초록 ▼

The device is for attaching a syringe or other type of dispenser to a container containing pharmaceutical. The device preferably includes a rubber band and a syringe holder. The syringe holder preferably includes an attachment lip, a bracket, and a clamp. The attachment lip and bracket preferably fr

The device is for attaching a syringe or other type of dispenser to a container containing pharmaceutical. The device preferably includes a rubber band and a syringe holder. The syringe holder preferably includes an attachment lip, a bracket, and a clamp. The attachment lip and bracket preferably frame the rubber band, which is used to hold the attachment lip against the container. The clamp preferably is used to engage and hold the syringe.

대표청구항 ▼

The device is for attaching a syringe or other type of dispenser to a container containing pharmaceutical. The device preferably includes a rubber band and a syringe holder. The syringe holder preferably includes an attachment lip, a bracket, and a clamp. The attachment lip and bracket preferably fr

The device is for attaching a syringe or other type of dispenser to a container containing pharmaceutical. The device preferably includes a rubber band and a syringe holder. The syringe holder preferably includes an attachment lip, a bracket, and a clamp. The attachment lip and bracket preferably frame the rubber band, which is used to hold the attachment lip against the container. The clamp preferably is used to engage and hold the syringe. wherein: the multilayered insulation composite has a burn through time of at least 5 minutes. 7. The insulation system for increasing the burn through resistance of an aircraft fuselage having an outer skin, according to claim 2, wherein: the insulation layers are polyimide foam insulation layers; and the multilayered insulation composite is encapsulated within a polymeric film. 8. The insulation system for increasing the burn through resistance of an aircraft fuselage having an outer skin, according to claim 7, wherein: the polymeric film is a polyimide film. 9. The insulation system for increasing the burn through resistance of an aircraft fuselage having an outer skin, according to claim 7, wherein: the multilayered insulation composite has a burn through time of at least 5 minutes. 10. The insulation system for increasing the burn through resistance of an aircraft fuselage having an outer skin, according to claim 2, wherein: the first interleaf barrier layer is intermediate the major surfaces of the first and second insulation layers which are opposed to each other. 11. The insulation system for increasing the burn through resistance of an aircraft fuselage having an outer skin, according to claim 10, wherein: the multilayered insulation composite includes a third insulation layer and a second interleaf barrier layer of a high temperature resistant reflective material; the third insulation layer and the second interleaf barrier layer each have major surfaces extending in planes substantially parallel to the major surfaces of the first and second insulation layers and the first interleaf barrier layer; and the second interleaf barrier layer is intermediate the major surfaces of the second and third insulation layers which are opposed to each other. 12. The insulation system for increasing the burn through resistance of an aircraft fuselage having an outer skin, according to claim 1, wherein: the first interleaf barrier layer of a high temperature resistant reflective material is intermediate an outer major surface of the first insulation layer and the film. 13. The insulation system for increasing the burn through resistance of an aircraft fuselage having an outer skin, according to claim 12, wherein: a second interleaf barrier layer of high temperature resistant reflective material is intermediate the major surfaces of the first and the second insulation layers which are opposed to each other. 14. The insulation system for increasing the burn through resistance of an aircraft fuselage having an outer skin, according to claim 12, wherein: there is a third insulation layer and a second interleaf barrier layer of high temperature resistant reflective material which is intermediate the opposed major surfaces of two of the insulation layers. 15. The insulation system for increasing the burn through resistance of an aircraft fuselage having an outer skin, according to claim 12, wherein: the interleaf barrier layer comprises a reflective mineral. 16. The insulation system for increasing the burn through resistance of an aircraft fuselage having an outer skin, according to claim 15, wherein: the interleaf barrier layer comprises a reflective mineral coated sheet. 17. The insulation system for increasing the burn through resistance of an aircraft fuselage having an outer skin, according to claim 16, wherein: the foam is a polyimide foam and the polymeric film is a polyimide film. 18. The insulation system for increasing the burn through resistance of an aircraft fuselage having an outer skin, according to claim 12, wherein: the insulation layers are glass fiber insulation layers; and the multilayered insulation composite is encapsulated within a polymeric film. 19. The insulation system for increasing the burn through resistance of an aircraft fuselage having an outer skin, according to claim 18, wherein: the polymeric film is a polyimide film. 20. The insulation