WO2004091453A1 - An orbital implant applicator - Google Patents

An orbital implant applicator Download PDF

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Publication number
WO2004091453A1
WO2004091453A1 PCT/IB2004/050408 IB2004050408W WO2004091453A1 WO 2004091453 A1 WO2004091453 A1 WO 2004091453A1 IB 2004050408 W IB2004050408 W IB 2004050408W WO 2004091453 A1 WO2004091453 A1 WO 2004091453A1
Authority
WO
WIPO (PCT)
Prior art keywords
orbital implant
barrel
guide
applicator
orbital
Prior art date
Application number
PCT/IB2004/050408
Other languages
French (fr)
Inventor
Jeremias Daniél WILKINS
Michael Edward Thomas
Petrus Nicolaas Jacobus Gous
Paul Wilhelm Richter
Duncan Hope
Lewis Mark Levitz
Mark Minnaar
Jan Talma
Paul Roux
Original Assignee
Eyeborn (Proprietary) Limited
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Eyeborn (Proprietary) Limited filed Critical Eyeborn (Proprietary) Limited
Publication of WO2004091453A1 publication Critical patent/WO2004091453A1/en

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Classifications

    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61FFILTERS IMPLANTABLE INTO BLOOD VESSELS; PROSTHESES; DEVICES PROVIDING PATENCY TO, OR PREVENTING COLLAPSING OF, TUBULAR STRUCTURES OF THE BODY, e.g. STENTS; ORTHOPAEDIC, NURSING OR CONTRACEPTIVE DEVICES; FOMENTATION; TREATMENT OR PROTECTION OF EYES OR EARS; BANDAGES, DRESSINGS OR ABSORBENT PADS; FIRST-AID KITS
    • A61F2/00Filters implantable into blood vessels; Prostheses, i.e. artificial substitutes or replacements for parts of the body; Appliances for connecting them with the body; Devices providing patency to, or preventing collapsing of, tubular structures of the body, e.g. stents
    • A61F2/02Prostheses implantable into the body
    • A61F2/14Eye parts, e.g. lenses, corneal implants; Implanting instruments specially adapted therefor; Artificial eyes
    • A61F2/141Artificial eyes

Definitions

  • THIS INVENTION relates to an orbital implant applicator. It also relates to an orbital implant kit and to a method of inserting an orbital implant into an orbit.
  • An orbital implant is placed into the orbit or eye socket of a mammal, such as the human, to occupy volume following the loss of an eye.
  • a mammal such as the human
  • Such a mammal is thus one who has had an ocular enucleation or evisceration, or one who needs an orbital implant replacement.
  • the orbital implant is implanted to replace the contents of the eye.
  • the implant is placed into the eye muscle cone and the eye muscles are attached directly to the implant or, if the implant is covered or wrapped with tissue or artificial material, to the orbital implant wrapping. Instead, the eye muscles can be wrapped around the implant and secured together without direct attachment of the eye muscles to the orbital implant.
  • An anterior surface of the orbital implant is typically covered with tissue including the conjunctiva. Following a healing period, a prosthesis, i.e. an artificial eye, is located in position to obtain an artificial eye with natural appearance.
  • Such orbital implants may be spherical or they may have more complicated shapes, for example a posterior portion of the implant may be conical with channels to locate eye muscles, and other features to which the eye muscles can be attached.
  • the orbital implant may also be porous or non-porous.
  • the Applicant is aware of a method of inserting an orbital implant, in which two slightly overlapping sheets of a smooth synthetic plastics or polymeric material are inserted over the implant site, with the orbital implant then being placed in position and manually pushed into the orbit. Correctly positioning the orbital implant with this method is difficult. Once inserted, the sheets are removed from behind the orbital implant. During the removal of the sheets, care must be taken that the orientation and position of the orbital implant are not changed.
  • an orbital implant applicator which includes
  • a barrel or guide shaped and dimensioned to receive an orbital implant, the barrel or guide having an outlet at one end thereof sized to allow an orbital implant to pass therethrough;
  • an ejector or ejection means to eject an orbital implant received in the barrel or guide outwardly through the outlet of the barrel or guide.
  • the ejector or ejection means may include a plunger slidably received or receivable in the barrel or guide.
  • the plunger may have a tip which defines a bearing surface or seat for an orbital implant received in the barrel or guide.
  • the bearing surface or seat may be shaped to bear, over the entire surface of the bearing surface or seat, against a spherical surface of predetermined radius.
  • this configuration allows spreading of the load over a larger surface area of an orbital implant when an orbital implant is ejected from the barrel or guide by means of the plunger.
  • the plunger may define or include an inspection passage, having an outlet in its tip, to allow inspection of an orbital implant received in the barrel or guide. This feature may be important for correct application of orbital implants having to be implanted in a particular orientation in an eye socket or orbit.
  • the inspection passage extends coaxially with the plunger, providing the seat at the tip of the plunger with a central, circular bore.
  • the orbital implant applicator may include locking means or a lock to lock the plunger releasably in the barrel or guide, thereby to prevent inadvertent ejection of an orbital implant from the barrel or guide.
  • the barrel or guide is shaped and dimensioned snugly, but not tightly, to receive an orbital implant.
  • the barrel or guide or at least an end portion thereof defines a circular cylindrical interior surface, with an inside diameter ranging between about 18 mm and about 22 mm, e.g. about 20 mm.
  • the barrel typically has a length of between about 30 mm and about 60 mm, e.g. about 55 mm.
  • the orbital implant applicator may include a closure formation at least partially closing the outlet of the barrel or guide.
  • a closure formation at least partially closing the outlet of the barrel or guide.
  • this would prevent or inhibit contamination or damage to an orbital implant received in the barrel or guide, which is typically located inside the barrel or guide in the vicinity of the outlet but in front of the plunger.
  • the closure formation may comprise a plurality of petal-like members displaceable between an open condition and a closed condition. Typically, between about 3 and about 7, e.g. 5 petal-like members are included.
  • the petal-like members together may define a tip for the barrel or guide which is tapered, e.g. a blunt rounded tip, when in their closed condition.
  • this configuration assists in pushing the tip into eye socket tissue during insertion of an orbital implant into an orbit or eye socket.
  • the petal-like members may be biased towards their closed condition.
  • the petal -like members may together define a seat for an orbital implant received in the barrel or guide.
  • the seat may be shaped to correspond with a substantial surface portion of an orbital implant.
  • the seat is thus hemispherical, to accommodate or seat a spherical orbital implant.
  • the seat is conical, to accommodate or seat an orbital implant having a conical posterior surface.
  • the petal-like members may be defined by cuts or slits in the tip of the barrel or guide.
  • these cuts or slits extend longitudinally, rearwardly over the tip of the barrel or guide, and radially outwardly from a centre of the tip.
  • the cuts or slits stop short, in a radially outward direction, of a maximum diameter of the barrel or guide, thereby to assist in biasing the petal-like members toward their closed conditions.
  • the barrel or guide may be of a flexible synthetic plastics or polymeric material, e.g. polyurethane or linear low density polyurethane.
  • the material may have a Shore A hardness of between about Shore A 50 and about Shore A 90, e.g. about Shore A 70, and typically has a smooth external surface to facilitate insertion into eye socket tissue.
  • the lock or locking means may be configured to lock the plunger in a position where it is bearing with slight force against an orbital implant sandwiched between the plunger and the closure formation.
  • the slight force is sufficient to retain the implant with correct orientation (if the implant has a correct orientation) in the barrel, during normal handling of the applicator.
  • the locking means is in the form of a stop formation that can be clamped to the plunger, between an end of the barrel or guide remote from its outlet and a thumb pad of the plunger, preventing depression of the plunger into the barrel or guide.
  • the applicator may include depth markings to provide to a user thereof information on the depth to which the outlet of the barrel or guide has been inserted into an orbit or eye socket.
  • the depth markings may be provided externally on the barrel or guide, e.g. in the form of a plurality of longitudinally spaced annular marks on the barrel.
  • an orbital implant kit including
  • both the orbital implant applicator and the orbital implant are sterilized.
  • the orbital implant is typically matched to the applicator so that it can be inserted into an orbit by means of the applicator.
  • the implant is shaped and sized to be received or receivable inside the applicator.
  • the orbital implant applicator may be an applicator as hereinbefore described.
  • the orbital implant may be located inside the barrel or guide of the applicator.
  • the plunger may be releasably locked in position in the barrel or guide, with the orbital implant seated against the plunger and against the closure formation.
  • the kit may include a sterilized package within which the applicator and the orbital implant are packaged.
  • the orbital implant may be ejected from the barrel or guide by means of a plunger slidably received in the barrel or guide.
  • the orbital implant is ejected by keeping the plunger stationary and sliding the barrel or guide along the plunger away from the orbit. In this fashion, the orbital implant is inserted at the same depth into the orbit as the depth to which the barrel or guide was inserted into the orbit.
  • the method may include measuring the depth to which the end of the barrel or guide has been inserted into the orbit, prior to ejecting the orbital implant. Measuring the depth may include using depth markings located on the barrel or guide.
  • the barrel may form part of an orbital implant applicator as hereinbefore described.
  • reference numeral 10 generally indicates an orbital implant applicator in accordance with the invention, which is associated with an orbital implant 12.
  • the applicator 10 includes a barrel 14 and ejection means in the form of a plunger
  • the barrel 14 is moulded from polyurethane or LLDPE and has a length of about 55 mm and an internal diameter of about 20 mm.
  • the material of the barrel 14 has a Shore A hardness of about 70.
  • the barrel 14 is circular cylindrical with a tip 18 defining an outlet at one end thereof and an oval flange 20 at an opposite end thereof.
  • the outlet defined by the tip 18 is closed by a closure formation in the form of five petal-like members 22.
  • the petal-like members 22 are defined by cuts or slits' 24 in the tip 18 of the barrel 14 and are displaceable between an open condition in which they are forced apart and substantially straightened, and a closed condition in which they are curved, as shown in the drawing.
  • the cuts or slits 24 extend longitudinally, rearwardly over the tip 18, and radially outwardly from a centre of the tip 18, as can be clearly seen in the drawing.
  • the cuts or slits 24 stop short, in a radially outward direction, of a maximum diameter of the barrel 14. The Applicant has found that this arrangement assists in biasing the petal-like members 22 toward their closed condition as shown in the drawing.
  • the plunger 16 includes a shank 26 with an oval thumb pad 28 at one end of the shank 26.
  • the entire plunger 16 is moulded from polyethylene, which is substantially more rigid than the polyurethane or LLDPE from which the barrel 14 is moulded.
  • the shank 26 is circular cylindrical and is slidably receivable inside the barrel 14 in syringe fashion. An end portion of the shank 26, adjacent the thumb pad 28, is of reduced diameter compared to an end portion thereof remote from the thumb pad 28.
  • An inspection passage 30 extends longitudinally through the shank 26 and opens out in a tip 32 thereof and in the thumb pad 28. As a result of the inspection passage 30 opening out in the tip 32, the tip 32 defines an annular seat to bear against the orbital implant 12.
  • the annular seat defined by the tip 32 is chamfered, as can be clearly seen in the drawing, in use to spread the load over a larger surface area of the orbital implant 12 when the orbital implant 12 is ejected from the barrel 14 by means of the plunger 16.
  • a lock or locking means in the form of a stop formation 34 is provided to lock the plunger 16 in a particular longitudinal position in the barrel 14.
  • the stop formation 34 includes a split circular cylindrical body 36 of a rigid plastics material.
  • the body 36 is shaped to clip around and thus to receive the portion of the shank 26 of reduced diameter.
  • Two diverging gripping wings 38 are integrally moulded with the body 36 and extend from diagonally opposite portions of the body 36.
  • the gripping wings 38 allow easy manipulation of the stop formation 34.
  • the gripping wings 38 are positioned such that, when they are gripped between a thumb and an index finger with slight force, the body 36 opens up slightly to facilitate clipping of the body 36 onto the shank 26, or removal of the body 36 from the shank 26.
  • One hook-like receiving formation 40 is shaped and dimensioned to receive a peripheral portion of the flange 20 when the body 36 is clamped onto the shank 26.
  • the other hook-like receiving formation 40 is shaped and dimensioned to receive a peripheral portion of the thumb pad 28 when the body 36 is clamped to the shank 26.
  • the orbital implant 12 is spherical and has a diameter slightly less that the diameter of the barrel 14, thus allowing the implant 12 to be snugly but not tightly received inside the barrel 14.
  • the orbital implant 12 and the applicator 10 are supplied together as a kit in a sterilized package and the invention thus extends to such an orbital implant kit.
  • the kit the orbital implant 12 is received inside the barrel 14 and is sandwiched between the tip 32 of the plunger 16 and the tip 18 of the barrel 14, or more specifically, the petal-like members 22.
  • the petal-like members 22 define a hemispherical seat against which the orbital implant 12 is bearing.
  • the plunger 16 is pushing with slight force against the orbital implant 12 so that the petal-like members 22 are only slightly forced apart.
  • the stop formation 34 is clamped by means of the body 36 to the reduced diameter portion of the shank 26 of the plunger 16 and is dimensioned to ensure that the slight force imparted by the plunger 16 on the orbital implant 12 is maintained.
  • the stop formation 34 being clipped to the plunger 16, and being clipped to the thumb pad 28 of the plunger 16 and the flange 20 of the barrel 14, further depression of the plunger 16 into the barrel 14, or retraction of the plunger 16 from the barrel 14, is prevented.
  • the inspection passage 30 can be used to inspect the orientation of the orbital implant 12 sandwiched between the tip 32 of the shank 26 and the petal-like members 22.
  • Some orbital implants such as the orbital implant 12 shown in the drawing, must be implanted in a particular orientation in an eye socket or orbit.
  • the orbital implant 12 has an anterior cap 40 and the orbital implant 12 must thus be planted into an orbit such that the anterior cap 40 faces outwardly through the mouth of the orbit.
  • the inspection passage 30 it is possible to inspect the orbital implant 12 inside the barrel 14 to ensure that the anterior cap 40 is fully visible through the inspection passage 30, which would mean a correct orientation, before the orbital implant 12 is inserted into an orbit.
  • the sterilized package within which the orbital implant 12 and the orbital implant applicator 10 are supplied is opened only once the orbital implant site has been prepared by the physician.
  • the physician inspects, if necessary, the orbital implant 12 through the inspection passage 30 to ensure that it is correctly orientated inside the barrel 14 and the rounded tip 18 of the barrel 14 is then pushed into the orbit tissue to the required depth.
  • the barrel 14 may include depth markings, such as longitudinally spaced annular rings.
  • the stop formation 34 is removed and the barrel 14 is pulled by means of the flange 20 toward the thumb pad 28 thereby to slide the plunger 16 deeper into the barrel 14 until the orbital implant 12 has been ejected through the outlet in the tip 18.
  • the orbital implant applicator 10 is removed leaving the orbital implant 12 correctly positioned in the eye socket tissue.

Abstract

An orbital implant applicator (10) includes a barrel or guide (14) shaped and dimensioned to receive an orbital implant (12). The barrel or guide (14) has an outlet at one end thereof sized to allow an orbital implant (12) to pass therethrough. An ejector or ejection means (16) to eject an orbital implant (12) received in the barrel or guide (14) outwardly through the outlet of the barrel or guide (14) is also provided.

Description

Description AN ORBITAL IMPLANT APPLICATOR
[1] THIS INVENTION relates to an orbital implant applicator. It also relates to an orbital implant kit and to a method of inserting an orbital implant into an orbit.
[2] An orbital implant is placed into the orbit or eye socket of a mammal, such as the human, to occupy volume following the loss of an eye. Such a mammal is thus one who has had an ocular enucleation or evisceration, or one who needs an orbital implant replacement. In the case of evisceration, the orbital implant is implanted to replace the contents of the eye. In the case of enucleation, the implant is placed into the eye muscle cone and the eye muscles are attached directly to the implant or, if the implant is covered or wrapped with tissue or artificial material, to the orbital implant wrapping. Instead, the eye muscles can be wrapped around the implant and secured together without direct attachment of the eye muscles to the orbital implant. An anterior surface of the orbital implant is typically covered with tissue including the conjunctiva. Following a healing period, a prosthesis, i.e. an artificial eye, is located in position to obtain an artificial eye with natural appearance.
[3] Such orbital implants may be spherical or they may have more complicated shapes, for example a posterior portion of the implant may be conical with channels to locate eye muscles, and other features to which the eye muscles can be attached. The orbital implant may also be porous or non-porous.
[4] In view of the above, as will be appreciated, when inserting an orbital implant in the eye muscle cone, it may be necessary to achieve deep penetration as well as correctly to orientate the orbital implant. The insertion procedure is complicated by the confined space within which the physician has to work, particularly if it is necessary to achieve correct orientation for orbital implants with more complicated features. In the case of orbital implants which exhibit high surface roughness and porosity, such as implants of the integrated type, tissue adherence due to the hygroscopicity of the orbital implant material also causes problems and may make it difficult to achieve correct orientation of the implant.
[5] The Applicant is aware of a method of inserting an orbital implant, in which two slightly overlapping sheets of a smooth synthetic plastics or polymeric material are inserted over the implant site, with the orbital implant then being placed in position and manually pushed into the orbit. Correctly positioning the orbital implant with this method is difficult. Once inserted, the sheets are removed from behind the orbital implant. During the removal of the sheets, care must be taken that the orientation and position of the orbital implant are not changed.
[6] It is an object of the present invention to at least alleviate the problems currently ex- perienced when an orbital implant is inserted into an orbit or eye socket.
[7] According to one aspect of the invention, there is provided an orbital implant applicator which includes
[8] a barrel or guide shaped and dimensioned to receive an orbital implant, the barrel or guide having an outlet at one end thereof sized to allow an orbital implant to pass therethrough; and
[9] an ejector or ejection means to eject an orbital implant received in the barrel or guide outwardly through the outlet of the barrel or guide.
[10] The ejector or ejection means may include a plunger slidably received or receivable in the barrel or guide.
[11] The plunger may have a tip which defines a bearing surface or seat for an orbital implant received in the barrel or guide. The bearing surface or seat may be shaped to bear, over the entire surface of the bearing surface or seat, against a spherical surface of predetermined radius. Advantageously, this configuration allows spreading of the load over a larger surface area of an orbital implant when an orbital implant is ejected from the barrel or guide by means of the plunger.
[12] The plunger may define or include an inspection passage, having an outlet in its tip, to allow inspection of an orbital implant received in the barrel or guide. This feature may be important for correct application of orbital implants having to be implanted in a particular orientation in an eye socket or orbit.
[13] Preferably, the inspection passage extends coaxially with the plunger, providing the seat at the tip of the plunger with a central, circular bore.
[14] The orbital implant applicator may include locking means or a lock to lock the plunger releasably in the barrel or guide, thereby to prevent inadvertent ejection of an orbital implant from the barrel or guide.
[15] Preferably, the barrel or guide is shaped and dimensioned snugly, but not tightly, to receive an orbital implant. Typically, the barrel or guide or at least an end portion thereof defines a circular cylindrical interior surface, with an inside diameter ranging between about 18 mm and about 22 mm, e.g. about 20 mm. The barrel typically has a length of between about 30 mm and about 60 mm, e.g. about 55 mm.
[16] The orbital implant applicator may include a closure formation at least partially closing the outlet of the barrel or guide. Advantageously, this would prevent or inhibit contamination or damage to an orbital implant received in the barrel or guide, which is typically located inside the barrel or guide in the vicinity of the outlet but in front of the plunger.
[17] The closure formation may comprise a plurality of petal-like members displaceable between an open condition and a closed condition. Typically, between about 3 and about 7, e.g. 5 petal-like members are included. The petal-like members together may define a tip for the barrel or guide which is tapered, e.g. a blunt rounded tip, when in their closed condition. Advantageously, this configuration assists in pushing the tip into eye socket tissue during insertion of an orbital implant into an orbit or eye socket.
[18] The petal-like members may be biased towards their closed condition.
[19] In their closed condition, the petal -like members may together define a seat for an orbital implant received in the barrel or guide. The seat may be shaped to correspond with a substantial surface portion of an orbital implant. In one embodiment of the invention, the seat is thus hemispherical, to accommodate or seat a spherical orbital implant. In another embodiment of the invention, the seat is conical, to accommodate or seat an orbital implant having a conical posterior surface.
[20] The petal-like members may be defined by cuts or slits in the tip of the barrel or guide. Typically, these cuts or slits extend longitudinally, rearwardly over the tip of the barrel or guide, and radially outwardly from a centre of the tip. Preferably, the cuts or slits stop short, in a radially outward direction, of a maximum diameter of the barrel or guide, thereby to assist in biasing the petal-like members toward their closed conditions.
[21] The barrel or guide may be of a flexible synthetic plastics or polymeric material, e.g. polyurethane or linear low density polyurethane. The material may have a Shore A hardness of between about Shore A 50 and about Shore A 90, e.g. about Shore A 70, and typically has a smooth external surface to facilitate insertion into eye socket tissue.
[22] The lock or locking means may be configured to lock the plunger in a position where it is bearing with slight force against an orbital implant sandwiched between the plunger and the closure formation. Preferably, the slight force is sufficient to retain the implant with correct orientation (if the implant has a correct orientation) in the barrel, during normal handling of the applicator.
[23] In one embodiment of the invention, the locking means is in the form of a stop formation that can be clamped to the plunger, between an end of the barrel or guide remote from its outlet and a thumb pad of the plunger, preventing depression of the plunger into the barrel or guide.
[24] The applicator may include depth markings to provide to a user thereof information on the depth to which the outlet of the barrel or guide has been inserted into an orbit or eye socket. The depth markings may be provided externally on the barrel or guide, e.g. in the form of a plurality of longitudinally spaced annular marks on the barrel.
[25] According to another aspect of the invention, there is provided an orbital implant kit, the kit including
[26] an orbital implant applicator; and
[27] an orbital implant.
[28] Preferably, both the orbital implant applicator and the orbital implant are sterilized. The orbital implant is typically matched to the applicator so that it can be inserted into an orbit by means of the applicator. Thus, typically, the implant is shaped and sized to be received or receivable inside the applicator.
[29] The orbital implant applicator may be an applicator as hereinbefore described.
[30] The orbital implant may be located inside the barrel or guide of the applicator. The plunger may be releasably locked in position in the barrel or guide, with the orbital implant seated against the plunger and against the closure formation.
[31] The kit may include a sterilized package within which the applicator and the orbital implant are packaged.
[32] According to a further aspect of the invention, there is provided a method of inserting an orbital implant into an orbit, the method including
[33] inserting an end of a barrel or guide, within which the orbital implant is received, into an orbit; and
[34] guidingly ejecting the orbital implant from the barrel or guide into the orbit.
[35] The orbital implant may be ejected from the barrel or guide by means of a plunger slidably received in the barrel or guide. Typically, the orbital implant is ejected by keeping the plunger stationary and sliding the barrel or guide along the plunger away from the orbit. In this fashion, the orbital implant is inserted at the same depth into the orbit as the depth to which the barrel or guide was inserted into the orbit.
[36] The method may include measuring the depth to which the end of the barrel or guide has been inserted into the orbit, prior to ejecting the orbital implant. Measuring the depth may include using depth markings located on the barrel or guide.
[37] The barrel may form part of an orbital implant applicator as hereinbefore described.
[38] The invention will now be described, by way of example only, with reference to the single accompanying diagrammatic drawing which shows an exploded three-dimensional view of an orbital implant applicator in accordance with the invention, and an orbital implant.
[39] In the drawing, reference numeral 10 generally indicates an orbital implant applicator in accordance with the invention, which is associated with an orbital implant 12.
[40] The applicator 10 includes a barrel 14 and ejection means in the form of a plunger
16 which is slidably receivable in the barrel 14.
[41] The barrel 14 is moulded from polyurethane or LLDPE and has a length of about 55 mm and an internal diameter of about 20 mm. The material of the barrel 14 has a Shore A hardness of about 70.
[42] The barrel 14 is circular cylindrical with a tip 18 defining an outlet at one end thereof and an oval flange 20 at an opposite end thereof. The outlet defined by the tip 18 is closed by a closure formation in the form of five petal-like members 22. The petal-like members 22 are defined by cuts or slits' 24 in the tip 18 of the barrel 14 and are displaceable between an open condition in which they are forced apart and substantially straightened, and a closed condition in which they are curved, as shown in the drawing. The cuts or slits 24 extend longitudinally, rearwardly over the tip 18, and radially outwardly from a centre of the tip 18, as can be clearly seen in the drawing. The cuts or slits 24 stop short, in a radially outward direction, of a maximum diameter of the barrel 14. The Applicant has found that this arrangement assists in biasing the petal-like members 22 toward their closed condition as shown in the drawing.
[43] The plunger 16 includes a shank 26 with an oval thumb pad 28 at one end of the shank 26. The entire plunger 16 is moulded from polyethylene, which is substantially more rigid than the polyurethane or LLDPE from which the barrel 14 is moulded.
[44] The shank 26 is circular cylindrical and is slidably receivable inside the barrel 14 in syringe fashion. An end portion of the shank 26, adjacent the thumb pad 28, is of reduced diameter compared to an end portion thereof remote from the thumb pad 28. An inspection passage 30 extends longitudinally through the shank 26 and opens out in a tip 32 thereof and in the thumb pad 28. As a result of the inspection passage 30 opening out in the tip 32, the tip 32 defines an annular seat to bear against the orbital implant 12. The annular seat defined by the tip 32 is chamfered, as can be clearly seen in the drawing, in use to spread the load over a larger surface area of the orbital implant 12 when the orbital implant 12 is ejected from the barrel 14 by means of the plunger 16.
[45] A lock or locking means, in the form of a stop formation 34 is provided to lock the plunger 16 in a particular longitudinal position in the barrel 14. The stop formation 34 includes a split circular cylindrical body 36 of a rigid plastics material. The body 36 is shaped to clip around and thus to receive the portion of the shank 26 of reduced diameter. Two diverging gripping wings 38 are integrally moulded with the body 36 and extend from diagonally opposite portions of the body 36. The gripping wings 38 allow easy manipulation of the stop formation 34. As will be appreciated, the gripping wings 38 are positioned such that, when they are gripped between a thumb and an index finger with slight force, the body 36 opens up slightly to facilitate clipping of the body 36 onto the shank 26, or removal of the body 36 from the shank 26.
[46] Two spaced hook-like receiving formations 40 are integrally moulded with the body
36. One hook-like receiving formation 40 is shaped and dimensioned to receive a peripheral portion of the flange 20 when the body 36 is clamped onto the shank 26. The other hook-like receiving formation 40 is shaped and dimensioned to receive a peripheral portion of the thumb pad 28 when the body 36 is clamped to the shank 26.
[47] The orbital implant 12 is spherical and has a diameter slightly less that the diameter of the barrel 14, thus allowing the implant 12 to be snugly but not tightly received inside the barrel 14. Typically, the orbital implant 12 and the applicator 10 are supplied together as a kit in a sterilized package and the invention thus extends to such an orbital implant kit. In the kit, the orbital implant 12 is received inside the barrel 14 and is sandwiched between the tip 32 of the plunger 16 and the tip 18 of the barrel 14, or more specifically, the petal-like members 22. The petal-like members 22 define a hemispherical seat against which the orbital implant 12 is bearing. The plunger 16 is pushing with slight force against the orbital implant 12 so that the petal-like members 22 are only slightly forced apart. The stop formation 34 is clamped by means of the body 36 to the reduced diameter portion of the shank 26 of the plunger 16 and is dimensioned to ensure that the slight force imparted by the plunger 16 on the orbital implant 12 is maintained. As will be appreciated, with the stop formation 34 being clipped to the plunger 16, and being clipped to the thumb pad 28 of the plunger 16 and the flange 20 of the barrel 14, further depression of the plunger 16 into the barrel 14, or retraction of the plunger 16 from the barrel 14, is prevented.
[48] The inspection passage 30 can be used to inspect the orientation of the orbital implant 12 sandwiched between the tip 32 of the shank 26 and the petal-like members 22. Some orbital implants, such as the orbital implant 12 shown in the drawing, must be implanted in a particular orientation in an eye socket or orbit. The orbital implant 12 has an anterior cap 40 and the orbital implant 12 must thus be planted into an orbit such that the anterior cap 40 faces outwardly through the mouth of the orbit. By means of the inspection passage 30, it is possible to inspect the orbital implant 12 inside the barrel 14 to ensure that the anterior cap 40 is fully visible through the inspection passage 30, which would mean a correct orientation, before the orbital implant 12 is inserted into an orbit.
[49] In use, the sterilized package within which the orbital implant 12 and the orbital implant applicator 10 are supplied, is opened only once the orbital implant site has been prepared by the physician. The physician then inspects, if necessary, the orbital implant 12 through the inspection passage 30 to ensure that it is correctly orientated inside the barrel 14 and the rounded tip 18 of the barrel 14 is then pushed into the orbit tissue to the required depth. In order to assist the surgeon to determine when the tip 18 of the barrel 14 has been inserted to the required depth, the barrel 14 may include depth markings, such as longitudinally spaced annular rings. Once the barrel 14 has been inserted to the required depth, the stop formation 34 is removed and the barrel 14 is pulled by means of the flange 20 toward the thumb pad 28 thereby to slide the plunger 16 deeper into the barrel 14 until the orbital implant 12 has been ejected through the outlet in the tip 18. Once the implant 12 has been deposited, the orbital implant applicator 10 is removed leaving the orbital implant 12 correctly positioned in the eye socket tissue. [50] The Applicant believes that the invention provides a simple but efficient device, and an improved method, for inserting an orbital implant into an orbit.

Claims

Claims
[1] An orbital implant applicator which includes a barrel or guide shaped and dimensioned to receive an orbital implant, the barrel or guide having an outlet at one end thereof sized to allow an orbital implant to pass therethrough; and an ejector or ejection means to eject an orbital implant received in the barrel or guide outwardly through the outlet of the barrel or guide. [2] The orbital implant applicator as claimed in claim 1, in which the ejector or ejection means includes a plunger slidably received or receivable in the barrel or guide. [3] The orbital implant applicator as claimed in claim 2, in which the plunger has a tip which defines a bearing surface or seat for an orbital implant received in the barrel or guide, the bearing surface or seat being shaped to bear, over the entire surface of the bearing surface or seat, against a spherical surface of predetermined radius. [4] The orbital implant applicator as claimed in claim 2 or claim 3, in which the plunger defines an inspection passage, having an outlet in its tip, to allow inspection of an orbital implant received in the barrel or guide. [5] The orbital implant applicator as claimed in any one of claims 2 to 4 inclusive, which includes locking means or a lock to lock the plunger releasably in the barrel or guide, thereby to prevent inadvertent ejection of an orbital implant from the barrel or guide. [6] The orbital implant applicator as claimed in any one of the preceding claims, in which the barrel or guide is shaped and dimensioned snugly, but not tightly, to receive an orbital implant, the barrel or guide or at least an end portion thereof defining a circular cylindrical interior surface. [7] The orbital implant applicator as claimed in any one of the preceding claims, which includes a closure formation at least partially closing the outlet of the barrel or guide. [8] The orbital implant applicator as claimed in claim 7, in which the closure formation comprises a plurality of petal-like members displaceable between an open condition and a closed condition. [9] The orbital implant applicator as claimed in claim 8, in which the petal-like members together define a tip for the barrel or guide which is tapered, when in their closed condition. [10] The orbital implant applicator as claimed in claim 8 or claim 9, in which the petal-like members are biased towards their closed condition. [11] The orbital implant applicator as claimed in any one of claims 8 to 10 inclusive in which, in their closed condition, the petal-like members together define a seat for an orbital implant received in the barrel or guide. [12] The orbital implant applicator as claimed in claim 5 and claim 7, in which the lock or locking means is configured to lock the plunger in a position where it is bearing with slight force against an orbital implant sandwiched between the plunger and the closure formation. [13] The orbital implant applicator as claimed in any one of the preceding claims, which includes depth markings to provide to a user thereof information on the depth to which the outlet of the barrel or guide has been inserted into an orbit or eye socket. [14] An orbital implant kit, the kit including an orbital implant applicator; and an orbital implant. [15] The kit as claimed in claim 14, in which both the orbital implant applicator and the orbital implant are sterilized. [16] The kit as claimed in claim 14 or claim 15, in which the orbital implant applicator is an applicator as claimed in any one of claims 1 to 13 inclusive. [17] The kit as claimed in any one of claims 14 to 16 inclusive, in which the orbital implant applicator is an applicator as claimed in any one of claims 7 to 11 inclusive and in which the orbital implant is located inside the barrel or guide of the applicator, with the plunger being releasably locked in position in the barrel or guide, and with the orbital implant seated against the plunger and against the closure formation. [18] A method of inserting an orbital implant into an orbit, the method including inserting an end of a barrel or guide, within which the orbital implant is received, into an orbit; and guidingly ejecting the orbital implant from the barrel or guide into the orbit. [19] The method as claimed in claim 18, in which the orbital implant is ejected from the barrel or guide by means of a plunger slidably received in the barrel or guide. [20] The method as claimed in claim 18 or claim 19, which includes measuring the depth to which the end of the barrel or guide has been inserted into the orbit, prior to ejecting the orbital implant, measuring the depth including using depth markings located on the barrel or guide.
PCT/IB2004/050408 2003-04-15 2004-04-08 An orbital implant applicator WO2004091453A1 (en)

Applications Claiming Priority (2)

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ZA2003/2961 2003-04-15
ZA200302961 2003-04-15

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WO2004091453A1 true WO2004091453A1 (en) 2004-10-28

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WO2014165124A1 (en) * 2013-03-12 2014-10-09 Oculeve, Inc. Implant delivery devices, systems, and methods
US9687652B2 (en) 2014-07-25 2017-06-27 Oculeve, Inc. Stimulation patterns for treating dry eye
US9737712B2 (en) 2014-10-22 2017-08-22 Oculeve, Inc. Stimulation devices and methods for treating dry eye
US9764150B2 (en) 2014-10-22 2017-09-19 Oculeve, Inc. Contact lens for increasing tear production
US9821159B2 (en) 2010-11-16 2017-11-21 The Board Of Trustees Of The Leland Stanford Junior University Stimulation devices and methods
US10143846B2 (en) 2010-11-16 2018-12-04 The Board Of Trustees Of The Leland Stanford Junior University Systems and methods for treatment of dry eye
US10207108B2 (en) 2014-10-22 2019-02-19 Oculeve, Inc. Implantable nasal stimulator systems and methods
US10238861B2 (en) 2013-04-19 2019-03-26 Oculeve, Inc. Nasal stimulation devices and methods for treating dry eye
US10252048B2 (en) 2016-02-19 2019-04-09 Oculeve, Inc. Nasal stimulation for rhinitis, nasal congestion, and ocular allergies
US10426958B2 (en) 2015-12-04 2019-10-01 Oculeve, Inc. Intranasal stimulation for enhanced release of ocular mucins and other tear proteins
US10610095B2 (en) 2016-12-02 2020-04-07 Oculeve, Inc. Apparatus and method for dry eye forecast and treatment recommendation
US10799696B2 (en) 2014-02-25 2020-10-13 Oculeve, Inc. Polymer formulations for nasolacrimal stimulation
US10918864B2 (en) 2016-05-02 2021-02-16 Oculeve, Inc. Intranasal stimulation for treatment of meibomian gland disease and blepharitis

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Cited By (27)

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Publication number Priority date Publication date Assignee Title
US10328262B2 (en) 2010-11-16 2019-06-25 The Board Of Trustees Of The Leland Stanford Junior University Stimulation devices and methods
US10722718B2 (en) 2010-11-16 2020-07-28 The Board Of Trustees Of The Leland Stanford Junior University Systems and methods for treatment of dry eye
US11771908B2 (en) 2010-11-16 2023-10-03 The Board Of Trustees Of The Leland Stanford Junior University Systems and methods for treatment of dry eye
US9821159B2 (en) 2010-11-16 2017-11-21 The Board Of Trustees Of The Leland Stanford Junior University Stimulation devices and methods
US10143846B2 (en) 2010-11-16 2018-12-04 The Board Of Trustees Of The Leland Stanford Junior University Systems and methods for treatment of dry eye
US10835748B2 (en) 2010-11-16 2020-11-17 Oculeve, Inc. Stimulation devices and methods
US9717627B2 (en) 2013-03-12 2017-08-01 Oculeve, Inc. Implant delivery devices, systems, and methods
WO2014165124A1 (en) * 2013-03-12 2014-10-09 Oculeve, Inc. Implant delivery devices, systems, and methods
US10537469B2 (en) 2013-03-12 2020-01-21 Oculeve, Inc. Implant delivery devices, systems, and methods
US10967173B2 (en) 2013-04-19 2021-04-06 Oculeve, Inc. Nasal stimulation devices and methods for treating dry eye
US10238861B2 (en) 2013-04-19 2019-03-26 Oculeve, Inc. Nasal stimulation devices and methods for treating dry eye
US10799695B2 (en) 2013-04-19 2020-10-13 Oculeve, Inc. Nasal stimulation devices and methods
US10835738B2 (en) 2013-04-19 2020-11-17 Oculeve, Inc. Nasal stimulation devices and methods
US10799696B2 (en) 2014-02-25 2020-10-13 Oculeve, Inc. Polymer formulations for nasolacrimal stimulation
US10722713B2 (en) 2014-07-25 2020-07-28 Oculeve, Inc. Stimulation patterns for treating dry eye
US9687652B2 (en) 2014-07-25 2017-06-27 Oculeve, Inc. Stimulation patterns for treating dry eye
US10780273B2 (en) 2014-10-22 2020-09-22 Oculeve, Inc. Stimulation devices and methods for treating dry eye
US10610695B2 (en) 2014-10-22 2020-04-07 Oculeve, Inc. Implantable device for increasing tear production
US10207108B2 (en) 2014-10-22 2019-02-19 Oculeve, Inc. Implantable nasal stimulator systems and methods
US10112048B2 (en) 2014-10-22 2018-10-30 Oculeve, Inc. Stimulation devices and methods for treating dry eye
US9764150B2 (en) 2014-10-22 2017-09-19 Oculeve, Inc. Contact lens for increasing tear production
US9737712B2 (en) 2014-10-22 2017-08-22 Oculeve, Inc. Stimulation devices and methods for treating dry eye
US10426958B2 (en) 2015-12-04 2019-10-01 Oculeve, Inc. Intranasal stimulation for enhanced release of ocular mucins and other tear proteins
US10252048B2 (en) 2016-02-19 2019-04-09 Oculeve, Inc. Nasal stimulation for rhinitis, nasal congestion, and ocular allergies
US10940310B2 (en) 2016-02-19 2021-03-09 Oculeve, Inc. Nasal stimulation for rhinitis, nasal congestion, and ocular allergies
US10918864B2 (en) 2016-05-02 2021-02-16 Oculeve, Inc. Intranasal stimulation for treatment of meibomian gland disease and blepharitis
US10610095B2 (en) 2016-12-02 2020-04-07 Oculeve, Inc. Apparatus and method for dry eye forecast and treatment recommendation

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