Dumping and Arming Systems

Abstract

A disarming device for a storage unit is provided, the device comprising a first attachment system and a second attachment system, an interlocking connector coupled to the first attachment system and the second attachment system, and a disarming clip, wherein each of the first attachment system and the second attachment system comprises a first frangible connector coupled to the disarming unit and the interlocking connector, and a second frangible connector coupled to the interlocking connector and the storage unit. The interlocking connector is coupled to the first attachment system via a first coupling arrangement and to the second attachment system via a second coupling arrangement, wherein the first coupling arrangement and the second coupling arrangement are different. The first coupling arrangement and the second coupling arrangement are manually secured.

Description

[Technical field]

[0001] The present invention relates generally to arming devices, and more particularly to arming devices for use in storage of ammunition projectiles and the like. [Background technology]

[0002] The ejector release unit is typically installed on an aircraft pylon or an aircraft internal bay and is used for the transport and release of a storage unit, such as an ammunition projectile. The storage unit may be carried on the ejector release unit by two suspension hooks that engage with two storage unit mounting suspension lugs. The ejector release unit may comprise a cartridge actuated device or a pressurized gas device. When the ejector release unit is activated or operated, it releases the suspension hooks and operates a piston within the ejector release unit, which effectively "pushes" the storage unit away from the aircraft, ensuring that the storage unit does not collide with the aircraft structure upon release. Other coupling mechanisms to the hanging hooks may actually be used, for example the storage unit may be placed on a selectively collapsible shelf.

[0003] A particular fuze (sometimes called a "fuze") system for a canister may have a combination of electrical and mechanical inputs required for actuation (i.e., first and second fuze inputs, respectively). Typically, for safety reasons, electrical power is not usually available in the fuze system prior to the release of the canister, and therefore power must be supplied from the aircraft during release or generated by the canister after release.

[0004] In one example, the supply of power is achieved via inductive transfer of energy from outside the fuze system and outside the containment to the fuze system within the containment. Alternatively, a hardwired connection may be used for the transfer of power, for example in the form of a plug and socket like arrangement or contact pins etc. In one example, the fuze system includes a deployable wind turbine operable to generate electricity via rotating a wind turbine rotor to activate an electrical input of the fuze system.

[0005] The wind turbine is deployed to be deployed during the release of the storage unit. However, it is difficult to ensure that the wind turbine is deployed by the lanyard at an acceptable angle. If the wind turbine is deployed outside of the acceptable parameters, it will not operate correctly and may be damaged. Existing solutions require long lanyards to achieve this.

[0006] In addition, additional retaining wires are required to ensure that the lanyard is released with the storage unit after it is activated, which leads to increased complexity. These additional wires and the arming connector need to be correctly routed and secured to ensure that they operate correctly. To do this, a tape that remains secured during high speed transport, such as speed tape, is often required to secure the arming connector and the additional wire storage unit. The speed tape runs the risk of peeling off and becoming dislodged during flight or after the storage unit is released, which could mean that the wires do not operate as designed.

[0007] The fuse system allows the stowage to be loaded onto the aircraft in a safe state. The stowage can be released in two ways: jettisoned release, where the stowage is released in an unarmed state, and live release, where the stowage is released in an armed state and becomes armed when it reaches a safe distance from the aircraft. The stowage is usually jettisoned in an emergency, for example in a situation where the aircraft needs to reduce weight and aerodynamic drag. In this case, the stowage is released, but the fuse system does not arm the munitions projectile, so that the stowage hits the ground but does not explode.

[0008] An alternative to a jettisoned release is a live release, in which a fuze system is activated at the time of release of the canister. The fuze system allows the canister to be armed at a safe distance from the launching aircraft and for the canister to detonate at the required time.

[0009] In some instances the containment is actuated by one or two electromagnetically operated safety release units. These are typically mounted at either end of the ejector release unit. In some instances an additional electrical safety release input is provided. In existing systems there is a risk that during a jettison event, if one of the safety release units fails, the containment will be released in an actuated state. Summary of the Invention

[0010] It is an object of exemplary embodiments of the present invention to at least partially reduce or avoid one or more of the disadvantages of the prior art discussed above or elsewhere, or at least to provide a viable alternative to existing arming devices.

[0011] In a first example, an arming apparatus for a storage section is provided, the apparatus comprising a first attachment system and a second attachment system, a mating connector coupled to the first attachment system and the second attachment system, and an arming clip coupled to the mating connector and for coupling to an arming connector of a first fuze input of the storage section, wherein each of the first attachment system and the second attachment system comprises an attachment for the arming unit, a first frangible connector coupled to the mating connector, and a second frangible connector coupled to the mating connector and the storage section, the mating connector being coupled to the first attachment system via a first coupling arrangement and to the second attachment system via a second coupling arrangement, wherein the first coupling arrangement and the second coupling arrangement have different structural configurations, and wherein each of the first coupling arrangement and the second coupling arrangement is manually secured.

[0012] Providing different coupling configurations means that the orientation of the arming device can be easily identified by the user during installation. Furthermore, the device may be delivered to the technician in assembled form. In other words, the device may be provided as a self-contained piece of equipment that the technician can easily install in a stowage to connect to the aircraft. This configuration means that the arming device can be easily attached to a stowage during installation and easily removed from said stowage after flight if the stowage was not released during flight. That is, the arming device is self-contained and may be reused to connect to other stowage in the future.

[0013] The provision of this arming device eliminates the need for excessively long arming wires and lanyards that can be caught and damaged during installation, actuated by aerodynamic forces in flight, or inadvertently actuated by ground crew during stowage preparation or weapon loading. Additionally, the requirement for speed tape is significantly reduced. Simplified cable routing allows for quick assembly and reduces the possibility of operator error. Additionally, the fuze system can be prefabricated with specified procedures and tolerances in a controlled factory environment, away from the aircraft, thus reducing the possibility of end user assembly / installation errors of the lanyard system. The arming device is configured such that all connectors fall off with the stowage during release. The arming device also provides a system in which two arming units must both be actuated for live release of the stowage. The arming device is configured to connect to the arming unit via an attachment. In some examples, the attachment includes a loop or ring or coupler for connecting the arming device to the arming unit. Additionally, the device provides an indication of which event occurred, for example, whether the containment was released as a live release, released as a jettison event, or released as a failed jettison event. When the containment is released as a live release, the tops of both first shear wires are retained within the arming unit.

[0014] In contrast, in case of a correct jettisoning event, both first shear wires are released in their entirety together with the retracted parts. In case of a failed jettisoning event indicating that one of the arming units did not operate correctly, in a post-flight check, one of the upper parts of the first shear wires is retained in the respective arming unit. Furthermore, the device allows the first input wind turbine lid to be opened within the correct operating angle range during a live release.

[0015] Furthermore, this configuration means that the arming device may be easily attached to a stowage section during installation and easily removed from said stowage section after flight if the stowage section is not released during flight, i.e. the arming device is self-contained and may be reused to connect other stowage sections in the future.

[0016] In one example, the second frangible connector comprises a clip at the second end, where the clip is configured to pass or loop through a lug of the housing to couple with the second frangible connector between the first and second ends. The clip may comprise a hook having a manually actuable member for selectively encircling the further member. The clip may include a carabiner clip, a Maillon, or a shackle. The clip may be folded back on itself with overlapping portions biased into contact with each other.

[0017] In one example, the second end of the second frangible connector is crimped together with a region of the second frangible connector between the first end and the second end of the second frangible connector.

[0018] In the first coupling configuration, the interlocking connector may be directly coupled to the first attachment system.

[0019] In a second coupling configuration, the interlocking connector may be coupled to the second attachment system via an intermediate coupler.

[0020] The intermediate coupler may comprise an intermediate ring.

[0021] The presence of an intermediate ring between the interlocking connector and the second attachment system allows the operator to easily identify the correct orientation of the arming system, thus reducing the risk of installation errors.

[0022] In one example, the gag rod wire is coupled to the storehouse and the second fuze input via a second attachment system. The gag rod wire provides a safety interlock during storehouse transport and a second input to the fuze system during live release. In an alternative example, there may be no gag rod wire and no second input to the fuze system at all.

[0023] Each attachment system may include a safety connector coupled to the interlocking connector and to the housing, the safety connector ensuring that components of the first attachment system and the second attachment system do not fall together with the housing.

[0024] The length of the safety connector may be greater than the length of the arming connector.

[0025] One or more of the first frangible connector and the second frangible connector may comprise a shear wire.

[0026] The first frangible connector may have a higher break strength compared to the break strength of the second frangible connector. The first frangible connector may have a break strength of about 700N to 1000N.

[0027] The second frangible connector may have a breaking force of approximately 100N to 200N.

[0028] The arming unit may comprise a arming solenoid, which has a first attachment force for the first frangible connector when the arming unit is energized and a second attachment force for the first frangible connector when the arming unit solenoid is not energized. The arming unit may comprise a ferromagnetic bolt that is mechanically biased (by a spring) to close a gate (e.g., a ball bearing) that partially occludes the channel. Under mechanical bias, the gate can be opened by a force above a first threshold (first attachment force). The arming unit may also comprise a solenoid surrounding the ferromagnetic bolt. When actuated by an electric current, the solenoid holds the bolt with the gate in a closed position. When the solenoid is actuated, the gate can be opened by a force above a second threshold (second attachment force). Although the arming unit is described above as comprising a solenoid, in practice any locking mechanism suitable for selectively providing an attachment force for the frangible connector can be used. For example, the arming unit may comprise a pneumatic piston and / or a locking mechanism that comprises a moveable pin to which a frangible connector may be coupled.

[0029] Thus, when an attachment (e.g., a loop or ring of cable) is placed around the gate that defines an opening that corresponds to the safety release unit, the safety release unit can provide two levels of holding force on the attachment (and whatever may be attached to the attachment) depending on whether the solenoid is activated or not.

[0030] The second attachment force may be greater than the break force of the first frangible connector.

[0031] The first attachment force may be less than a break force of the second frangible connector.

[0032] In one example, when the ejector release unit is actuated and the arming unit is energized, the second frangible connector of the first and second attachment systems may be configured to break under the weight of the storage section such that a load from the storage section is transferred through the arming connector to the ejector release unit, thereby actuating a first input of the fuse system.

[0033] The first frangible connector of the first and second attachment systems is configured to break following activation of the first input of the fuze system under the weight of the storage section.

[0034] In one example, the interlocking connector is configured to connect with a lid of a first fuse input of the enclosure. The lid may be operable to position the wind turbine.

[0035] In one example, a method of operating a safety release device is provided that includes energizing a first safety release unit and a second safety release unit and releasing a storage portion from a hook of an ejection release unit.

[0036] In one example, a method of installing a safety release device is provided, the device including identifying first and second ends of the device based on a first coupling configuration and a second coupling configuration, coupling a first frangible connector of a first attachment system to the first safety release unit, coupling a second frangible connector of the first attachment system to a first lug of the storage portion, coupling a first frangible connector of a second attachment system to the second safety release unit, coupling a second frangible connector of the second attachment system to a second lug of the storage portion, and coupling a safety release clip to the safety release connector. [Brief description of the drawings]

[0037] Examples of the present disclosure will now be described with reference to the accompanying drawings. [Figure 1]FIG. 1 shows some examples of existing arming devices. [Figure 2a] FIG. 2a shows a first example of the present disclosure. [Figure 2b] FIG. 2b shows a second example of the present disclosure. [Figure 2c] FIG. 2c shows various coupling configurations and / or clips. [Figure 2d] FIG. 2d shows various coupling configurations and / or clips. [Figure 2e] FIG. 2e shows various coupling configurations and / or clips. [Figure 2f] FIG. 2f shows various coupling configurations and / or clips. [Figure 2h] FIG. 2h shows various attachment configurations and / or clips. [Figure 2i] FIG. 2i shows various coupling configurations and / or clips. [Figure 2j] FIG. 2j shows details of the connection between the second frangible connector and the enclosure. [Diagram 3] FIG. 3 shows an example of a containment section being released from an ejector release unit during a jettison release. [Figure 4] FIG. 4 shows an example of the first stage of release of the containment section from the ejector release unit during live release. [Diagram 5] FIG. 5 shows an example of the second stage of release of the containment section from the ejector release unit during live release. [Figure 6] FIG. 6 shows an example of a third stage of release of the containment section from the ejector release unit during live release. [Figure 7a] FIG. 7a shows an example of a first stage of release of the containment section from the ejector release unit during a failed jettison release in the first example. [Figure 7b] FIG. 7b shows an example of a second stage of release of the containment section from the ejector release unit during a failed jettison release in the first example. [Figure 8a]FIG. 8a shows an example of the first stage of release of the containment section from the ejector release unit during a failed jettison release in the second example. [Figure 8b] FIG. 8b shows an example of a second stage of release of the containment section from the ejector release unit during a failed jettison release in the second example. [Figure 9] FIG. 9 shows example process steps of a dump release of a containment section from an ejector release unit in the second example. [Figure 10] FIG. 10 shows example process steps for live release of a containment section from an ejector release unit. [Figure 11] FIG. 11 shows an example of the process steps of a failed jettison release of a containment section from an ejector release unit. [Figure 12] FIG. 12 shows example steps for installing an arming device. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0038] Figure 1 shows a side view of a known portion of an arming device 100. Figure 1 shows an example of a connection between an ejector release unit (not shown) and a storage section 102 via an arming unit 104. In this example, one arming unit 104 operates with one fuse system 118.

[0039] The first cable 106 is attached to the arming unit 104 via a swivel link assembly 108. The first cable 106 is coupled at a second end to a second cable 110 and a third cable 112 at a connection point 114. The connection point 114 may include a ring to accommodate the looped ends or hooks of each of the first cable 106, the second cable 110, and the third cable 112. The second cable 110 is attached to a lid 116 of an electrical input 118 of a fuze system (not shown). The third cable 112 is connected at one end to a suspension lug 120 of the housing 102.

[0040] In this example, the lid 116 of the electrical input 118 system comprises a wind turbine. After the lid 116 is opened, the rotor of the wind turbine rotates, which generates electricity for the electrical input of the fuse system 118. For the wind turbine to operate effectively, it needs to be opened at the correct angle relative to the enclosure 102. As shown in FIG. 1, the first cable 106 and the second cable 110 are angled relative to the vertical. The purpose of angling the first cable 106 and the second cable 110 relative to the vertical is to allow the lid 116 of the electrical input 118 to open so that it is within the operating cone angle of the lid 116 of the electrical input 118.

[0041] The purpose of the third cable 112 is to ensure that the first cable 106 and the second cable 110 are released together when the enclosure 122 is ejected. In other words, the first cable 106, the second cable 110, and the third cable 112 are removed from the arming unit 104 and remain attached to the enclosure 122, and the enclosure 122 is ejected. In this existing system, relatively long cables are required to ensure that the lid 116 is opened within an acceptable operating cone angle.

[0042] Furthermore, in the event of a failed jettison, i.e., if the pilot attempts to jettison the stowage section 102 but the arming unit maintains a relatively high holding force, the stowage section 102 may be released in an armed condition, which is highly undesirable.

[0043] FIG. 2a shows a first example of an arming device 200 for a storage unit 204, such as an ammunition projectile, according to the present disclosure. Although the storage unit 204 comprises the ammunition projectile of FIG. 2a, the arming device 200 is configured to cooperate with other storage units as well. For example, the storage unit can take the form of any component that is removable from the aircraft. In particular, the arming device 200 is suitable for providing a mechanical input to the releasable component upon release from the aircraft. Other examples of storage units include drones, surveillance devices, etc.

[0044] The arming device 200 includes a first attachment system 202a and a second attachment system 202b, each of which is configured to couple a housing 204 to an ejector release unit 206.

[0045] The interlocking connector 208 is configured to couple with the first attachment system 202a and the second attachment system 202b and extend between the first attachment system 202a and the second attachment system 202b. In one example, the interlocking connector 208 includes a lanyard. In one example, the interlocking connector 208 is a fixed length element.

[0046] The arming device 200 also includes an arming clip 219 coupled to the mating connector 208. The arming clip 219 is configured to connect with the arming connector 210, which may be part of the arming device 200 or may be part of the fuze system 216. The arming connector 210 may be coupled to the arming clip 219 and a cap 212 of an electrical input 214 of the fuze system 216. In some examples, the fuze system 216 does not include a cap 212. The electrical input 214 may be connected to the fuze system 216 via one or more wires 236. In one example, the arming connector 210 is a fixed length element. The arming connector 210 may be coupled to the arming clip 219 via a coupling device 218, such as a ring. In some examples, the coupling device 218 is integral with the arming connector 210. The connection between the arming connector 210 and the coupling device 218 may be the same as the connection shown in FIG. 2d and may have a crimp configuration, for example. The arming clip 219 can move along the mating connector 208 so that the angle between the arming connector 210 and the lid 212 of the electrical input 214 can self-adjust in use. Coupling to a coupling device using the clip 219 means that the user can manually release the device 200 from the arming connector 210 in use.

[0047] The arming clip may comprise a hook having a manually operable member for selectively encircling the arming connector 210. The arming clip may have the general form of a carabiner clip, maillot, or shackle. The arming clip may have the form of a resilient member (e.g., a wire) folded back on itself and biased such that overlapping portions are biased into contact with one another.

[0048] Once the lid 212 of the electrical input 214 is opened, it may be locked in place to remain open. In this example, the lid 212 of the electrical input 214 of the fuze system 216 comprises a wind turbine. After 212 is opened, the rotor of the wind turbine spins, which generates electricity for the electrical input of the fuze system 216.

[0049] The first attachment system 202a is coupled to the first arming unit 220a and the first lug 222a of the housing 204. The second attachment system 202b is coupled to the second arming unit 220b and the second lug 222b. In other words, each of the first attachment system 202a and the second attachment system 202b is coupled to the respective arming units 220a, 220b and the respective lugs 222a, 222b of the housing 204. The first attachment system 202a and the second attachment system 202b are coupled to the respective arming units 220a, 220b via attachments. In some examples, the attachments include loops or rings or couplers for connecting the attachment systems to the respective arming units.

[0050] In one example, the first lug 222a is a forward lug of the storage unit 204 and the second lug 222b is an aft lug of the storage unit 204. In this example, the first arming unit 220a is a forward arming unit and the second arming unit 220b is an aft arming unit. In one example, the storage unit 204 is coupled to the aircraft via one or more ejector release unit suspension hooks 227a, 227b. The ejector release unit suspension hooks 227a, 227b are controllable by the pilot to enable the pilot to release the storage unit 204 from the suspension hooks 227a, 227b during operation.

[0051] Each of the first and second attachment systems 202a, 202b includes a first frangible connector 224a, 224b coupled to a respective arming unit 220a, 220b and mating connector 208. Each of the first frangible connectors 224a, 224b includes an attachment 221a, 221b for coupling to a respective arming unit 220a, 220b.

[0052] Additionally, each of the first attachment system 202a and the second attachment system 202b includes a second frangible connector 226a, 226b coupled to the interlocking connector 208 and the housing 204. In one example, the second frangible connector 226a, 226b is coupled to the lugs 222a, 222b of the housing 204. The second frangible connector 226a, 226b includes a first end coupled to the interlocking connector 208. In one example, the second frangible connector 226a, 226b is coupled to the interlocking connector 208 via one or more rings.

[0053] The second frangible connector 226a, 226b includes a second end configured to pass through a lug of the housing 204. A clip 233b may be present at the second end of the second frangible connector 226a, 226b and may pass through a lug of the housing 204. In some examples, the clip 233b is configured to couple to the second frangible connector between the first and second ends of the second frangible connector 226a, 226b.

[0054] The clip 233b may include a hook that may be clipped or hooked onto another member. In some examples, the clip 233b includes a manually operable member. The hook and the manually operable member may selectively encircle an additional member.

[0055] For example, the second frangible connector 226a of the first attachment system 202a is coupled to the first lug 222a of the housing 204, and the second frangible connector 226b of the second attachment system 202b is coupled to the second lug 222b of the housing 204.

[0056] The first lug 222a and the second lug 222b can comprise bail lugs that screw into the receptacle 204. The first lug 222a and the second lug 222b can have loops for receiving the second frangible connectors 226a, 226b of the first attachment system 202a and the second attachment system 202b.

[0057] In one example, the interlocking connector 208 comprises a first connection point 230a at a first end of the interlocking connector 208 and a second connection point 230b at a second end of the interlocking connector. The interlocking connector 208 is configured to mate with a first attachment system 202a at the first connection point 230a via a first interlocking arrangement. The interlocking connector 208 is configured to mate with a second attachment system 202b at the second connection point 230b via a second interlocking arrangement that is different from the first interlocking arrangement. The first interlocking arrangement and the second interlocking arrangement have different structural configurations, i.e., they have different geometric configurations, and a user can easily identify that they are different (i.e., they differ by more than a slight discrepancy due to manufacturing tolerances, etc.).

[0058] For example, the interlocking connector 208 may be configured to couple directly to the first attachment system 202a. In other words, a first end of the interlocking connector 208 may be directly coupled to the first frangible connector 224a and the second frangible connector 226a. In some examples, the interlocking connector 208 includes a ring at the first end that couples with the rings of the first frangible connector 224a and the second frangible connector 226a. However, there is no intermediate ring between the interlocking connector 208 and the first frangible connector 224a and the second frangible connector 226a at the first connection point 230a.

[0059] In contrast, at the second connection point 230b, the interlocking connector 208 may be configured to be coupled to the first frangible connector 224b and the second frangible connector 226b via an intermediate coupler 231, such as an intermediate ring. The presence of the intermediate coupler 231 aids in the orientation of the arming device 200. In other words, the presence of the intermediate coupler 231 means that a technician can easily identify the front and rear of the arming device 200 and install it in the correct orientation. The intermediate coupler 231 does not necessarily have to be ring-shaped, and may indeed take the form of other shapes.

[0060] The first and second coupling arrangements are configured to be manually secured, i.e., a user or technician cannot manually undo the coupling without the use of equipment. This is in contrast to couplings at other points in the device 200 where the couplings are not manually secured but are manually releasable, i.e., a user can manually undo the coupling without the need for additional equipment. The manually releasable coupling is between the second frangible connectors 226a, 226b and the lugs 222a, 222b of said housing 204.

[0061] The first frangible connector 224a of the first attachment system 202a may be configured to be coupled between the first arming unit 220a and the first connection point 230a, and the first frangible connector 224b of the second attachment system 202b may be configured to be coupled between the second arming unit 220b and the second connection point 230b. Further, the second frangible connector 226a of the first attachment system 202a may be configured to be coupled between the first connection point 230a and the first lug 222a of the receptacle 204. The second frangible connector 226b of the second attachment system 202b may be configured to be coupled between the second connection point 230b and the second lug 222b of the receptacle 204.

[0062] The first frangible connector 224 is configured to break at a predetermined load. For example, the first frangible connector 224 may have a breaking load or breaking force of about 700N to 1000N. If the first frangible connector 224 is subjected to a load that exceeds the breaking force, it breaks. In one example, the first frangible connector 224 and the second frangible connector 226 are shear wires, although other types of frangible connectors may actually be used. A frangible connector is any element that has a predetermined breaking force. For example, any cable, connector, thread configured to break at a predetermined breaking force may be considered to be a frangible connector.

[0063] The second frangible connector 226 is also configured to break at a predetermined load. In one example, the first frangible connector 224 has a higher break force compared to the break force of the second frangible connector 226. In other words, the first frangible connector 224 can receive a higher load compared to the second frangible connector 226 before breaking. Thus, when subjected to the same load, the second frangible connector 226 is configured to break before the first frangible connector 224. In this example, when an increasing load is applied to the first attachment system 202a and the second attachment system 202b, the second frangible connector 226 is configured to break when the increasing load exceeds the break force of the second frangible connector 226.

[0064] In one example, the second frangible connector 226 has a breaking load or force of 100N to 200N.

[0065] In one example, the arming device 200 also includes a first safety connector 228a configured to be coupled between the mating connector 208 and the housing 204, for example, via a first connection point 230a and a first lug 222a. The arming device 200 may also include a second safety connector 228b configured to be coupled between the mating connector 208 and the housing 204, for example, via a second connection point 230b and a second lug 222b. The first safety connector 228a and the second safety connector 228b are optional.

[0066] In one example, the lengths of the first safety connector 228a and the second safety connector 228b are substantially identical. Each of the first safety connector 228a and the second safety connector 228b has a longer length compared to the length of the arming connector 210. Providing the first safety connector 228a and the second safety connector 228b that are longer than the length of the arming connector 210 means that the electrical input 214 of the fuse system 216 is activated before the first safety connector 228a and the second safety connector 228b are taut, as described in more detail below.

[0067] In one example, the fuze system 216 includes a first input 214 and a second input 234, both of which must be actuated to arm the fuze system 216. As previously mentioned, the first input 214 may be an electrical input and the second input 234 may be a mechanical input, such as a gag rod. A gag rod wire 232 passes through the second input 234. In operation, the gag rod wire 232 must be physically removed from the gag rod 234 to actuate the second input 234.

[0068] 2a shows an example of a gag rod wire 232 coupled to a second input 234 of the fuse system 216 and to a second attachment system 202b via a gag rod attachment 235. For example, the gag rod 232 is attached to the gag rod attachment 235 at a second connection point 230b of the second attachment system 202b. The gag rod attachment 235 may comprise a clip that may be clipped onto a ring of the gag rod 232 in use.

[0069] Figure 2b shows an alternative example of the arming device 200 for the housing 204. The example of Figure 2b is identical to the example shown in Figure 2a, except that the gag rod wire 232 passes through the second connection point 208b of the interlocking connector 230 and is coupled to the gag rod attachment 235 at the first lug 222a of the housing 204.

[0070] 2c and 2d show an example of an end detail of the second frangible connector 226b coupled with an intermediate coupler 231 or ring at the end of the second frangible connector 226b. Note that this detail is equally applicable to other elements such as the first frangible connector 224b or the interlocking connector 208.

[0071] In this example, a portion of the second frangible connector 226b is fed through the intermediate coupler 231 and back along the second frangible connector 226b. A shroud or sleeve 229 is then threaded over the portions of the second frangible connector 226b that are adjacent to each other, as shown in FIG. 2c.

[0072] In Figure 2d, the sleeve 229 is reduced in size to crimp or bond adjacent portions of the second frangible connector 226b together. In one example, the sleeve 229 may be mechanically compressed or heat shrunk between Figures 2c and 2d. The crimping ensures a firm connection between the second frangible connector 226b (or other elements described above) and additional elements such as the intermediate coupler 231.

[0073] FIG. 2e shows an alternative example of a connection between elements. In this example, a first frangible connector 224a and a second frangible connector 226a are referenced, but the details may be applicable to other connections in the system. This configuration is identical to the example shown in FIG. 2c and FIG. 2d, except that the first frangible connector 224a is directly coupled to the second frangible connector 226a. The crimping configuration of the sleeve 229 is the same as FIG. 2d, except that a portion of the frangible connector is looped around a portion of another frangible connector rather than a ring or intermediate coupler 231.

[0074] FIG. 2f shows an alternative coupling configuration. In this example, the sleeve 229 comprises at least three channels through which the frangible wire can pass. The wire from the second frangible connector 226a, etc. passes through a first channel in the sleeve 229, then back on itself to pass through a second channel in the sleeve 229, then back on itself again to pass through a third channel in the sleeve 229. The serpentine of the wire through the sleeve should lock the wire in place by friction, although the sleeve 229 may be reduced in size to further crimp or bond the frangible connector in place. The configuration of FIG. 2f may be referred to as a shear locking device.

[0075] 2g and 2h show example end details of second frangible connector 226b coupled with clip 233a at the end of second frangible connector 226b.

[0076] In this example, a portion of the second frangible connector 226b is fed through the clip 233a and back along the second frangible connector 226b. A shroud or sleeve 229 is then threaded over the portions of the second frangible connector 226b that are adjacent to each other, as shown in FIG.

[0077] In Figure 2h, the sleeve 229 is reduced in size to crimp or bond adjacent portions of the second frangible connector 226b together. In one example, the sleeve 229 may be mechanically compressed or heat shrunk between Figures 2g and 2h. The crimping ensures a firm connection between the second frangible connector 226b (or other elements described above) and an additional element such as the clip 233a.

[0078] The clip 233a is in the form of a carabiner clip. Thus, the clip 233a includes a pivot gate 2330 that is manually operable to open and close. Thus, the clip can be coupled to a further member by manually opening the gate to allow a further member (e.g., the second frangible connector 226a) to enter the clip 233a, and then manually closing the gate. Furthermore, the further member can be released from the clip 233 by manually opening the gate, and thus the coupling is manually releasable and not manually secured.

[0079] A further clip 233b is shown in Figure 2i. Clip 233b comprises an elastic member (e.g. a wire) that stretches and returns on itself to form a loop, with portions of the elastic member crossing and biased into contact with each other.

[0080] Clip 233b has a barb 2331 at one end which projects to capture the other end of the member when the loop is spread apart.

[0081] Clip 233b includes a ring 2332 at the other end for convenient attachment to a wire and crimping arrangement.

[0082] In use, clip 233b can be manually operated to accept an additional member (e.g., second frangible connector 226a) by spreading apart the intersection of the elastic members and threading the additional member within the loop. With the additional member within the loop, the elastic members can then be released so that the bias of the elastic members closes the loop at the intersection, thereby enclosing the additional member.

[0083] In use, the clip 233b can be manually operated to release the enclosed further member by spreading apart the intersections of the elastic members and allowing the further member to exit the loop, and thus the bond between the clip 233b and the further member is manually releasable but not manually secured.

[0084] Figure 2j shows an example of a connection between an attachment system and a storage unit, e.g., the detail indicated by arrow A in Figure 2a. Figure 2j is based on a connection between a first attachment system 202a and a storage unit 204, but can be applied to a connection between a second attachment system 202b and a storage unit 204 as well.

[0085] As shown in FIG. 2j, the second frangible connector 226a of the first attachment system 202a has a first end coupled to the interlocking connector 208. The first attachment system 202a has a second end configured to pass or loop over the first lug 222a of the housing 204 and couple to the second frangible connector 226a between the first and second ends of the second frangible connector 226a. The second frangible connector 226b of the second attachment system 202b has a first end coupled to the interlocking connector 208. The second frangible connector 226b of the second attachment system 202b has a second end configured to pass or loop over the second lug 222b of the housing 204 and couple to the second frangible connector 226b between the first and second ends of the second frangible connector 226b.

[0086] The safety connectors 228a, 228b may have a similar configuration, i.e., a first end of the first safety connector 228a is coupled to the mating connector 208 and a second end of the first safety connector 228a is configured to loop through the lug 222a of the housing 204 and mate with the first safety connector 228a between the first and second ends.

[0087] Similarly, a first end of the second safety connector 228b is coupled to the interlocking connector 208 and a second end of the second safety connector 228b is configured to pass or loop through the lug 222b of the storage portion 204 and couple with the second safety connector 228b between the first and second ends.

[0088] This configuration allows the first attachment system 202a and the second attachment system 202b to be quickly attached and detached from the lugs 222a, 222b of the storage unit 204 during installation of the storage unit 204 on the aircraft. It allows the arming device 200 to be reused in a different storage unit in the future if the storage unit 204 is not deployed in flight. In this manner, the arming device 200 becomes a self-contained device that may be utilized multiple times. Additionally, this configuration makes it easier for a technician to connect the arming device 200 to the storage unit 202 during installation.

[0089] A second end of the second frangible connector 226a, 226b includes a clip 233b that clips to the second frangible connector 226a, 226b between the first and second ends of the second frangible connector 226a, 226b. An alternative clip, such as a carabiner clip 233a, may be used in place of the clip 233a.

[0090] The second ends of the safety connectors 228a, 228b are provided with clips 233b. The clips 233b are fastened to the safety connectors 228a, 228b between the first and second ends of the safety connectors 228a, 228b. An alternative clip, such as a carabiner clip 233a, may be used in place of the clips 233a.

[0091] The presence of clip 233b (or alternatively clip 233a for example) means that the first attachment system 202a and the second attachment system 202b are manually connectable to and manually releasable from the housing 204.

[0092] In one example, the safety connectors 228a, 228b may be crimped to hold the clip 233b in place at the second ends of the safety connectors 228a, 228b, as shown in Figures 2c and 2d above.

[0093] The details shown in FIG. 2j may be equally applicable to the configuration shown in FIG. 2b, with the difference being that the gag rod wire is also bonded to the first lug 222a.

[0094] 3-8 show the gag rod wire 232 being coupled to a gag rod attachment 235 in a second attachment system 202b as shown in FIG. 2a. However, in each of these figures, the gag rod wire 232 may be coupled with a gag rod attachment 235 at the first lug 222a of the housing 204 as shown in Figure 2b. The configuration shown in Figure 2i may also be present in Figures 3 to 8.

[0095] The arming units 220a, 220b may be configured to couple the attachment systems to the ejector release unit 206, for example, the first arming unit 220a couples the first attachment system 202a to the ejector release unit 206, and the second arming unit 220b couples the second attachment system 202b to the ejector release unit 206. In one example, each of the arming units 220a, 220b comprises an arming solenoid. The pilot can energize the arming units 220a, 220b to change the pull force required to detach the first frangible connector 224 from the arming unit 220. In one example, the arming unit 220 has a relatively low pull force when not energized and a relatively high pull force when the arming unit is energized. In one example, the unenergized pull force of the first frangible connector 224a, 224b from the arming units 220a, 220b is about 35N to 70N. The energized pull force of the first frangible connector 224a, 224b from the arming units 220a, 220b is greater than about 1100N. In some examples, the unenergized pull force of the first frangible connector 224a, 224b from the arming units 220a, 220b is less than the break strength of the second frangible connector 226a, 226b. In one example, the energized pull force of the first frangible connector 224a, 224b from the arming units 220a, 220b is greater than the break strength of the second frangible connector 226a, 226b. The weight of the storage section 204 is greater than the break strength of the first frangible connectors 224a, 224b, the break strength of the second frangible wires 226a, 226b, and twice the pull-out force of the arming unit, whether in a de-energized or energized state.

[0096] As described above, the storage unit 204 may be coupled to the aircraft via one or more ejector release unit suspension hooks 227a, 227b. The ejector release unit suspension hooks 227a, 227b are controllable by the pilot to allow the pilot to release the storage unit 204 from the suspension hooks during operation. In one example, the one or more ejector release unit suspension hooks 227a, 227b are part of the aircraft rather than part of the arming device.

[0097] The dump sequence of the system will now be described. The initial state of the arming device 200 is shown in Figures 2a and 2b. The arming units 220a, 220b are in a de-energized state so as to have a relatively low pull-out force requirement.

[0098] The pilot activates the jettison sequence, which releases the stowage section 204 from the ejector release unit suspension hooks 227a, 227b. In some examples, at this stage the stowage section 204 may be pushed away from the aircraft by one or more ejector release unit rams.

[0099] 3 illustrates the next stage of the jettison sequence of the arming device 200. The weight of the storage section 204 is transferred to the first and second attachment systems 202a, 202b. In other words, the weight of the storage section 204 is transferred to the ejector release unit 206 via the second frangible connectors 226a, 226b, the first frangible connectors 224a, 224b, and the attachments coupled to the arming units 220a, 220b of the first and second attachment systems 202b, respectively. Because the arming units 220a, 220b are in a de-energized state, the pull force required to remove the first frangible connectors 224a, 224b from the respective arming units 220a, 220b is relatively small. The break strength of the first frangible connectors 224a, 224b and the second frangible connectors 226a, 226b is higher than the pull force of the first frangible connectors 224a, 224b from the arming units 220a, 220b in the de-energized state. Thus, the weight of the housing 204 pulls the respective first frangible connectors 224 from the respective arming units 220 as shown by the arrows in FIG.

[0100] In this example, the first frangible connectors 224a, 224b, the second frangible connectors 226a, 226b, the interlocking connector 208, the arming connector 210, and the safety connector 228 are released along with the storage unit 204. The gag rod wire 232 is not removed from the fuze system 216, and the cap 212 of the electrical input 214 of the fuze system 216 is not opened. Thus, in the jettison sequence, neither of the two inputs of the fuze system 216 are activated, and the storage unit 204 is released in an unarmed state.

[0101] Next, the live release sequence of the system will be described. The initial state of the arming device 200 is shown in Fig. 2a or 2b. The pilot initiates the live release sequence, which energizes the arming units 220a, 220b. Thus, the pull force of the first frangible connectors 224a, 224b from the arming units 220a, 220b is increased until it exceeds the breaking strength of the first frangible connectors 224a, 224b and the second frangible connectors 226a, 226b.

[0102] The stowage section 204 is then released from the ejector release unit suspension hooks 227a, 227b. In some examples, at this stage the stowage section 204 may be pushed away from the aircraft by one or more ejector release unit rams.

[0103] 4 shows an example of the next stage of the live release sequence. After releasing the enclosure 204 from the ejector release unit suspension hooks 227a, 227b, the weight of the enclosure 204 is transferred to the ejector release unit 206 via the first attachment system 202a and the second attachment system 202b. In this example, the weakest element in each of the attachment systems 202a, 202b is the second frangible connector 226a, 226b. Therefore, the second frangible connector 226a, 226b of each of the attachment systems 226 breaks because the weight of the enclosure is greater than the breaking strength of the second frangible connector 226a, 226b and the limiting factor in each of the attachment systems is the strength of the second frangible connector 202a, 226b.

[0104] As shown in FIG. 4, following the fracture of the second frangible connectors 226a, 226b, the load path of the enclosure 204 now passes through the arming connector 210, which therefore becomes taut.

[0105] 5 illustrates the next stage in the live release sequence: the load path travels through the arming connector 210, opening the cap 212 of the first input 214 of the fuze system 216. Thus, the first input 214 of the fuze system 216 is armed.

[0106] As the storage section 204 falls further from the ejector release unit 206, the gag rod wire 232 is detached from the second input 234 of the fuze system 216, thereby allowing the fuze system 216 to be activated by power from the electrical input 214. Thus, both the first input 214 and the second input 234 of the fuze system 216 are activated.

[0107] 5 shows that the interlocking connector 208 can deform when the weight of the storage section 204 is transferred from the interlocking connector 208 through the arming connector 210 to each of the first frangible connectors 224a, 224b of each of the first and second attachment systems 202. In one example, the interlocking connector 208 is deformed to have a "V-shape". In an example where the arming connector 210 is coupled to the arming clip 219 via a coupling device 218, the coupling point between the arming connector 210 and the interlocking connector 208 may change. Providing the coupling device 218 and arming clip 219 means that the lid 212 of the first input 214 can be opened within the correct operating angle range.

[0108] 6 shows the next stage of the live release sequence. After the lid of the first input 214 is opened, the safety connectors 228a, 228b are taut and the load path from the housing 204 to the ejector release unit 206 is through the safety connectors 228a, 228b to the first frangible connectors 224a, 224b of each of the attachment systems 202a, 202b, through the respective attachments to the arming units 220a, 220b. The next limiting factor of the system 200 is the strength of the first frangible connectors 224a, 224b, which break as shown in FIG. 6. The housing 204 falls from the ejector release unit 206 as shown by the arrow in FIG. 6. When the first frangible connectors 224a, 224b break, the storage section 204 is no longer connected to the ejector release unit 206 and is released in a live state when both the first input 214 and the second input 234 of the fuze system 216 are activated. The safety connectors 228a, 228b ensure that the various connectors are released with the storage section 204 to avoid them swinging under the aircraft and thus damaging the aircraft. The safety connectors 228a, 228b ensure that the various connectors that are released remain attached to the storage section 204.

[0109] A failed dump sequence of the system 200 will now be described. The starting condition is first shown in FIG. 2a or 2b. As in a normal dump sequence, in a failed dump event, none of the arming units 220a, 220b are energized. However, one of the arming units may become locked, so that it acts as if it is energized and has a relatively high pull-out force of the first frangible connector 224b from the second arming unit 220b. In one example, the arming units 220a, 220b may become locked due to internal wear of the components generating dust that clogs the internal mechanisms of the arming units 220a, 220b.

[0110] 7a shows a first stage of a failed jettisoning event in which the second arming unit 220b is in a failed locked state. After releasing the storage unit 204 from the ejector release unit suspension hooks 227a, 227b, the weight of the storage unit 204 is transferred to the ejector release unit 206 via the first attachment system 202a and the second attachment system 202b. In this example, in the first attachment system 202a, the first frangible connector 224a is released from the first arming unit 220a according to a standard jettisoning event. However, in the second attachment system 202b, the first frangible connector 224b is locked in the arming unit 220b and therefore is not released as intended.

[0111] The interlocking connector 208 can begin to pivot or rotate as the first attachment system 202a separates downwardly away from the first arming unit 220a The next weakest element is the second frangible connector 226b, and the load path from the housing 204 to the ejector release unit 206 passes through the second attachment system 202b, causing the second frangible connector 226b to break.

[0112] The next stage of the failed jettison event is that the safety connector 228b of the second attachment system 202b becomes taut as the containment section 204 falls. As the containment section 204 falls, the gag rod wire 232 is detached from the second input 234 of the fuse system 216. FIG. 7b shows an example of a failed jettison event in which the safety connector 228b of the second attachment system 202b becomes taut. In this scenario, the load path from the containment section 204 to the ejector release unit 206 is through the first frangible connector 224b of the second attachment system 202b. This causes the first frangible connector 224b of the second attachment system 202b to break because the weight of the containment section 204 is higher than the breaking strength of the first frangible connector 224b. Thus, the storage section 204 is released from the ejector release unit 206 without the first input 214 of the fuze system 216 being actuated. Thus, even in the event of a failed jettison event, the storage section 204 is not activated and the storage section is released in a safe state. The arming apparatus 200 provides a mechanism for connecting the two arming units 220a, 220b and provides an automatic protection system such that if one arming unit 220a, 220b fails during a jettison event, the storage section 204 is still released in an unarmed state.

[0113] The start condition is first shown in FIG. 2a or 2b. In a failed dump event, according to the normal dump sequence, none of the arming units 220a, 220b are energized. However, one of the arming units may become locked, so that it acts as if it is energized and has a relatively high pull-out force of the first frangible connector 224b from the second arming unit 220b. In one example, the arming units 220a, 220b may become locked due to internal wear of the components generating dust that clogs the internal mechanisms of the arming units 220a, 220b.

[0114] 8a shows a first stage of a failed jettisoning event, in which the first arming unit 220a is in a failed locked state. After releasing the storage unit 204 from the ejector release unit suspension hooks 227a, 227b, the weight of the storage unit 204 is transferred to the ejector release unit 206 via the first attachment system 202a and the second attachment system 202b. In this example, in the second attachment system 202b, the first frangible connector 224b is released from the second arming unit 220b according to a standard jettisoning event. However, in the first attachment system 202a, the first frangible connector 224a is locked in the first arming unit 220a and is therefore not released as intended.

[0115] The interlocking connector 208 can begin to pivot or rotate as the second attachment system 202b separates downwardly away from the second arming unit 220b. The next weakest element is the second frangible connector 226a, and the load path from the housing 204 to the ejector release unit 206 passes through the first attachment system 202a, causing the second frangible connector 226a to break.

[0116] The next stage of the failed jettison event is that the safety connector 228a of the first attachment system 202a goes taut as the containment section 204 falls. In this example, the gag rod wire 232 may not be removed from the second input 234 of the fuse system 216 as the containment section 204 falls. FIG. 8b shows an example of a failed jettison event in which the safety connector 228a of the first attachment system 202a goes taut. In this scenario, the load path from the containment section 204 to the ejector release unit 206 is through the first frangible connector 224a of the first attachment system 202a. This causes the first frangible connector 224a of the first attachment system 202a to break as the weight of the containment section 204 is higher than the breaking strength of the first frangible connector 224a. Thus, the storage section 204 is released from the ejector release unit 206 without either the first input 214 of the fuze system 216 or the second input 234 of the fuze system 216 being actuated. Thus, even in a failed jettison event, the storage section 204 is not activated and the storage section is released in a safe state. The arming device 200 is configured to connect the two arming units 220a, 220b and provides an automatic protection system such that in the event that one arming unit 220a, 220b fails during a jettison event, the storage section 204 is still released in an unarmed state.

[0117] The provision of this arming device 200 eliminates the need for excessively long arming wires and lanyards that can be caught and damaged during installation or inadvertently operated by ground crew members during weapon loading. Additionally, the requirements for speed tape are significantly reduced. Simplified cable routing allows for quick assembly and reduces the possibility of operator error. Additionally, the fuse system 216 can be prefabricated off the aircraft in a controlled factory environment, thus reducing the possibility of assembly errors in the lanyard system. The arming device 200 is configured such that all connectors drop out along with the retractable section 204 during release.

[0118] The device provides an indication of what event occurred, for example, whether the containment section 204 was released as a live release, released as a dump event, or released as a failed dump event.

[0119] When housing 204 is released as a live release, the upper portions of first shear wires 224a and 224b are held within arming units 220a and 220b, as shown in FIG.

[0120] In contrast, in the case of a correct jettison event, both first shear wires 224a and 224b are released in their entirety along with storage portion 204, as shown in FIG.

[0121] In the event of a failed jettison event indicating that one of the arming units 220a, 220b is not operating correctly, during a post-flight check, one of the upper portions of the shear wires 224a, 224b is retained within the respective arming unit 220a, 220b, as shown in either FIG. 7b or FIG. 8b.

[0122] 9 illustrates an example of a method for performing a jettison release, according to an example. In step 300, the pilot initiates the release of the storage section 204 without energizing the arming units 220a, 220b. In step 302, the first frangible connectors 224a, 224b are released from the arming units 220a, 220b of the first and second attachment systems 202a, 202b, respectively, to release the storage section 204 in an unarmed state from the ejector release unit 206.

[0123] 10 illustrates an example of a method for performing a live release according to one embodiment. In step 400, the pilot energizes the arming units 220a, 220b. In step 402, the storage section 204 is released from the ejector release unit suspension hook.

[0124] In step 404 , the second frangible connectors 226 a , 226 b of each of the first and second attachment systems 202 a , 202 b break due to the weight of the enclosure 204 .

[0125] In step 406 , the lid 212 of the first input 214 is opened by the weight of the enclosure 204 passing through the arming connector 210 .

[0126] In step 408 , the gag rod is released from the second input 234 of the fuze system 216 .

[0127] In step 410 , the first frangible connectors 224 a , 224 b of the first and second attachment systems 202 a , 202 b break due to the weight of the enclosure, thereby releasing the enclosure 204 from the ejector release unit 206 .

[0128] FIG. 11 shows an example of the steps of a faulty jettisoning event.

[0129] In step 500, the pilot initiates the release of the storage section 204 without energizing the arming units 220a, 220b. However, one of the arming units 220 fails. In this example, it is the second arming unit 220b that fails, but in other examples, the first arming unit 220a may fail and the same process applies.

[0130] In step 502, the first frangible connector 224a is released from the arming unit 220a of the first attachment system 202a, while the first frangible connector 224b is retained within the arming unit 220b of the second attachment system.

[0131] In step 504 , the second frangible connector 226 b of the second attachment system 202 b breaks due to the weight of the enclosure 204 .

[0132] In step 506, the second safety connector 228b becomes taut and transfers the load to the first frangible connector 224b of the second attachment system 202b, causing the first frangible connector 224b of the second attachment system 202b to break under the weight of the storage portion 204, thereby releasing the storage portion 204 from the ejector release unit 206.

[0133] 12 shows an example of steps for installing the arming device 200. In step 600, a user identifies first and second ends of the device 200 based on a first and second coupling configuration. The first end may be the front end and the second end may be the rear end of the device 200.

[0134] The first coupling configuration may be, for example, a direct coupling between the first frangible connector 224a and the second frangible connector 226a of the first attachment system, as shown in FIG. 2e above. The second coupling configuration may be an indirect connection between the first frangible connector 224b and the second frangible connector 226b of the second attachment system 202b. For example, there may be an intermediate coupler 231 between the first frangible connector 224b and the second frangible connector 226b of the second attachment system 202b. The difference in the coupling configurations allows the user to identify the correct orientation of the device so that the device is placed in the correct position.

[0135] In step 602, the first frangible connector 224a of the first attachment system 202a is coupled to the first arming unit.

[0136] In step 604, the second frangible connector 226a of the first attachment system 202a is coupled to a first lug of the housing, e.g., the clip 233 of the second frangible connector passes through the lug of the housing 204 and connects to the second frangible connector between the first and second ends.

[0137] In step 606, the first frangible connector 224b of the second attachment system 202b is coupled to the second arming unit.

[0138] In step 608, the second frangible connector 226b of the second attachment system 202b is coupled to a second lug of the housing, e.g., the clip 233 of the second frangible connector passes through the lug of the housing 204 and connects to the second frangible connector between the first end and the second end.

[0139] In step 610, the arming clip 219 is coupled to the arming connector.

[0140] Attention is directed to all publications and documents related to this application that are filed contemporaneously with or prior to this application and that are open to public inspection herewith, and the entire contents of such publications and documents are incorporated herein by reference.

[0141] All of the features disclosed in this specification (including any accompanying claims, abstract, and drawings), and / or all of the steps of any method or process so disclosed, may be combined in any combination, except combinations where at least some of such features and / or steps are mutually exclusive.

[0142] Each feature disclosed in this specification (including any accompanying claims, abstract, and drawings), unless expressly stated otherwise, may be replaced by alternative features serving the same, equivalent, or similar purpose. Thus, unless expressly stated otherwise, each feature disclosed is only one example of a common series of equivalent or similar features.

[0143] The invention is not limited to the details of the foregoing embodiments, but extends to any novel one or any novel combination of features disclosed in this specification (including any accompanying claims, abstract and drawings), or to any novel one or any novel combination of steps of any method or process so disclosed. The invention as described in the claims of the original application is set forth below. [C1] An arming device (200) for a storage section (204), comprising: a first attachment system (202a) and a second attachment system (202b); an interlocking connector (208) coupled to the first attachment system (202a) and the second attachment system (202b); a disarming clip (219) coupled to the interlocking connector for mating with an arming connector (210) of a first fuse input (214) of the storage section (204); Here, each of the first attachment system (202a) and the second attachment system (202b) comprises: an attachment for a safety release unit (220); a first frangible connector (224) coupled to the arming unit (220) and the mating connector (208); a second frangible connector (226) coupled to the interlocking connector (208) and the housing portion (204); wherein the interlocking connector (208) is coupled to the first attachment system (202a) via a first coupling arrangement and is coupled to the second attachment system (202b) via a second coupling arrangement, wherein the first coupling arrangement and the second coupling arrangement have different structural configurations; wherein each of the first coupling arrangement and the second coupling arrangement is manually secured to the apparatus (200). [C2] The apparatus (200) of claim C1, wherein in the first coupling configuration, the interlocking connector (208) is directly coupled to the first attachment system (202a). [C3] The apparatus (200) according to any one of operations C1 or C2, wherein in the second coupling configuration, the interlocking connector is coupled to the second attachment system (202a) via an intermediate coupler (231). [C4] The apparatus (200) according to C3, wherein the intermediate coupler (231) comprises an intermediate ring. [C5] 5. The apparatus (200) of any one of claims 1 to 4, comprising a gag rod wire (232) coupled to the storage portion (204) and a second fuse input (234) via the second attachment system (202b). [C6] The device (200) of any one of C1 to C5, wherein each attachment system (202a, 202b) comprises a safety connector (228a, 228b) coupled to the interlocking connector (208) and the storage portion (204). [C7] The apparatus (200) according to C6, wherein a length of the safety connectors (228a, 228b) is greater than a length of the arming connector (210). [C8] The apparatus (200) of any one of C1 to C7, wherein one or more of the first frangible connectors (224a, 224b) and the second frangible connectors (226a, 226b) comprise a shear wire. [C9] The apparatus (200) of any one of C1 to C8, wherein the first frangible connectors (224a, 224b) have a higher breaking strength compared to a breaking strength of the second frangible connectors (226a, 226b). [C10] 10. The apparatus (200) of any one of claims 1 to 9, wherein the arming unit (220a, 220b) of each of the first attachment system (202a) and the second attachment system (202b) comprises a arming solenoid, wherein the arming solenoid has a first attachment force relative to the first frangible connector (224a, 224b) when the arming unit is energized and a second attachment force relative to the first frangible connector (224a, 224b) when the arming unit solenoid is not energized. [C11] The apparatus (200) of claim C10 when dependent on any one of claims C7, 8 or 9, wherein the second attachment force is greater than a break force of the first frangible connectors (224a, 224b). [C12] The apparatus (200) of C11, wherein the first attachment force is less than a break force of the second frangible connectors (226a, 226b). [C13] The apparatus (200) of C11 or 12, wherein when an ejector release unit is actuated and the arming unit is energized, the second frangible connectors (226a, 226b) of the first and second attachment systems (202a, 202b) are configured to break under the weight of the storage section (204), thereby transmitting a load from the storage section through the arming connector (210) to the ejector release unit, thereby actuating a first input (214) of a fuse system (216). [C14] The apparatus (200) described in C13, wherein the first frangible connectors (224a, 224b) of the first and second attachment systems (202a, 202b) are configured to break following activation of the first input (214) of the fuse system (216) by the weight of the storage portion (204). [C15] A method for operating a safety release device (200) according to any one of claims 1 to 14, comprising the steps of: energizing the first arming release unit and the second arming release unit; and releasing the storage portion from a hook of the ejection release unit. [C16] A method for installing a safety release device according to any one of claims 1 to 15, comprising the steps of: identifying first and second ends of the device based on the first coupling configuration and the second coupling configuration; coupling the first frangible connector (224a) of the first attachment system (202a) to the first arming unit; coupling the second frangible connector (226a) of the first attachment system (202a) to a first lug of the housing; coupling the first frangible connector (224b) of the second attachment system (202b) to the second arming unit; coupling the second frangible connector (226b) of the second attachment system (202b) to a second lug of the housing; and coupling the arming clip to the arming connector.

Claims

1. An arming device (200) for a storage section (204), comprising: a first attachment system (202a) and a second attachment system (202b); an interlocking connector (208) coupled to the first attachment system (202a) and the second attachment system (202b); a disarming clip (219) coupled to the mating connector for mating with an arming connector (210) of a first fuse input (214) of the storage section (204); wherein each of the first attachment system (202a) and the second attachment system (202b) comprises: an attachment for an arming unit (220); a first frangible connector (224) coupled to said arming unit (220) and said mating connector (208); a second frangible connector (226) coupled to the interlocking connector (208) and the housing portion (204); wherein the interlocking connector (208) is coupled to the first attachment system (202a) via a first coupling arrangement and is coupled to the second attachment system (202b) via a second coupling arrangement, wherein the first coupling arrangement and the second coupling arrangement have different structural configurations; An apparatus (200), wherein each of the first coupling arrangement and the second coupling arrangement is manually secured.

2. The apparatus (200) of claim 1, wherein in the first coupling configuration, the interlocking connector (208) is directly coupled to the first attachment system (202a).

3. 3. The apparatus (200) of claim 1 or 2, wherein in the second coupled configuration, the interlocking connector is coupled to the second attachment system (202a) via an intermediate coupler (231).

4. The apparatus (200) of claim 3, wherein the intermediate coupler (231) comprises an intermediate ring.

5. 5. The apparatus (200) of claim 1, further comprising a gag rod wire (232) coupled to the housing (204) and a second fuse input (234) via the second attachment system (202b).

6. The apparatus (200) of any one of claims 1 to 5, wherein each attachment system (202a, 202b) comprises a safety connector (228a, 228b) coupled to the interlocking connector (208) and the storage portion (204).

7. The apparatus (200) of claim 6, wherein the length of the safety connectors (228a, 228b) is greater than the length of the arming connector (210).

8. The apparatus (200) of any one of claims 1 to 7, wherein one or more of the first frangible connectors (224a, 224b) and the second frangible connectors (226a, 226b) comprise shear wires.

9. The apparatus (200) of any one of claims 1 to 8, wherein the first frangible connectors (224a, 224b) have a higher break strength compared to a break strength of the second frangible connectors (226a, 226b).

10. 10. The apparatus of claim 1, wherein the arming unit of each of the first and second attachment systems comprises an arming solenoid having a first attachment force against the first frangible connector when the arming unit is energized and a second attachment force against the first frangible connector when the arming unit solenoid is not energized.

11. The apparatus (200) of claim 10, wherein the second attachment force is less than a break force of the first frangible connectors (224a, 224b).

12. The apparatus (200) of claim 11, wherein the first attachment force is greater than a break force of the second frangible connector (226a, 226b).

13. 13. The apparatus (200) of claim 11 or 12, wherein when an ejector release unit is actuated and the arming unit is energized, the second frangible connectors (226a, 226b) of the first and second attachment systems (202a, 202b) are configured to break under the weight of the storage section (204), thereby transmitting a load from the storage section through the arming connector (210) to the ejector release unit, thereby actuating a first input (214) of a fuse system (216).

14. 14. The apparatus (200) of claim 13, wherein the first frangible connectors (224a, 224b) of the first and second attachment systems (202a, 202b) are configured to break following activation of the first input (214) of the fuze system (216) by a weight of the storage portion (204).

15. 2. A method of operating the arming device (200) of claim 1, comprising the steps of: energizing the first arming unit and the second arming unit; and releasing the storage portion from a hook of an ejector release unit.

16. 13. A method for installing the arming device of claim 1, comprising the steps of: identifying first and second ends of the device based on the first coupling configuration and the second coupling configuration; coupling the first frangible connector (224a) of the first attachment system (202a) to a first arming unit; coupling the second frangible connector (226a) of the first attachment system (202a) to a first lug of the storage portion; coupling the first frangible connector (224b) of the second attachment system (202b) to a second arming unit; coupling the second frangible connector (226b) of the second attachment system (202b) to a second lug of the storage portion; and coupling the arming clip to the arming connector.

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