EP0426627A2 - Ammunition impact fuse - Google Patents

Ammunition impact fuse Download PDF

Info

Publication number
EP0426627A2
EP0426627A2 EP90850279A EP90850279A EP0426627A2 EP 0426627 A2 EP0426627 A2 EP 0426627A2 EP 90850279 A EP90850279 A EP 90850279A EP 90850279 A EP90850279 A EP 90850279A EP 0426627 A2 EP0426627 A2 EP 0426627A2
Authority
EP
European Patent Office
Prior art keywords
locking member
barrier
armament
safety
arrangement according
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.)
Withdrawn
Application number
EP90850279A
Other languages
German (de)
French (fr)
Other versions
EP0426627A3 (en
Inventor
Bengt Carlsson
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.)
Saab Bofors AB
Original Assignee
Bofors AB
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 Bofors AB filed Critical Bofors AB
Publication of EP0426627A2 publication Critical patent/EP0426627A2/en
Publication of EP0426627A3 publication Critical patent/EP0426627A3/en
Withdrawn legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C1/00Impact fuzes, i.e. fuzes actuated only by ammunition impact
    • F42C1/02Impact fuzes, i.e. fuzes actuated only by ammunition impact with firing-pin structurally combined with fuze
    • F42C1/08Impact fuzes, i.e. fuzes actuated only by ammunition impact with firing-pin structurally combined with fuze with delayed action after ignition of fuze or after impact
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C19/00Details of fuzes

Definitions

  • the present invention relates to an arrangement primarily for a long ammunition unit having a fuze function which is sensitive to impact on both soft and hard targets.
  • the ammunition unit is also provided with a front barrier which effects piercing of a hard target, when the ammuni­tion unit penetrates the latter, before triggering of the charge carried.
  • the fuze function comprises a safety and armament part mounted behind the barrier and in the latter and/or in a part connected to the barrier.
  • the ammunition units concerned are chiefly in the form of shells.
  • the invention is particularly applicable to shells of high velocity, for example 500 m/s or higher.
  • the shell is of the type which can penetrate thick targets.
  • the invention is a further development of the shell which is described in Swedish Patent 85 02575-7, which corres­ponds to American Patent 4,690,057.
  • This shell is intended for use against both soft and hard targets.
  • the shell comprises a front barrier of hard material and a fuze part which extends in front of this barrier.
  • the shell also comprises a safety and armament part which is included in or is acted upon by the said fuze function.
  • the armament and safety part is mounted in the barrier.
  • shells of the present type func­tion unreliably upon impact against hard targets in cases where the shell is to be designed relatively long, for example with lengths of approximately 1 metre and above.
  • the said lengths may apply especially in the case of large calibres.
  • the shell may function incorrectly upon impact against a hard target.
  • the safety and armament part In this type of shell, which is to function against both soft and hard targets, it is important for the safety and armament part to be arranged in such a way that undesirable ignitions do not occur.
  • the incorporation of percussion ignition is essential in this context.
  • the safety and armament part was anchored by means of a threaded coupling which it was found could not hold during the said expansion movement of the shell.
  • the safety and armament part can become inclined in its bearing when a threaded coupling of this type breaks. This inclination acts undesirably on the ignition func­tion and results in the said unreliability in initiation of the charge carried.
  • the centring of the safety and armament part can be maintained throughout the entire functioning time of the shell in order to permit a reliable and accurate triggering of the charge carried.
  • the safety and armament part executes a slight movement, for example a movement of approximately 2.0 mm, relative to the other part of the shell/the barrier.
  • the main aim of the present invention is to solve the abovementioned problems, and it provides details regard­ing a bearing function for the safety and armament part in which a substantially maintained centring of the safety and armament part is obtained throughout the entire functioning time of the shell, even if this is achieved at the expense of a slight relative longitudinal displacement movement between the safety and armament part and the barrier, or part connected to the barrier.
  • the feature which may principally be regarded as charac­terizing the new arrangement is that the safety and armament part is fixed in its longitudinal displacement direction by means of a locking member which is designed to yield when the ammunition unit, after striking the target (which causes a certain compression of the ammuni­tion unit in its longitudinal direction), undergoes rearward compression/expands and thus causes a relative movement between the barrier or the part connected to it and the safety and armament part.
  • a further charac­teristic is that the bearing of the safety and armament part is designed to permit, after the locking member yields, the relative movement between the barrier and the part connected to it while simultaneously retaining the centring of the safety and armament part in the ammuni­tion unit.
  • the locking member comprises an annular element which is designed to withstand accelera­tion forces occurring in the ammunition unit when the latter strikes the target.
  • the locking member is more­over provided with a projecting flange which is designed to be sheared off by the barrier, or the part connected to it, when the said rearward compression or expansion occurs.
  • a space is in this respect arranged in front of the shear-off part which can be displaced into the space without disturbing the said centring function.
  • the locking member is held in position with the aid of a sleeve-shaped nut member which fixes the locking member in its position where the said shearing-­off can take place.
  • the locking member can have an L-shaped longitudinal section and comprises a part extending in the longitudinal direction of the ammunition unit and a part at an angle relative to the latter part and thus forming the shear-off part.
  • the retaining member is designed with an arrow-shaped longitudinal section which connects to a part in the shape of the shaft of an arrow.
  • the part in the shape of the shaft of an arrow extends in the longitudinal direction of the ammunition part, and this part and the part of the locking member extending in the longitudinal direction of the ammunition part have essentially the same outer diameters.
  • the said arrow-­shaped part constitutes a delimiting part for the said space which will permit the shearing-off and the relative movement.
  • a part is connected to the barrier and effects the shearing-off of the shear-off part of the locking member via a front surface.
  • the part connected to the barrier has an inner diameter which slightly exceeds the said outer diameters of the locking and retaining members.
  • the locking member is mounted threadlessly on an outer surface of the safety and armament part.
  • the retaining member is screwed securely on the safety and armament part via a threaded coupling and bears with one end surface against the locking member.
  • the part connected to the barrier is threadlessly mounted on bearing sur­faces on the safety and armament part and the locking member.
  • the safety and armament part is designed with a pliant section at one surface which bears against a corresponding inner surface of the part connected to the barrier.
  • the pliant section yields at accelerations above a predetermined value in order to prevent inappro­priate actuation of the locking member upon impact of the ammunition unit on the target.
  • the yielding is of the order of magnitude of 0.5-1.0 mm.
  • a simple shear-off part can thus be designed as well as a space which permits the said shearing-off and relative movement.
  • the parts of the fuze function which operate with great accuracy can be kept intact and are not disturbed by the new bearing principle for the safety and armament part. In all cases this can provide a distinct trigger function where, for example, undesirable gas leakage due to the said expan­sion phenomenon in the shell is prevented.
  • the shell comprises a barrier or piercing part 2 for hard as well as soft targets.
  • the fuze function therefore comprises a front part 3 which is situated in front of the barrier and is contained in a nose cone 1a.
  • a part 4 is connected to the barrier, which part is joined to the barrier via a threaded coupling 5.
  • a safety and armament part 6 In the rear part of the barrier and at the said part 4 there is mounted a safety and armament part 6.
  • the safety and armament part comprises a delay primer charge 7, a detonator cap safety 8 and a bottom charge 9.
  • a primer charge 10 which constitutes a reinforcement of the flame which occurs in a central channel 11 through the barrier 2 when the initiation charge 12 is initiated from the percussion cap 13 in the nose of the shell or upon direct impact against a hard target.
  • a locking member in the form of an annular locking element 14 is arranged at the front parts of the part 6. The locking member 14 is held in position by means of a sleeve-shaped nut element 15. The nut-shaped element is screwed securely via a threaded coupling 16 on the front section of part 6. The front end surface of the element 15 bears against an inner wall 2a of the barrier via an elastic member 17.
  • the part 4 is designed with different outer diameters, and the section 4a with the smaller outer diameter is in cooperation with the locking member 14.
  • the section 4b with the larger outer diameter of part 4 partially surrounds an outer surface 6a of part 6.
  • the locking member 14 is designed with an L-shaped longitudinal section, the locking member having a part 14a which extends in the longitudinal direction of the shell and a part 14b which is at an angle relative to the part 14a.
  • the part 6 is provided with an outer surface 6b which is recessed relative to the surface 6a and serves as a bearing surface for section 4a of part 4.
  • the part 6 also has a transverse surface 6c which fini­shes the said bearing surface 6b.
  • the transverse surface constitutes a surface fixing the longitudinal position for the locking member 14 which bears against the stop surface 6c via an end surface on its part 14a.
  • the part 14a of the locking member 14 has an outer diameter which corresponds essentially to the outer diameter of 6b. In this way the locking member part 14a can function as a bearing surface for the section 4a of part 4.
  • Part 4 is also provided with an end surface 14c which bears against the angled part 14b.
  • Part 4 also comprises a transverse surface 4d which bears against a corresponding rear end surface of the barrier 2 in order to define the relative positions of the barrier and the part 4.
  • the nut-shaped element 15 is provided with an arrow-shaped part 15a and a part 15b in the shape of an arrow shaft.
  • the element 15 cooperates with the locking member via an end surface 15c of part 15b.
  • the part in the shape of an arrow shaft has an outer surface with an outer diameter which cor­responds essentially to the outer diameters of the surfaces 6b and section 14a. Behind the arrow-shaped part 15a there is a space (annular) which is delimited at the front by the arrow-shaped part 15a and at the rear by the angled part 14b of the locking member 14.
  • the locking member is made of a material which affords a distinct shearing-off capacity. An example which may be mentioned is light metal BML79, which is a material with distinct shearing properties.
  • the front surface 4c of section 4a is used as a shearing element for the angled part 14b.
  • the material of part 4 is a hard material cor­responding to that of the barrier 2.
  • the shell expands after penetrating a target 19, the forces of inertia in the safety and armament part result in the barrier 2 and the part 4 moving forwards relative to the part 6.
  • the part 4 thus comes to shear off the angled part 14b which can move in the space 18.
  • the shearing-off takes place distinctly and the part 4 also acquires a bearing on the remaining part of 14a and parts of the part 15b formed in the shape of an arrow shaft.
  • the centring of the part 6 can therefore be retained with great accuracy.
  • the movement is of the order of magnitude of approximately 2.0 mm. The retained centring ensures a good triggering function.
  • the part 6 is provided with an inner transverse surface 6d which is set opposite an inner corresponding surface 4d of part 4.
  • the part 6 is provided with a pliant section 6e at the said surface 6d.
  • the said pliant section will yield upon impact forces of a predetermined magnitude in such a way that the angled part 14b is not inappropriately subjected to actuation forces in conjunc­tion with the striking of the target.
  • the movement of the yield is 0.5-1.0 mm.

Abstract

An ammunition unit (1) is provided with a fuze function which is sensitive to impact on both soft and hard targets (19) and comprises a front barrier (2) which effects piercing of a hard target. Mounted behind the barrier is a safety and armament part (6). This is fixed in its longitudinal displacement direction by means of a locking member (14). The locking member yields when the ammunition unit, after striking the target (which causes a certain compression of the ammunition unit in its longitudinal direction), undergoes rearward compression and thus causes a relative movement between the barrier of the part connected to it and the safety and armament part (6). A relative movement is permitted between the safety and armament part and the other parts of the shell, with simultaneous retention of the centring of the safety and armament part in the ammunition unit.

Description

    TECHNICAL FIELD
  • The present invention relates to an arrangement primarily for a long ammunition unit having a fuze function which is sensitive to impact on both soft and hard targets. The ammunition unit is also provided with a front barrier which effects piercing of a hard target, when the ammuni­tion unit penetrates the latter, before triggering of the charge carried. The fuze function comprises a safety and armament part mounted behind the barrier and in the latter and/or in a part connected to the barrier. The ammunition units concerned are chiefly in the form of shells. The invention is particularly applicable to shells of high velocity, for example 500 m/s or higher. Moreover, the shell is of the type which can penetrate thick targets.
  • PRIOR ART
  • The invention is a further development of the shell which is described in Swedish Patent 85 02575-7, which corres­ponds to American Patent 4,690,057. This shell is intended for use against both soft and hard targets. The shell comprises a front barrier of hard material and a fuze part which extends in front of this barrier. The shell also comprises a safety and armament part which is included in or is acted upon by the said fuze function. The armament and safety part is mounted in the barrier.
  • DESCRIPTION OF THE INVENTION TECHNICAL PROBLEM
  • It has been found that shells of the present type func­tion unreliably upon impact against hard targets in cases where the shell is to be designed relatively long, for example with lengths of approximately 1 metre and above. The said lengths may apply especially in the case of large calibres. In connection with the starting point of the invention, it was discovered that the shell may function incorrectly upon impact against a hard target. When the problems surrounding the strike functions against hard targets were analysed, it was observed that, because of its length, the shell on the one hand under­goes a certain compression movement upon impact itself and, on the other hand, executes a subsequent expansion movement when the piercing is complete and the shell is on its way into the target. In this type of shell, which is to function against both soft and hard targets, it is important for the safety and armament part to be arranged in such a way that undesirable ignitions do not occur. Among other things, the incorporation of percussion ignition is essential in this context. In the earlier construction, the safety and armament part was anchored by means of a threaded coupling which it was found could not hold during the said expansion movement of the shell. The safety and armament part can become inclined in its bearing when a threaded coupling of this type breaks. This inclination acts undesirably on the ignition func­tion and results in the said unreliability in initiation of the charge carried.
  • It is important that the centring of the safety and armament part can be maintained throughout the entire functioning time of the shell in order to permit a reliable and accurate triggering of the charge carried. In this connection it is of no importance if the safety and armament part executes a slight movement, for example a movement of approximately 2.0 mm, relative to the other part of the shell/the barrier.
  • SOLUTION
  • The main aim of the present invention is to solve the abovementioned problems, and it provides details regard­ing a bearing function for the safety and armament part in which a substantially maintained centring of the safety and armament part is obtained throughout the entire functioning time of the shell, even if this is achieved at the expense of a slight relative longitudinal displacement movement between the safety and armament part and the barrier, or part connected to the barrier.
  • The feature which may principally be regarded as charac­terizing the new arrangement is that the safety and armament part is fixed in its longitudinal displacement direction by means of a locking member which is designed to yield when the ammunition unit, after striking the target (which causes a certain compression of the ammuni­tion unit in its longitudinal direction), undergoes rearward compression/expands and thus causes a relative movement between the barrier or the part connected to it and the safety and armament part. A further charac­teristic is that the bearing of the safety and armament part is designed to permit, after the locking member yields, the relative movement between the barrier and the part connected to it while simultaneously retaining the centring of the safety and armament part in the ammuni­tion unit.
  • In a preferred embodiment the locking member comprises an annular element which is designed to withstand accelera­tion forces occurring in the ammunition unit when the latter strikes the target. The locking member is more­over provided with a projecting flange which is designed to be sheared off by the barrier, or the part connected to it, when the said rearward compression or expansion occurs. A space is in this respect arranged in front of the shear-off part which can be displaced into the space without disturbing the said centring function. In one embodiment, the locking member is held in position with the aid of a sleeve-shaped nut member which fixes the locking member in its position where the said shearing-­off can take place. The locking member can have an L-shaped longitudinal section and comprises a part extending in the longitudinal direction of the ammunition unit and a part at an angle relative to the latter part and thus forming the shear-off part.
  • In another embodiment the retaining member is designed with an arrow-shaped longitudinal section which connects to a part in the shape of the shaft of an arrow. The part in the shape of the shaft of an arrow extends in the longitudinal direction of the ammunition part, and this part and the part of the locking member extending in the longitudinal direction of the ammunition part have essentially the same outer diameters. The said arrow-­shaped part constitutes a delimiting part for the said space which will permit the shearing-off and the relative movement.
  • In one embodiment, a part is connected to the barrier and effects the shearing-off of the shear-off part of the locking member via a front surface. The part connected to the barrier has an inner diameter which slightly exceeds the said outer diameters of the locking and retaining members.
  • The locking member is mounted threadlessly on an outer surface of the safety and armament part. The retaining member is screwed securely on the safety and armament part via a threaded coupling and bears with one end surface against the locking member. The part connected to the barrier is threadlessly mounted on bearing sur­faces on the safety and armament part and the locking member. The safety and armament part is designed with a pliant section at one surface which bears against a corresponding inner surface of the part connected to the barrier. The pliant section yields at accelerations above a predetermined value in order to prevent inappro­priate actuation of the locking member upon impact of the ammunition unit on the target. The yielding is of the order of magnitude of 0.5-1.0 mm.
  • ADVANTAGES
  • The above proposal provides a technically simple solution to the above problems. A simple shear-off part can thus be designed as well as a space which permits the said shearing-off and relative movement. The parts of the fuze function which operate with great accuracy can be kept intact and are not disturbed by the new bearing principle for the safety and armament part. In all cases this can provide a distinct trigger function where, for example, undesirable gas leakage due to the said expan­sion phenomenon in the shell is prevented.
  • DESCRIPTION OF FIGURES
  • A presently proposed embodiment of an arrangement which has the features significant to the invention will be described hereinbelow with reference to the attached drawing in which
    the figure shows, in a longitudinal section, the front parts of a shell which uses the new bearing principle for the safety and armament part.
  • PREFERRED EMBODIMENT
  • Since the function and construction of the shell are well known per se, they will not be described in any great detail here, but only to the extent that they are relevant to the invention. The shell comprises a barrier or piercing part 2 for hard as well as soft targets. The fuze function therefore comprises a front part 3 which is situated in front of the barrier and is contained in a nose cone 1a. A part 4 is connected to the barrier, which part is joined to the barrier via a threaded coupling 5. In the rear part of the barrier and at the said part 4 there is mounted a safety and armament part 6. The safety and armament part comprises a delay primer charge 7, a detonator cap safety 8 and a bottom charge 9. At the front part of part 6 there is a primer charge 10 which constitutes a reinforcement of the flame which occurs in a central channel 11 through the barrier 2 when the initiation charge 12 is initiated from the percussion cap 13 in the nose of the shell or upon direct impact against a hard target. A locking member in the form of an annular locking element 14 is arranged at the front parts of the part 6.
    The locking member 14 is held in position by means of a sleeve-shaped nut element 15. The nut-shaped element is screwed securely via a threaded coupling 16 on the front section of part 6. The front end surface of the element 15 bears against an inner wall 2a of the barrier via an elastic member 17. The part 4 is designed with different outer diameters, and the section 4a with the smaller outer diameter is in cooperation with the locking member 14. The section 4b with the larger outer diameter of part 4 partially surrounds an outer surface 6a of part 6. The locking member 14 is designed with an L-shaped longitudinal section, the locking member having a part 14a which extends in the longitudinal direction of the shell and a part 14b which is at an angle relative to the part 14a. The part 6 is provided with an outer surface 6b which is recessed relative to the surface 6a and serves as a bearing surface for section 4a of part 4. The part 6 also has a transverse surface 6c which fini­shes the said bearing surface 6b. The transverse surface constitutes a surface fixing the longitudinal position for the locking member 14 which bears against the stop surface 6c via an end surface on its part 14a. The part 14a of the locking member 14 has an outer diameter which corresponds essentially to the outer diameter of 6b. In this way the locking member part 14a can function as a bearing surface for the section 4a of part 4. Part 4 is also provided with an end surface 14c which bears against the angled part 14b. Part 4 also comprises a transverse surface 4d which bears against a corresponding rear end surface of the barrier 2 in order to define the relative positions of the barrier and the part 4. The nut-shaped element 15 is provided with an arrow-shaped part 15a and a part 15b in the shape of an arrow shaft. The element 15 cooperates with the locking member via an end surface 15c of part 15b. The part in the shape of an arrow shaft has an outer surface with an outer diameter which cor­responds essentially to the outer diameters of the surfaces 6b and section 14a. Behind the arrow-shaped part 15a there is a space (annular) which is delimited at the front by the arrow-shaped part 15a and at the rear by the angled part 14b of the locking member 14. The locking member is made of a material which affords a distinct shearing-off capacity. An example which may be mentioned is light metal BML79, which is a material with distinct shearing properties. The front surface 4c of section 4a is used as a shearing element for the angled part 14b. The material of part 4 is a hard material cor­responding to that of the barrier 2.
  • When the shell expands after penetrating a target 19, the forces of inertia in the safety and armament part result in the barrier 2 and the part 4 moving forwards relative to the part 6. The part 4 thus comes to shear off the angled part 14b which can move in the space 18. In accordance with the above, the shearing-off takes place distinctly and the part 4 also acquires a bearing on the remaining part of 14a and parts of the part 15b formed in the shape of an arrow shaft. The centring of the part 6 can therefore be retained with great accuracy. The movement is of the order of magnitude of approximately 2.0 mm. The retained centring ensures a good triggering function.
  • The part 6 is provided with an inner transverse surface 6d which is set opposite an inner corresponding surface 4d of part 4. The part 6 is provided with a pliant section 6e at the said surface 6d. The said pliant section will yield upon impact forces of a predetermined magnitude in such a way that the angled part 14b is not inappropriately subjected to actuation forces in conjunc­tion with the striking of the target. The movement of the yield is 0.5-1.0 mm.
  • The invention is not limited to the embodiment illus­trated above as an example, but instead can be modified within the scope of the following patent claims and the inventive concept.

Claims (10)

1. Arrangement primarily for a long ammunition unit (1) having a fuze function sensitive to impact on both soft and hard targets (19) having a front barrier (2) which effects piercing of a hard target, when the ammuni­tion unit penetrates the latter, before triggering of the charge carried, in which respect the fuze function comprises a safety and armament part (6) which is mounted behind the barrier and in the latter, and/or in a part (4) connected to the barrier, characterized in that the safety and armament part is fixed in its longitudinal displacement direction by means of a locking member (14) which is designed to withstand acceleration forces occurring in the ammunition unit when it strikes the target and which is designed to yield when the ammunition unit, after striking the target (which causes a certain compression of the ammunition unit in its longitudinal direction), undergoes rearward compression/expands and thus causes a relative movement between the barrier or the part (4) connected to it and the safety and armament part (6), and in that the bearing of the safety and armament part is designed to permit, after the locking member yields, the relative movement between the barrier and the part (4) connected to it while simultaneously retaining the centring of the safety and armament part in the ammunition unit.
2. Arrangement according to patent claim 1, charac­terized in that the locking member (14) comprises an annular element which is provided with a projecting flange (14b) which is designed to be sheared-off by the barrier, or the part connected to it, when the said rearward compression/expansion occurs.
3. Arrangement according to patent claim 2, characterized in that a space (18) is arranged in front of the projecting flange or the shear-off part, which space receives the sheared-off flange or the part and permits the relative movement.
4. Arrangement according to patent claim 1, 2 or 3, characterized in that the locking member can cooperate with a sleeve-shaped retaining member (15) which holds the locking member (14) in a fixed position where it permits shearing-off of the projecting part of the locking member.
5. Arrangement according to any one of the preceding patent claims, characterized in that the locking member has an L-shaped longitudinal section with a part (14a) extending in the longitudinal direction of the ammunition unit and a part (14b) at an angle relative to the latter part.
6. Arrangement according to patent claim 5, charac­terized in that the retaining member has an essentially arrow-shaped longitudinal section (15b) which connects to a part (15b) in the shape of an arrow shaft, in that the part in the shape of an arrow shaft extends in the longitudinal direction of the ammunition unit, in that the part in the shape of an arrow shaft and the part (14a) of the locking member extending in the longitudinal direction of the ammunition part have essentially the same outer diameters, in that the angled part on the locking member can shear-off upon the relative movement, and in that, when the part is sheared off, it moves in the space (18) which is delimited at the front by the said arrow-shaped part (15a).
7. Arrangement according to patent claim 5 or 6, characterized in that the part (4) connected to the barrier effects the shearing-off of the shear-off part of the locking member via a front surface (4c) which, before the relative movement occurs, bears against the said shear-off part, and in that the part connected to the barrier has an inner diameter which slightly exceeds the said outer diameters of the locking and retaining mem­bers.
8. Arrangement according to any one of the preceding patent claims, characterized in that the locking member is threadlessly mounted on an outer surface of the safety and armament part, in that the retaining member is secured on the safety and armament part via a threaded coupling (16), and in that the part connected to the barrier is threadlessly mounted on bearing surfaces on the safety and armament part and the locking member.
9. Arrangement according to any one of the preceding patent claims, characterized in that the safety and armament part is designed with a pliant section (6e) at a surface (6d) which bears against a corresponding inner surface on the part connection to the barrier, and in that the pliant section yields at acceleration beyond a predetermined value in order to prevent undesirable actuation of the locking member upon impact on the target.
10. Arrangement according to patent claim 9, charac­terized in that the said surfaces (4e and 6e) consist of an internal collar surface and a shoulder surface situated behind the locking member.
EP19900850279 1989-08-25 1990-08-15 Ammunition impact fuse Withdrawn EP0426627A3 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SE8902822A SE463436B (en) 1989-08-25 1989-08-25 DEVICE WITH PRIORLY LONG AMMUNITION UNIT WITH TEMPERATURE FUNCTION SENSITIVELY BEFORE HAVING SUFFICIENT SOFT SOFT TARGETS
SE8902822 1989-08-25

Publications (2)

Publication Number Publication Date
EP0426627A2 true EP0426627A2 (en) 1991-05-08
EP0426627A3 EP0426627A3 (en) 1992-04-29

Family

ID=20376733

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19900850279 Withdrawn EP0426627A3 (en) 1989-08-25 1990-08-15 Ammunition impact fuse

Country Status (2)

Country Link
EP (1) EP0426627A3 (en)
SE (1) SE463436B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6489480B2 (en) 1999-12-09 2002-12-03 Exxonmobil Chemical Patents Inc. Group-15 cationic compounds for olefin polymerization catalysts
FR2872274A1 (en) * 2004-06-25 2005-12-30 Tda Armements Sas Soc Par Acti SHIELD-SHIELD AND PROJECTILE, IN PARTICULAR AN OBUS, EQUIPPED WITH SUCH A CLOISON

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB159771A (en) * 1920-04-06 1921-03-10 John Bonner Semple Selectively acting projectile fuses
CH148799A (en) * 1930-08-07 1931-08-15 Schwob Freres & Cie Sa Self-delayed mechanical percussion fuze for projectiles.
GB2006397A (en) * 1977-10-12 1979-05-02 Oerlikon Buehrle Ag Projectile
FR2522405A1 (en) * 1982-02-26 1983-09-02 Meca Ste Nle Et Base fuse for rifle grenade - is percussion type fired dynamically with safety lock

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB159771A (en) * 1920-04-06 1921-03-10 John Bonner Semple Selectively acting projectile fuses
CH148799A (en) * 1930-08-07 1931-08-15 Schwob Freres & Cie Sa Self-delayed mechanical percussion fuze for projectiles.
GB2006397A (en) * 1977-10-12 1979-05-02 Oerlikon Buehrle Ag Projectile
FR2522405A1 (en) * 1982-02-26 1983-09-02 Meca Ste Nle Et Base fuse for rifle grenade - is percussion type fired dynamically with safety lock

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6489480B2 (en) 1999-12-09 2002-12-03 Exxonmobil Chemical Patents Inc. Group-15 cationic compounds for olefin polymerization catalysts
FR2872274A1 (en) * 2004-06-25 2005-12-30 Tda Armements Sas Soc Par Acti SHIELD-SHIELD AND PROJECTILE, IN PARTICULAR AN OBUS, EQUIPPED WITH SUCH A CLOISON
WO2006000575A1 (en) * 2004-06-25 2006-01-05 Tda Armements S.A.S. Shield and a projectile, such as a shell, which is equipped with one such shield
US7493860B2 (en) 2004-06-25 2009-02-24 Tda Armements S.A.S. Projectile, such as a shell, which is equipped with a bulkhead shield

Also Published As

Publication number Publication date
SE463436B (en) 1990-11-19
SE8902822D0 (en) 1989-08-25
SE8902822A (en) 1990-11-19
EP0426627A3 (en) 1992-04-29

Similar Documents

Publication Publication Date Title
IL107769A (en) Tandem charge warhead with piezoelectrical fuses
GB2089946A (en) A practice projectile
US4480551A (en) Point-detonating variable time-delayed fuze
US3576165A (en) Safety projectile percussion primer
US3994230A (en) Self-destruction type nose impact fuze for spinning projectiles
US4242964A (en) Explosive fuse for projectile
US2619905A (en) Impact fuse for rocket projectiles
US2705921A (en) Fuze for non-rotating shaped charge projectiles
EP0426627A2 (en) Ammunition impact fuse
US5591935A (en) Shock sensing dual mode warhead
CA3091710C (en) Projectile having a pyrotechnic charge
US3119336A (en) Fuze for an explosive projectile
US20010054365A1 (en) Safety device for a pyrotechnic impact fuse of a ballistic high explosive shell
US4449456A (en) Safety device for a projectile
US3351018A (en) Percussion fuze
US3177810A (en) Impact fuze
CA1308605C (en) Shotgun cartridge with explosive shell
US2455603A (en) Fuse
JPS59157499A (en) Warhead fuse
EP0097911B1 (en) Projectile fuze
US1648603A (en) Detonating fuse
US3980021A (en) Projectile having at least two charges
US2173620A (en) Combination projectile fuse
US5355801A (en) Small caliber fuze with arming delay, second impact and graze sensitivity
US4693180A (en) Impact detonator with a detonator cap

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): DE FR IT

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): DE FR IT

17P Request for examination filed

Effective date: 19920825

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 19940301