AU763036B2 - Shrouded aerial bomb - Google Patents

Description

S&FRef: 511910D2

AUSTRALIA

PATENTS ACT 1990 COMPLETE SPECIFICATION FOR A STANDARD PATENT

ORIGINAL

Name and Address of Applicant: Actual Inventor(s): Address for Service: Invention Title: Lockheed Martin Corporation 6801 Rockledge Drive Bethesda Maryland 20817 United States of America Bruce E. Schmaker, Ronald L. Wooten Spruson Ferguson St Martins Tower,Level 31 Market Street Sydney NSW 2000 (CCN 3710000177) Shrouded Aerial Bomb The following statement is a full description of this invention, including the best method of performing it known to me/us:- 5845c SHROUDED AERIAL BOMB The present invention relates to aerial bombs, that is, bombs dropped from aircraft, and more particularly, to aerial bombs for penetrating hard targets.

B3ACKGROUTND A bomb typically includes a hard casing having an interior hollow space for containing an explosive material. The physical characteristics of the bomb, including the weight, center of gravity, moments or inertia, and the aerodynamic shape, all affect the free-fall1 response of the bomb, whether or not a guidance package is included with the bomb.

Bombs delivered from aircraft, including free-fall guided or unguided bombs, 15 glide bombs, and boosted bombs, must pass rigorous field testing which includes the safe release from a deploying aircraft and accuracy of delivery to the target. These tests must be conducted for each type of aircraft that will carry the bomb. The development of new weapons, therefore, is subject to significant delay and expense before the weapon is qualified for use.

The ability of a bomb, or other projectile, to penetrate a target is proportional to the mass and the velocity of impact of the projectile and inversely proportional to the cross-sectional area of the bomb. That is, the greater the kinetic energy and the smaller the cross-sectional area, the greater the penetration that can be expected. To adapt an existing bomb for greater penetration by reducing the exteral diameter of the bomb can also result however, in changes in the mass properties such as weight, center of gravity, moment of inertia, and in the aerodynamic properties, all of which can affect khe flight characteristics of the bomb. These changes also require that the adapted bomb be qualified for use.

Summary of the Invention In a first aspect the present invention provides a shrouded aerial bomb comprising: a penetrating body having a nose section shaped with an ogive and having a hollow bore with an opening at a tail end and extending toward the nose section; and an aerodynamic shroud mounted to an outer surface of the penetrating body, the shroud including at least one clamp mounted to a center portion of the penetrating body, wherein the at least one clamp includes a forward clamp and an aft clamp mounted in longitudinally spaced relationship, each clamp including semi cylindrical parts fastened together to encircle the penetrating body.

In another aspect the present invention provides a shrouded aerial bomb, comprising: a penetrating body having a nose section shaped with an ogive; and an aerodynamic shroud mounted to an outer surface of the penetrating body, the shroud including a forward clamp and an aft clamp mounted to a center portion of the penetrating body in longitudinally spaced relationship, each clamp including two semi-cylindrical parts fastened together to encircle the penetrating body, a nose cone shaped with an ogive, a forward tube fastened to the nose cone and the forward clamp, shells attached between the clamps, and an aft tube fastened to the aft clamp, and a tail tubular section fastened to the aft tube.

More particularly, the preferred bomb has an improved penetrating warhead, that is, a warhead that more deeply penetrates a protected target, however, the shrouded structure of the bomb enables the detailed design of the bomb to provide substantially oooo identical aerodynamic and mass properties to that of a qualified bomb. As a result, the 25 preferred bomb can be readily qualified by similarity of function to the existing bomb for use on an aircraft. In addition, if desired, the preferred bomb can use existing guidance packages available for the qualified bomb.

To avoid lengthy and expensive delays required to qualify a new bomb, the preferred bomb emulates the free-fall properties of an existing bomb pertinent to o• [R:\LIBLL] 12780.doc:ssl:jmt:TCW/klp qualification, while at the same time, providing a warhead with the desired improved penetrating capability.

The preferred warhead is a penetrating body shaped for improved target penetration through a smaller cross-sectional area compared to an existing qualified bomb. An aerodynamic shroud mounted around the warhead emulates the shape of the qualified bomb, and the weight, center of gravity and moments of inertia of the bomb (the penetrating body and shroud) closely approximate those properties of the existing bomb.

Brief Description of the Drawings The invention will be better understood by reference to the following detailed description in conjunction with the appended drawings, in which: Figure 1 is a side view of a bomb in accordance with the invention; i Figure 2 is a side, section view of a penetrating body of the bomb of Figure 1; Figure 3 is a perspective, exploded view of the bomb of Figure 1 illustrating the various components of the shroud assembly and penetrator; Figure 4 is a side view of a bomb with a mounted guidance package; *e [R:\LIBLL] 12780.doc:ssl:jmt:TCW Figure 5 is a sectional view of a nose portion of the shrouded warhead showing attachment structure for a nose guidance unit; Figure 6 is a sectional view of a forward clamp of the shroud; and Figure 7 is a sectional view of a tail of the shroud showing a mounting structure for atail fin unit.

DETAILED DESCRPION Figure 1 is a side view of a shrouded bomb 20 in accordance with a preferred form of the invention. The bomb 20 includes a penetrating body 24 or warhead (shown in Figure 2) and a shaped to emulate the aerodynamic shape of an existing, qualified bomb. In the exemplary embodiment, the bomb 20 is shaped to emulatc the BLtT-1091B bomb, that is, the outer shape of the shroud 40 is substantially identical to the outer shape of the hard case of the BLU-1091B. In addition, the weight, center of gravity, and moments of inertia of the bomb 20 are substantially identical to those physical characteristics of the BLU- 109/B.

The bomb 20 will therefore have the same frnee-fall and aerodynamic properties as the emulated bomb, and. as a result can be carried on any aircraft for which the emulated bomb is qualified. Further, the bomb 20 can be used with any guidance package appropriate for the emulated bomb. The improved bomb 20, however, avoids the lengthy and costly flight qualification tests because it is qualed by similarity to the qualified bomb. The preferred aerial bomb thus improves on the function of an existing bomb, but qualifies for use by emulating the handling and aerial delivery characteristics of the exisl bomb.

The invention is not limited to emulating a particular qualified bomb, such as the BLU-109/B, which is used as an example here, but, as will be appreciated by those skilled in the art from the following description, the invention may be directed to improvements in other existing bombs.

The penetrating body 24 in the illustrative embodiment is designed for improved target penetrating capability. The penetrating body 24 includes a case formed of a hard, dense material, such as steel, tungsten, or'depleted uranium. The penetrating body 24 is narrower than the case of the emulated bomb to provide a smaller cross sectional area.

The penetrating body 24 has an interior hollow space 26 that may contain an explosive.

The space 26 opens at the tail end of thle body 28 and extends toward the nose 30, leaving a solid, nose section. A bulkhead 32 is attached to the penetrating body 24 to close the opening at the tail and to support mounting of a fuze that activates the warhead, as futher described below.

in the example provided of the BLU-109/B as an emulated qualified bomb, the penetrating body 24 is narrower than a BLU-l09fB, but has thicker walls to maintain most of the weight of the BLU- 109/B. According to the exemplary embodiment, the penetrating body 24 has a weight (loaded with an explosive charge) that is between 80% and 90% of the weight of the BLU- 109/B. The reduced diameter with approximately the same weight increases the penetration ability of the penetrating body as compared to the BLU- 109/B by focusing kinetic energy on a smaller impact area. The diameter and weight of the warhead are to be selected, for example, for the penetrating and explosive functions desired, within the constraint of the total weight of the warhead and shroud being approximately equal to that of the emulated weapon.

The penetrating body 24 is shaped at the nose end 30 with an ogive having a variable radius of curvature. The nose end 30 outer shape leads to a cylindrical center portion 34. The outer diameter of the penetrating body 24, measured at the cylindrical center portion 34 is 10.7 inches, as compared to an outer diameter of the BLU-1I09/B of 14.6 inches at a center portion. The thickness of the wall 36 of the penetrating body surrounding the bore 26 is 2.26 inches.

Figure 3 is an exploded view of the shroud 40 and penetrating body 24. The shroud 40 includes a forward clamp 42 and an aft clamp 44 that are fastened to the center portion 34 of the penetrating body 24 in spaced relationship. The clamps 42,44 each are of two-part construction, each having a pair of seinicylindrical members that are bolted together about the penetrating body 24. The clamps 42, 44 are sized on the inner diameter to closely fit the penetrating body 24 to provide supporting locations for ground handling and storage pallets. Shear pins (not illustrated) are mounted in holes in the penetrating body 24 and extend outward therefrom to engage mating holes in the ciamps 42, 44. The shear pins prevent the clamps 42, 44 from moving longitudinally and rotating relative to the penetrating body 24 during ground handling of the bomb and while carried on an aircraft.

Alternatively, other mechanical engagement means could be used to prevent movement of the clamps. 42, 44 on the penetrating body 24. For example, longitudinal grooves formed in the penetrating body 24 could engage ribs extending from the clamps 42, 44, or the outer surface of the penetrating body 24 and the inner surfaces of the clamps 42, 44.could be formed as roughened surface to provide increased friction between the surfaces.

The shear pins and the clamps are designed to have a material strength so that they break under the force of impact of the bomb on a target to help the penetrating body 24 shed the shroud 40 for better penetration into the target The upper part of each clamp 42, 44 includes mounting holes for lugs 48, 50 to mount the bomb on an aircraft hanger system. The spacing of the lugs 48, 50 and their position relative to the center of gravity of the bomb 20 is identical to that for the selected weapon, in the illustrated embodiment, the BLU-1091B.

The shroud 40 also includes skin members that form the outer surface and are shaped to have the aerodynamic characteristics of the emulated bomb. The sin members include a nose cone 60 mounted at the nose 30 of the penetrating body 24, and a forward :tube 62 mounted between the nose cone 60 and the forward clamp 42. The nose cone, and forward tube 62 are fastened together, and the forward tube 62 is fastened to the forward clamp 42. A nose ring 64 helps secure the nose cone 60 in place and provides a mounting structure for a nose guidance unit, shown in Figures 4 and The forward end 61 of the nose cone 60 is cylindrically shaped and extends longtudinaly forward from the penetrating body 24. The forward-extending cylinder end 61 is designed upon impact of the warhead on a target to break away from the I penetrating body 24, to assist the penetrating body 24 in shedding the forward portion of the shroud.

Between the forward clamp 42 and the aft clamp 44, an upper shell 70 and a lower shell 72 are fastened. The lower shell 72 is made sufficiently thick, typically about inches, to help support the weight of the bomb during ground handling by conventional lift equipment, and for resting the bomb on storage pallets. The upper shell 70 includes a switch plate 74 which cooperates with a release-indicating switch on the aircraft, which is used to signal the release of the bomb from an aircraft.

Rearward of the aft clamp 4,the skin is completed by an aft tube 76 and a tail tube 78. In the illustrated embodiment, the tail tube 78 flares outward to emulate the tail *~sh ape ofthe BLU-109/B. A tail ring 80 is fastened on the tail end of the bomb and the shroud, and provides a mounting structure for an aerodynamic tail unit; exemplary tail .units are shown in Figures 4 and 7.

15 Te clamps 42, 44 provide support for ground handling and storage of the bomb on racks, pallets and lifts. Additional support is provided by support rings which are installed between the penetrating body 24 and the skin elements at the support locations 82, 83 shown by the arrows. The support rings may, for example, be or "IT' profiled rings, and are positioned to bridge the space between the skin and the penetrating body 24 to help support the weight of the body.

The unit 20 shown in Figure 1 is designed to have the same length, weight, center *.of gravity, and aerodynamic shape of the selected, qualfed weapon. As will be appreciated by those skilled in the art, the weight and center of grvity can be adjusted by ballasting the penetrating body 24 or the shroud 40, by the addition or removal of material at selected locations. For example, the length of the bore 26, or the thickness of the penetrating body walls 36 can be readily changed to adjust the weight and center of gravity. The shroud components, in particular, the clamps 42, 44, may also be adapted in weight and/or size to adjust the center of gravity and total weight Figure 4 is a side view of the shrouded bomb 20 with a guidance package attahed. The guidance package includes a nose guidance unit 102 having target sensing devices (not illustrated), and a tail fin unit 104. The nose guidance unit 102 has fins 106 that are controllable by the nose guidance unit 102 for steering the bomb during frec-fail and a folding fin stabilization assembly. The guidance package, including the fins, does not form a part of this invention, except that the shroud is designed to accept mounting of a guidance package, as explained below.

As shown in Figure 5, the nose ring 64 sits on the nose end of the penetrating body 24, and is fastened to the front end of the penetrating body and to the nose cone of the shroud. The nose ring 64 includes a circumferential groove 66 that accepts a mating rib 103 of the nose unit 102. A retaining ring 68 secures the nose unit 102 to the nose ring 64.

Figure 7 illustrates a tail fin mounting arrangement The tail ring 80 includes a vshaped groove 84 that mates with a conventional ring clamp (not shown) of a tail fin unit fuze 110 is installed in the tail end of the penetrating body 24. To activate the *fuze 110, a power generator 45, a wind-driven turbine, is mounted in a seat 46 in the part of the forward clamp 42. The generator 45 is active when the bomb is in freefall togenerate electric power to activate the fuze 110. A cable 49 to connect the generator 45 to the fuze 110 is routed in a space between the shroud 40 and the penetrating body 24, thus passing under the mid shell 70, along the aft clamp 44 and under the aft tube 76 and tail tube 78. The cable 49 is then routed through a hole in the tail ring 80 and into the tail end of the penetrating body 24. A safe/arm device may be included with the fuze 1 10, and mounted in proximity to the fuze 110 within or on. the shroud The fuze 110 and power generator 45 are not a part of the bomb except that the warhead is designed to accommodate fuzing systems. Other suitable fuzing systems could be used with the bomb.

The invention has been described in terms of preferred emibodiments, principles, and examples. Those skilled in thie art will recognize that substitutions and equivalents may be made without departing from the scope of the invention as defined in the following claims.

Claims (3)

1. A shrouded aerial bomb comprising: a penetrating body having a nose section shaped with an ogive and having a hollow bore with an opening at a tail end and extending toward the nose section; and an aerodynamic shroud mounted to an outer surface of the penetrating body, the shroud including at least one clamp mounted to a center portion of the penetrating body, wherein the at least one clamp includes a forward clamp and an aft clamp mounted in longitudinally spaced relationship, each clamp including semi cylindrical parts fastened together to encircle the penetrating body.

2. A shrouded aerial bomb, comprising: a penetrating body having a nose section shaped with an ogive; and an aerodynamic shroud mounted to an outer surface of the penetrating body, the shroud including a forward clamp and an aft clamp mounted to a center portion of the penetrating body in longitudinally spaced relationship, each clamp including two semi-cylindrical parts fastened together to encircle the penetrating body, a nose cone shaped with an ogive, a forward tube fastened to the nose cone and the forward clamp, shells attached between the clamps, and an aft tube fastened to the aft clamp, and a tail tubular section fastened to the aft tube.

3. A shrouded aerial bomb, substantially as hereinbefore described with reference to the accompanying drawings. Dated 8 May, 2003 Lockheed Martin Corporation o Patent Attorneys for the Applicant/Nominated Person SPRUSON FERGUSON a.. o0•0 00•0 [R:\LIBLL] 1 2780.doc:ssI:jmt:TCW/klp