 27. Tracer ammunition 12, detail design (side view).

[0111] FIG. 28. Washer 15 (side view).

[0112] FIG. 29. Acute shell for noiseless flameless shooting, hereafter—shell 17 (side view).

[0113] FIG. 30. Shell 17, detail design (side view).

[0114] FIG. 31. Blunt-ended shell for noiseless flameless shooting, hereafter—shell 19 (side view)

[0115] FIG. 32. Detail design of shell 19 (side view).

[0116] FIG. 33. Body 57 (side view).

[0117] FIG. 34. Tip 58 (side view).

[0118] FIG. 35. Tip 59 (side view)

[0119] FIG. 36. Acute shell, hereafter—shell 21 (side view).

[0120] FIG. 37. Igniter block for mechanical extraction, hereafter—igniter block 4 (side view).

[0121] FIG. 38. Igniter block for magnetic extraction, hereafter—igniter block 5 and training igniter block 22 (side view)

[0122] FIG. 39. Igniter block 4, detail design (side view).

[0123] FIG. 40. Igniter block 5 and training igniter block 22, detail design (side view).

[0124] FIG. 41. Body of igniter block, hereafter—body 66 (side view).

[0125] FIG. 42. External washer-marker 70 (side view).

[0126] FIG. 43, FIG. 44. Protection of primer of igniter block with anvil 67 from ignition by acute end 24 of ammunition 1; 8; 10; 12; 16; 20 (side view).

[0127] FIG. 45. Mechanism for extraction of caseless ammunition (side view).

[0128] FIG. 46. Unit A of mechanism for extraction of caseless ammunition 1; 6; 8; 10; 12; 16; 18; 20 in weapon with open chamber, hereafter - mechanism (side view).

[0129] FIG. 47. Side view of extractor.

[0130] FIG. 48. Mechanism far extraction of caseless ammunition (side view).

[0131] FIG. 49. Unit B for mechanical extraction on FIG. 48.

[0132] FIG. 50. Unit B for magnetic exaction on FIG. 48. Beginning of ammunition extraction 1;6;8;10;12;16;18;20.

[0133] FIG. 51. Mechanism for extraction of caseless ammunition (side view).

[0134] FIG. 52. A cross-section 1-1 on FIG. 51. The supply of extractor 95 for ammunition 1; 6; 8; 10; 12; 16; 18; 20 is shown.

[0135] FIG. 53. Mechanism for extraction of caseless ammunition (side view).

[0136] FIG. 54. Unit C on FIG. 53.

[0137] FIG. 55. Unit C on FIG. 53. The removal of trapped ammunition 1; 6; 8; 10; 12; 16; 18; 20 by means of extractor 95 from bolt 88 is shown.

[0138] FIG. 56. Mechanism for extraction of caseless ammunition (side view). The ejection of ammunition 1; 6; 8; 10; 12; 16; 1.8; 20 by extractor 95 from weapon is shown.

[0139] Designations on the figures of the drawings which have been used in the claimed invention:

[0140] 1-caseless ammunition;

[0141] 2-shell;

[0142] 3-propellent;

[0143] 4-igniter block;

[0144] 5-igniter block;

[0145] 6-caseless ammunition;

[0146] 7-shell;

[0147] 8-caseless ammunition;

[0148] 9-shell;

[0149] 10-caseless ammunition;

[0150] 11-shell;

[0151] 12-caseless ammunition;

[0152] 13-shell;

[0153] 14-tracer compound;

[0154] 15-washer;

[0155] 16-caseless ammunition;

[0156] 17-shell;

[0157] 18-caseless ammunition;

[0158] 19-shell;

[0159] 20-caseless ammunition;

[0160] 21-shell;

[0161] 22-training igniter block;

[0162] 23-lancet section;

[0163] 24-acute end;

[0164] 25-cylindrical part;

[0165] 26-inclined surface;

[0166] 27-acute angle;

[0167] d27-measure of an acute angle;

[0168] 28-longitudinal axis;

[0169] 29-leading cylindrical part;

[0170] T29-thickness of a leading cylindrical part;

[0171] 30-rear cylindrical part

[0172] 31-ledge;

[0173] 32-chamfer;

[0174] 33-inlet interior cylindrical hole;

[0175] 34-middle cylindrical hole;

[0176] 35-conical transition;

[0177] 36-conical hole;

[0178] 37-ogive hole;

[0179] 38-shell chamber for propellent;

[0180] 39-truncated cone;

[0181] 40-ogive tip;

[0182] 41-body;

[0183] 42-armor-piercing tip;

[0184] 43-body;

[0185] 44-armor-piercing core tip;

[0186] 45-flat end of the lancet section 23;

[0187] 46-blind hole;

[0188] 47-cone;

[0189] 48-cylindrical ledge;

[0190] 49-through hole;

[0191] 50-cylindrical head;

[0192] 51-conical end;

[0193] 52-cylindrical rod:

[0194] 53- chamfer;

[0195] 54-circular plate;

[0196] 55-central through hole;

[0197] 56-external chamfer;

[0198] 57-body.

[0199] 58-tip;

[0200] 59-tip;

[0201] 60-end face;

[0202] 61-cylindrical ledge;

[0203] 62-end face;

[0204] 63-interior entering chamfer;

[0205] 64-blind cylindrical hole;

[0206] 65-conical hole;

[0207] 66-body of igniter block 4; 5; 22;

[0208] 67-primer of igniter block with anvil;

[0209] 68-interior washer;

[0210] 69-expanding ring;

[0211] 70-external washer-marker;

[0212] 71-magnetic extraction washer-marker;

[0213] 72-sterile capsule;

[0214] 73-small cylindrical section;

[0215] 74-big cylindrical section;

[0216] 75-end face;

[0217] 76-central seed hole;

[0218] 77-blind hole;

[0219] 78-smaller blind hole;

[0220] 79-cylinder;

[0221] 80-interior cylindrical hole;

[0222] 81-conical section;

[0223] 82-external chamfer;

[0224] 83-gap;

[0225] T83-thickness of gap 83;

[0226] 84-receiver;

[0227] 85-lid of receiver;

[0228] 86-lock frame;

[0229] 87-front ledge of lock frame;

[0230] 88-bolt;

[0231] 89-firing pin;

[0232] 90-conical section;

[0233] 91-cylindrical section;

[0234] 92-inclined ledge;

[0235] d92-angle of inclined ledge 92;

[0236] 93-conical bushing;

[0237] 94-interior ledges;

[0238] 95-extractor;

[0239] 96-ledge;

[0240] 97-semicircular hollow;

[0241] 98-upper ledge;

[0242] 99-front inclined area;

[0243] 100-rear inclined area;

[0244] 101-fore-part;

[0245] 102-rear part;

[0246] 103-shaft;

[0247] 104-circular groove;

[0248] 105-contr-washer;

[0249] 106-lower ledge;

[0250] 107-front inclined area;

[0251] 108-rear horizontal area;

[0252] 109-upper ledge;

[0253] 110-front inclined area;

[0254] 111-upper horizontal area;

[0255] 112-rear inclined area;

[0256] 113-lower part;

[0257] 114-gap;

[0258] T114-thickness of gap 114;

[0259] 115-gap;

[0260] T115-thickness of gap 115.

[0261] Shells are made of steel in the proposed invention.

[0262] Full description of the drawing of invention

[0263] FIG. 1 shows caseless ammunition 1 (side view). This configuration comprises: acute shell 2, propellant 3 (solid, liquid and gaseous) and igniter block 4 or 5.

[0264] FIG. 2 shows caseless ammunition 6 (side view). This configuration comprises: shell 7, propellant 3 (solid, liquid and gaseous) and igniter block 4 or 5.

[0265] FIG. 3 shows caseless ammunition 8 (side view). This configuration comprises shell 9, propellant 3 (solid, liquid and gaseous) and igniter block 4 or 5.

[0266] FIG. 4 shows caseless ammunition 10 (side view). This configuration comprises shell 11, propellant 3 (solid, liquid and gaseous) and igniter block 4 or 5.

[0267] FIG. 5 shows caseless ammunition 12 (side view). This configuration comprises shell 13, propellant 3 (solid, liquid and gaseous) and igniter block 4 or 5, tracer compound 14 and washer 15.

[0268] FIG. 6 shows caseless ammunition 16 (side view). This configuration comprises shell 17, propellant 3 (solid, liquid and gaseous) and igniter block 4 or 5.

[0269] FIG. 7 shows caseless ammunition 18 (side view). This configuration comprises shell 19, propellant 3 (solid, liquid and gaseous) and igniter block 4 or 5.

[0270] FIG. 8 shows caseless ammunition 20 (side view). This configuration comprises shell 21 and training igniter block 22.

[0271] FIG. 9 shows detail design of caseless ammunition 1 (side view). This configuration comprises acute shell 2, propellant 3 (solid, liquid and gaseous) and igniter block 4 or 5.

[0272] FIG. 10 shows detail design of caseless ammunition 6 (side view). This configuration comprises shell 7, propellant 3 (solid, liquid and gaseous) and igniter block 4 or 5.

[0273] FIG. 11 shows detail design of caseless ammunition 8 (side view). This configuration comprises shell 9, propellant 3 (solid, liquid and gaseous) and igniter block 4 or 5.

[0274] FIG. 12 shows detail design of caseless ammunition 10 (side view). This configuration comprises shell 11, propellant 3 (solid, liquid and gaseous) and igniter block 4 or 5.

[0275] FIG. 13 shows detail design of caseless ammunition 12 (side view). This configuration comprises shell 13, propellant 3 (solid, liquid and gaseous) and igniter block 4 or 5, tracer compound 14 and washer 15.

[0276] FIG. 14 shows detail design of caseless ammunition 16 (side view). This configuration comprises shell 17, propellant 3 (solid, liquid and gaseous) and igniter block 4 or 5.

[0277] FIG. 15 shows detail design of caseless ammunition 18 (side view). This configuration comprises shell 19, propellant 3 (solid, liquid and gaseous) and igniter block 4 or 5.

[0278] FIG. 16 shows detail design of caseless ammunition 20 (side view). This configuration comprises shell 21, propellant 3 (solid, liquid and gaseous) and training igniter block 22.

[0279] FIG. 17 shows side view of shell 2. The fore-part of the shell body 2 is made as a lancet section 23 with an acute end 24 which passes into a cylindrical part 25, which passes into an inclined surface 26 of the leading cylindrical part 29, which passes into the rear cylindrical part 30 with smaller diameter.

[0280] Inclined surface 26 is made at an angle 27 to the longitudinal axis 28 of the shell 2. Acute angle 27 has measure d27 which is equal to 30°-45° to the longitudinal axis 28 of the shell body, as a result, rifling of ammunition in the weapon occurs in less vulnerable state.

[0281] The thickness T29 of the leading cylindrical part 29 is 0.122D, where D-outside diameter of the ammunition, which is 1.5-2 times greater than thickness T.sub.swcb of side wall at case bottom of traditional ammunition for small arms, where (T.sub.swcb=0.052-0.078 D.sub.cb, where D.sub.cb is outer diameter at case bottom), that provides a great inertia of the shell heating. Thereby the moment of self-ignition of the shell inside the weapon is considerably delayed, wherein the shell 2 can operate in the weapon at pressures P.sub.max=620 MPa, which is two times higher than that of the traditional small arms, which makes it possible to increase the shooting energy.

[0282] Between the leading cylindrical part 29 and the rear cylindrical part 30 the ledge 31 is made. Rear cylindrical part 30 ends with a chamfer 32. The inlet interior cylindrical hole 33 is made in the body of the shell 2, into which c - igniter block 4 or 5 is installed; the inlet interior cylindrical hole 33 passes into the middle cylindrical hole 34 which via a conical transition 35 passes into the conical hole 36 which passes into ogive hole 37. The middle cylindrical hole 34, a conical transition 35, conical hole 36 and the ogive hole 37 form a shell chamber 38 for the propellant 38. All elements of shell 2, their shapes and interactions are shown on FIG. 17.

[0283] FIG. 18 shows side view of shell 7. The fore-part of the shell body (7 is made as a truncated cone 39 with an ogival tip 40. Truncated cone 39 passes into cylindrical part 25, which passes into an inclined surface 26. Inclined surface 26 is made at acute angle 27 to the longitudinal axis 28 of the shell 7.

[0284] Acute angle has measure d27 which is equal to 30°-45° to the longitudinal axis 28 of the shell body, as a result, rifling of ammunition in the weapon occurs in less vulnerable state.

[0285] The inclined surface 26 of the leading cylindrical part 29 passes into the rear cylindrical part 30 with smaller diameter.

[0286] The thickness T29 of the leading cylindrical part 29 is 0.122D, where D-outside diameter of the ammunition; which is 1.5-2 times greater than thickness T.sub.swcb of traditional ammunition for small arms, where T.sub.swcb=0.052-0.078 D.sub.cb, where D.sub.cb is outer diameter at case bottom, that provides a great inertia of the shell heating. Thereby the moment of self-ignition of the shell inside the weapon is considerably delayed, wherein the shell 7 can operate in the weapon at pressures P.sub.max=620 MPa, which is two times higher than that of the traditional small arms, which makes it possible to increase the shooting energy.

[0287] Between the leading cylindrical part 29 and the rear cylindrical part 30 the ledge 31 is made. Rear cylindrical part 30 ends with a chamfer 32. The inlet interior cylindrical hole 33 is made in the body of the shell, into which an igniter block 4 or 5 is installed; the inlet interior cylindrical hole 33 passes into the middle cylindrical hole 34 which via a conical transition 35 passes into the conical hole 36 which passes into ogive hole 37, herewith the middle cylindrical hole 34, a conical transition 35, conical hole 36 and the ogive hole 37. Middle cylindrical hole 34, conical transition 35, conical hole 36 and ogive hole 37 form a shell chamber 38 for the propellant 38. All elements of shell 2, their shapes and interactions are shown on FIG. 18.

[0288] FIG. 19 shows side view of shell 9. Shell 9 comprises body 41 and armor-piercing tip 42.

[0289] FIG. 20 shows detail design of shell 9, which comprises body 41 and armor-piercing tip 42 (side view).

[0290] FIG. 21 shows side view of shell 11. Shell 11 comprises both 43 and armor-piercing tip 44.

[0291] FIG. 22 shows detail design of shell 11, which comprises body 43 and armor-piercing tip 44 (side view).

[0292] FIG. 23 shows side view of body 41. The fore-part of the body 41 of the shell 9 is made as a lancet section 23 with a flat end 45 and blind hole 46, into which armor-piercing tip 42 is installed. A lancet section 23, which passes into a cylindrical part 25, which passes into an inclined surface 26. Inclined surface 26 is made at an angle 27 to the longitudinal axis 28 of the body 41. Acute angle has measure d27 which is equal to 30°-45° to the longitudinal axis 28 of the shell body; as a result, rifling of ammunition in the weapon occurs in less vulnerable state.

[0293] The inclined surface 26 of the leading cylindrical part 29 passes into the rear cylindrical part 30 with smaller diameter.

[0294] The thickness T29 of the leading cylindrical part 29 is 0.122D, where D-outside diameter of the ammunition; which is 1.5-2 times greater than thickness T.sub.swcb of traditional ammunition for small arms, where T.sub.swcb=0.052-0.078 D.sub.cb, where D.sub.cb is outer diameter at case bottom, that provides a great inertia, of the shell heating. Thereby the moment of self-ignition of the shell inside the weapon is considerably delayed, wherein the body 41 can operate in the weapon at pressures P.sub.max=620 Mpa, which is two times higher than that of the traditional small arms, which makes it possible to increase the shooting energy.

[0295] Between the leading cylindrical part 29 and the rear cylindrical part 30 the ledge 31 is made. Rear cylindrical part 30 ends with a chamfer 32. The inlet interior cylindrical hole 33 is made in the body 41, into which an igniter block 4 or 5 is installed; the inlet interior cylindrical hole 33 passes into the middle cylindrical hole 34 which via a conical transition 35 passes into the conical hole 36 which passes into ogive hole 37, herewith the middle cylindrical hole 34, a conical transition 35, conical hole 36 and the ogive hole 37. Middle cylindrical hole 34, conical transition 35, conical hole 36 and ogive hole 37 form a shell chamber 38 for the propellant 3. All elements of body 41, their shapes and interactions are shown on FIG. 23.

[0296] FIG. 24 shows armor-piercing tip 42 side view which is installed in the fore-part and made as a cone 47 with an acute end 24 and the cylindrical ledge 48 for blind hole 46 of body 41. All elements of armor-piercing tip 42, their shapes and interactions are shown on FIG. 24.

[0297] FIG. 25 shows side view of body 43 side view . The fore-part of the body 43 of the shell 9 is made as a lancet section 23 with a flat end 45 and blind hole 46 and through hole 49, herewith in a blind hole 46 and a through hole 49 armor-piercing core tip 44 is installed. Lancet section passes into cylindrical part 25, which passes into an inclined surface 26. Inclined surface 26 is made at an angle 27 to the longitudinal axis 2$ of the body 43. Acute angle 27 has measure d27, which is equal to 30°-45° to the longitudinal axis 28 of the shell body, as a result, rifling of ammunition in the weapon occurs in less vulnerable state.

[0298] The inclined surface 26 of the leading cylindrical part 29 passes into the rear cylindrical part 30 with smaller diameter. The thickness T29 of the leading cylindrical part 29 is 0.122D, where D-outside diameter of the ammunition; which is 1.5-2 times greater than thickness T.sub.swcb of side wall at case bottom of traditional ammunition for small arms, where T.sub.swcb=0.052-0.078 D.sub.cb, where D.sub.cb is outer diameter at case bottom, that provides a great inertia of the shell heating; thereby the moment of self-ignition of the shell inside the weapon is considerably delayed, wherein the body 43 can operate in the weapon at pressures P.sub.max=620 Mpa, which is two times higher than that of the traditional small arms, which makes it possible to increase the shooting energy.

[0299] Between the leading cylindrical part 29 and the rear cylindrical part 30 the ledge 31 is made. Rear cylindrical part 30 ends with a chamfer 32. The inlet interior cylindrical hole 33 is made in the body 43, into which an igniter block 4 or 5 is installed; the inlet interior cylindrical hole 33 passes into the middle cylindrical hole 34 which via a conical transition 35 passes into the conical hole 36 which passes into ogive hole 37, herewith the middle cylindrical hole 34, a conical transition 35, conical hole 36 and the ogive hole 37. Middle cylindrical hole 34, conical transition 35, conical hole 36 and ogive hole 37 form a shell chamber 38 for the propellant 3. All elements of body 43, their shapes and interactions are Shown on FIG. 25.

[0300] FIG. 26 shows side view of armor-piercing core tip 44 which is made as a cylindrical head 50, that passing into a conical end 51 with an acute end 24, on one side, and passing into a cylindrical rod 52 on other side. At the end of the cylindrical rod 52 a chamfer 53 is made. All elements of armor-piercing core tip 44, their shapes and interactions are shown on FIG. 26.

[0301] FIG. 27 shows side view of shell 13. The fore-part of the shell body 13 is made as a lancet section 23 with an acute end 24. Lancet section 23 passes into cylindrical part 25, which passes into an inclined surface 26. Inclined surface 26 is made at an angle 27 to the longitudinal axis 28 of the shell. Acute angle 27 has measure d27 which is equal to 30°-45° to the longitudinal axis 28 of the shell body; as a result, rifling of ammunition in the weapon occurs in less vulnerable state.

[0302] The inclined surf lice 26 of the leading cylindrical part 29 passes into the rear cylindrical part 30 with smaller diameter.

[0303] The thickness T29 of the leading cylindrical part 29 is 0.122D, where D-outside diameter of the ammunition; which is 1.5-2 times greater than thickness T.sub.swcb of side wall at case bottom of traditional ammunition for small arms, where T.sub.swcb=0.052-0.078 D, where D.sub.cb is outer diameter at case bottom, that provides a great inertia of the shell heating. Thereby the moment of self-ignition of the shell inside the weapon is considerably delayed, wherein the shell 13 can operate in the weapon at pressures P.sub.max=620 Mpa, which is two times higher than that of the traditional small arms, which makes it possible to increase the shooting energy.

[0304] Between the leading cylindrical part 29 and the rear cylindrical part 30 the ledge 31 is made. Rear cylindrical part 30 ends with a chamfer 32.

[0305] The inlet interior cylindrical hole 33 which is made in the shell body 13 passes into the middle cylindrical hole 34 which via a conical transition 35 passes into the conical hole 36 which passes into an ogive hole 37, herewith washer 15 is additionally installed in ammunition, a chamfer 56 of which bears against a conical transition 35, herewith the middle cylindrical hole 34 forms chamber 38 for the propellant 3. The tracer compound 14 is placed in the ogive hole 37 and the conical hole 36. The propellant 3 occupies the middle cylindrical hole 34. Washer 15 bears against conical transition 35 by the chamfer 59 which separates the propellant 3 and the tracer compound 14, thereby it doesn't allow tracer compound to burn out during initial stage of ignition. During ignition burning propellant 3 passes through the central through hole 55 under high pressure and ignites the tracer compound 14. Burnout velocity of tracer compound 14 depends on the size of the central through hole 55. All elements of ammunition 12, their shape and interactions axe shown on. FIG. 27.

[0306] FIG. 28 shows side view of washer 15, which is made as circular plate 54 with central through hole 55 in the middle and external chamfer 56. All elements of washer, their shapes and interactions are shown on. FIG. 28.

[0307] FIG. 29 Shows side view of shell 17, which comprises body 57 and tip 58.

[0308] FIG. 30 shows detail design of shell 17, which comprises body 57 and tip 58.

[0309] FIG. 31 Shows side view of shell 19, which comprises body 57 and tip 59.

[0310] FIG. 32 shows detail design of shell 19, which comprises body 57 and tip 59.

[0311] FIG. 33 shows body 57. In the body 57 of the shell 17 and shell 19 in an end face 60 of the cylindrical part 25 is made a cylindrical ledge 61 for blind cylindrical hole 64 of the rear part of tip 58 or 59. Cylindrical part 25, which passes into an inclined surface 26 of the leading cylindrical part 29. Which passes into the rear cylindrical part 30, with smaller diameter. Inclined surface 26 is made at acute angle 27 to the longitudinal axis 28 of the body 57. Acute angle has measure d27 which is equal to 30°-45° to the longitudinal axis 28 of the shell body; as a result, rifling of ammunition in the weapon occurs in less vulnerable state.

[0312] The thickness T29 of the leading cylindrical part 29 is 0.122D, where D-outside diameter of the ammunition; which is 1.5-2 times greater than thickness T.sub.swb of side wall at case bottom of traditional ammunition for small arms, where T.sub.swcb=0.052-0.078 D.sub.cb, where D.sub.cb is outer diameter at case bottom, that provides a great inertia of the shell heating; thereby the moment of self-ignition of the shell inside the weapon is considerably delayed, wherein the body 57 can operate in the weapon at pressures P.sub.max=620 Mpa, which is two times higher than that of the traditional small arms, which makes it possible to increase the shooting energy.

[0313] Between the leading cylindrical part 29 and the rear cylindrical part 30 the ledge 31 is made. Rear cylindrical part 30 ends with a chamfer 32. The inlet interior cylindrical hole 33 is made in the body 57, for an igniter block 4 or 5, which passes into the middle cylindrical hole 34 and ogive hole 37. Middle cylindrical hole 34 and ogive hole 37 form a shell chamber for the propellant 38. All elements of body 57, their shapes and interactions are shown on FIG. 33.

[0314] FIG. 34 shows side view of tip 58, which is made as lancet section 23 with an acute end 24. In the end face 62 of the lancet section 23 interior entering chamfer 63 is made, which passes into the blind cylindrical hole 64. Entering chamfer 63 anal blind cylindrical hole 64 are made for installation of tip 55 58 into the cylindrical ledge of body 57. All elements of tip 58, their shapes and interactions are shown on FIG. 34.

[0315] FIG. 35 shows side view of tip 59, which is made as a truncated cone 39 with an ogive tip 40. In the end face 62. of the truncated cone 39 interior entering chamfer 63 is made, which passes into the blind cylindrical hole 64. Interior entering chamfer 63 and blind cylindrical hole 64 are made for installation of tip 59 into the cylindrical ledge 61 of the body 57. All elements of tip 58, their shapes and interactions are shown on FIG. 35.

[0316] FIG. 36 shows side view of shell 21. The fore-part of the shell 21 is made as a lancet section 23 with an acute end 24 which passes into cylindrical part 25, which passes into an inclined surface 26. Inclined surface 26 is made at an acute angle 27 to the longitudinal axis 28 of the shell 21. An acute angle has measure d27 which is equal to 30°-45° to the longitudinal axis 28 of the shell 21; as a result, rifling of ammunition in the weapon occurs in less vulnerable state. The inclined surface 26 passes. into the leading cylindrical part 29 passes into the rear cylindrical part 30 with smaller diameter. Between the leading cylindrical part 29 and the rear cylindrical part 30 the ledge 31 is made. Rear cylindrical part 30 ends with a chamfer 32.

[0317] The inlet interior cylindrical hole 33 is made in the shell 21 for training igniter block 22, which passes into middle cylindrical hole 34, which passes into a conical hole 65, wherein the volume of the middle cylindrical hole 34 and the conical hole 65 is selected so that the total mass of the shell 21 is equal to the weight of careless ammunition 1 or 6 or 8 or 10 or 12 or 16 or 18 and the training, igniter block 22 is installed in the inlet interior cylindrical hole 33. All elements of shell 21, their shapes and interactions are shown on FIG. 36.

[0318] FIG. 37 shows side view of igniter block 4, which comprises body 66, primer of igniter block with an anvil 67, the interior washer 68, expanding ring 69 and the external washer-marker 70.

[0319] FIG. 38 Shows side view of igniter block 5 and training igniter block 22, which comprises body 66, primer of igniter block with an anvil 67, the magnetic. extraction washer-marker 71.

[0320] FIG. 39 show detail design of igniter block 4, which comprises body 66, primer of igniter block with an anvil 67, the interior washer 68. expanding ring 69 and the external washer-marker 70. The external washer-marker 70 is made in different colors in order to distinguish types of ammunition that is used.

[0321] FIG. 40 shows. detail design of igniter block 5 and training igniter block 22, which comprises body 66, primer of igniter block with an anvil of remington type 67 or sterile primer 72 the magnetic extraction washer-marker 71. The magnetic extraction washer-marker 71 is made in different colors which dependend on type of ammunitions that are used, Training igniter block 22 has a sterile primer 72.

[0322] FIG. 41 shows side view of body 66. Body 66 is made with small cylindrical section 73 which passes into a big cylindrical section 74. In the end face 75 of the small cylindrical section 73 central seed hole is made 76. In the end face of the big cylindrical section 74 a blind hole 77 is made, which passes into smaller blind hole 78. The blind hole 77 is used for interior washer 68, external washer-maker 70 or magnetic extraction washer-maker 71. Smaller blind hole 78 is used for primer of igniter block with anvil 67 or sterile capsule 72. All elements of body 66, their shapes and interactions are shown on FIG. 41.

[0323] FIG. 42 shows side view of external washer-maker 70. External washer-maker 70 which is made as a cylinder 79 with an interior cylindrical hole 80 for expanding ring 69. An interior cylindrical hole 80 passes into the small base of the conical section 81 with a smaller diameter. On a cylinder 79 external chamfer 82 is made from the side of the interior cylindrical hole 80. All elements of external washer-maker 70, their shapes and interactions are shown on FIG. 42.

[0324] FIG. 43, 44 shows the protection of primer with an anvil 67 from ignition by acute end 24 of ammunition 1 or 8 or 10 or 12 or 16 or 20. Gap 83, which is located between the primer with an anvil 67 and the acute end 24 of the ammunition 1 or 8 or 10 or 12 or 16 or 20, doesn't allow to stab primer with an anvil 67 by acute end of ammunition 1 or 8 or 10 or 12 or 16 or 20. The thickness T83 of the gap 83 is equal to 0.05D, where D-outside diameter of the ammunition 1 or 6 or 8 or 10 or 12 or 16 or 18 or 20. Acute end 24 of ammunition 1 or 8 or 10 or 12 or 16 or 20 reduces the air resistance of the shell flight trajectory, which reduces the loss of initial shell velocity, and also increases the penetrating, power soft ballistic vests thanks to separation of cells of cloth, and in solid armored jackets thanks to concentration of voltage on considerably smaller area in an acute end 24.

[0325] FIG. 45 shows side view of mechanism and FIG. 46—unit A of mechanism for extraction caseless ammunitions 1; 6; 8; 10; 12; 16; 18; 20 in weapon with open chamber. Mechanism comprises the receiver 84, the lid of the receiver $5, lock frame 86 with a front ledge 87, the bolt 88, the firing pin 89. On the front end of the firing pin 89 the conical part 90 is made, which passes into a cylindrical section of smaller diameter 91, wherein at the juncture of the conical section 90 and cylindrical section of smaller diameter 91 inclined ledge 92 is formed. The angle d92 of inclined ledge 92 about the axis of the firing pin 89 is 30-45. degrees what is optimum to ensure peeling force of ammunition 1 or 6 or 8 or 10 or 12 or 16 or 18 or 20 with riffling of the barrel. Mechanism also comprises conical bushing 93 which is made with interior ledges 94 of ammunition 1 or 6 or 8 or 10 or 12 or 16 or 18 or 20 and extractor 95.

[0326] FIG. 47 shows side view of extractor 95. The extractor 95 is made with a ledge 96 with a semicircular hollow 97 which passes into an upper ledge 98 which has a front inclined area 99 and a rear inclined area 100. The upper ledge 98 passes into the fore-part 101 which passes into the rear part 102. A shaft 103 with a circular groove 104 which is placed at the juncture of the fore-part 101 and the rear part 102. Circular groove 104 is made for fixation of extractor 95 with contr-washers in receiver 84. The rear part 102 passes into the lower ledge 106 which has a front inclined area 107 and a rear horizontal area 108. The lower ledge 106 passes into the upper ledge 109 which has a front inclined area 110, an upper horizontal area 111 and a rear inclined area 112. All elements of extractor 95, their shapes and interactions are shown on FIG. 47.

[0327] FIG. 48 shows side view of mechanism and FIG. 49—unit B for mechanical extraction on FIG. 48 and FIG. 50—unit B for magnetic extraction on FIG. 48. Beginning of extraction of ammunition 1 or 6 or 8. or 10 or 12 or 16 or 18 or 20. Extraction of the ammunition 1 or 6 or 8 or 10 or 12 or 16 or 18 or 20 begins with approach of the lower part 113, a front ledge of lock frame 87, lock frame 86 to front inclined. area 99 of extractor 95, wherein rear part of ammunition 1 or 6 or 8 or 10 or 12 or 16 or 18 or 20 enters into inclined ledge 92 on front ledge of lock frame 87 and bears against conical bushing. 93, wherein rear part of ammunition 1 or 6 or 8 or 10 or 12 or 16 or 18 or 20 holds in cylindrical section with small diameter 91 by inclined ledge 92 of firing pin 89 with the help of expanding ring 69 which is arranged in external washer-maker 70 and interior washer 68 of igniter block 4 for mechanical extraction. There is magnetic extraction washer-maker 71, which magnetizes to firing pin 89, inside the igniter block 5, which is used for magnetic extraction of ammunition 1 or 6 or 8 or 10 or 12 or 16 or 18 or 20. Between the end face of conical section 90 of the firing pin 89 and a primer with an anvil 67 of igniter block 4,5 a gap 114 is made. The thickness T114 of the gap 114 is 0.03-0.05D, wherein D-outside diameter of the ammunition 1 or 6 or 8 or 10 or 12 or 16 or 18 or 20. The gap 114 between the end face of conical section 90 of the firing pin 89 and a primer with an anvil 67 of igniter block 4,5 doesn't allow to stab primer with anvil 67 by conical section 90 of firing pin 89, what provides reliability of loading and reloading cycle.

[0328] FIG. 51 shows side view of mechanism and FIG. 52—cross-section 1-1 on FIG. 51. Supply of the extractor 95 under the ammunition 1 or 6 or 8 or 10 or 12 or 16 or 18 or 20. During the supply of the extractor 95 under ammunition 1 or 6 or 8 or 10 or 12 or 16 or 18 or 20 lower part 113 of front ledge 87 of lock frame 86 passes along the front inclined area 107 of the lower ledge 106 and comes to beginning of rear horizontal area 108 of lower ledge 106 of the extractor 95. Extractor 95 rotates on shaft 103 and semicircular hollow 97 capture the ledge 31 of ammunition 1 or 6 or 8 or 10 or 12 or 16 or 18 or 20.

[0329] FIG. 53 shows side view of mechanism and FIG. 54—unit C on FIG. 53, FIG. 55—unit C on FIG. 53. Removal of captured ammunition 1 or 6 or 8 or 10 or 12 or 16 or 18 or 20 from bolt 88 with the help of extractor 95 is shown. When the captured ammunition 1 or 6 or 8 or 10 or 12 or 16 or 18 or 20 is being removed, the lower part 113 of the front ledge 87 of the lock frame 86 passes along the rear horizontal platform 108 of the lower ledge 106 and bears against the beginning of the front inclined area 110 of the upper ledge 109 of the extractor 95.

[0330] The semicircular hollow 97 holds the ammunition 1 or 6 or 8 or 10 or 12 or 16 or 18 or 20 in place behind the ledge 31. Meanwhile, for mechanical extraction, inclined ledge 92 of firing pin 89 opens expanding ring 69 and firing pin 89 comes out of engagement with igniter block 4 and conical bushing 93 on bolt 88 gets a gap 115 with the rear end of ammunition 1 or 6 or 8 or 10 or 12 or 16 or 18 or 20. Dining the magnetic extraction conical section 90 of firing pin 89 is beyond the magnetic extraction washer-marker of the igniter block 5, wherein the magnetized magnetic extraction washer-marker 71 tons off from the firing pin 89, and the conical bushing 93 on the bolt 88 gets a gap 115 with the rear end of the ammunition 1 or 6 or 8 or 10 or 12 or 16 or 18 or 20. The thickness T115 of the gap 115 is equal to 0.2D, wherein D-outside diameter of the ammunition 1 or 6 or 8 or 10 or 12 or 16 or 18 or 20. The gap 115 between conical bushing 93 of bolt 88 and rear part of the ammunition 1 or 6 or 8 or 10 or 12 or 16 or 18 or 20 does not allow the rear end of the ammunition 1 or 6 or 8 or 10 or 12 or 16 or 18 or 20 to engage the conical bushing 93 during ejection beyond the weapon, what provides reliability of the loading cycle, reloading cycle.

[0331] FIG. 56 shows side view of mechanism. The ejection of ammunition 1 or 6 or 8 or 10 or 12 or 16 or 18 or 20 by extractor 95 from the weapon is shown. When the ammunition 1 or 6 or 8 or 10 or 12 or 16 or 18 or 20 is ejected by the extractor 95, the lower part 113 of the front ledge 87 of the lock frame 86 passes along the front inclined area 110 of the upper ledge 109, passes through the upper ledge 109, passes along the upper horizontal area 111 of the upper ledge 109, and stops at the end of it. During mentioned process the extractor 95 vigorously rotates on the shaft 103 and ejects the ammunition 1 or 6 or 8 or 10 or 12 or 16 or 18 or 20 from the weapon by semicircular hollow 97.

[0332] During the mechanism work in semi-automatic or automatic mode the lower part 113 of the front ledge 87 of the lock frame 86 only reaches the front inclined area 99 of the extractor 95, thanks to that the extractor 95 does not work during the shooting. Extractor 95 works in extraction of ammunition only during manual reloading what improve the reliability of weapon work in general and the extraction in particular. The reliability of extraction is achieved as expanding ring 69 or magnetic extraction washer-maker 71 take part in extraction once during the ejection of the training ammunition 20 or once during the ejection of the ammunition 1 or 6 or 8 or 10 or 12 or 18, in which the misfire has occurred, and are very simple in construction. The expanding ring 69 can make up to one million opening-closing cycles until failure in operation occurs, the magnetic extraction washer-marker 71 will have been demagnetized during 15 years no more than 5% of the initial magnetization.

[0333] In order to make a shot with the help of the claimed caseless ammunition, it is necessary to have a caseless weapon, which mast have at least such mechanisms as: rifled barrel with cartridge chamber, barrel box, bolt with obturator, firing mechanism with striker, hammer in cocked position, firing spring, trigger, spring-loaded sear.

[0334] Shot is made with the help of claimed caseless ammunition in such way: ammunition is inserted into cartridge chamber of caseless weapon and is locked by bolt with obturator, where the problem of gas obturation in the bolt is solved. When the trigger is pressed, the spring-loaded sear comes out of engagement with the cocked position of the hammer and the hammer vigorously rotates under the action of the firing spring and strikes the striker. Striker fires primer of igniter block in caseles ammunition by its pan, propellant ignites, gases of high temperature and pressure are formed during the ignition of propellant and igniter block, they force shell to fly out of the barrel, rifling, getting axial rotation of the shell which is needed for stabilization of shell flight. There is combustible washer-marker in front of the primer of igniter block and when the washer is being burnt, the released gases pushes the standard primer of igniter block out after the shell. Depending on the purpose, changing the shell, it is possible to achieve a wide variety of tasks in shooting; claimed for invention ammunition can be armor-piercing, tracing, training, etc. If the igniter block is non-combustible, a mechanism of the ejecting of the igniter block is necessary in the weapon.