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US20040159745A1 - Attachment apparatus for injection-molded frameless canopies - Google Patents

Attachment apparatus for injection-molded frameless canopies Download PDF

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Publication number
US20040159745A1
US20040159745A1 US10/367,064 US36706403A US2004159745A1 US 20040159745 A1 US20040159745 A1 US 20040159745A1 US 36706403 A US36706403 A US 36706403A US 2004159745 A1 US2004159745 A1 US 2004159745A1
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US
United States
Prior art keywords
canopy
rail
cavity
handle
attachment components
Prior art date
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Abandoned
Application number
US10/367,064
Inventor
Jeffrey Wood
Terry Sewell
Steven Miener
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing Co
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to US10/367,064 priority Critical patent/US20040159745A1/en
Assigned to BOEING COMPANY, THE reassignment BOEING COMPANY, THE ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: MIENER, STEVEN J., SEWELL, TERRY A., WOOD, JEFFREY H.
Priority to PCT/US2004/003476 priority patent/WO2005035359A2/en
Assigned to UNITED STATES AIR FORCE reassignment UNITED STATES AIR FORCE CONFIRMATORY LICENSE (SEE DOCUMENT FOR DETAILS). Assignors: THE BOEING COMPANY
Publication of US20040159745A1 publication Critical patent/US20040159745A1/en
Priority to US10/960,144 priority patent/US7040577B2/en
Abandoned legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/14Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
    • B64C1/1476Canopies; Windscreens or similar transparent elements
    • B64C1/1492Structure and mounting of the transparent elements in the window or windscreen
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10Manufacturing or assembling aircraft, e.g. jigs therefor

Definitions

  • This invention relates generally to vehicles with canopies and, more specifically, to closing mechanisms for injection-molded canopies.
  • Modern aircraft canopies contain many parts. A transparent portion of the canopy may be replaced several times during the life of an aircraft due to scratches and general deterioration. Replacement of the transparent portion entails frame disassembly and reassembly. This is time-consuming, labor intensive, and costly.
  • a frame provides structural stiffness and strong, secure, attachment points for hinges and latches.
  • the viable frameless canopy system must include a method for latching.
  • Prior latching methods include a male hook or pin located on the aircraft structure or canopy frame and a female receiver on the canopy frame structure or aircraft structure respectively. Such discrete latching methods produce concentrated loads, which cause bearing stress in the transparency in the region of the latch.
  • the present invention provides an apparatus and method for latching a canopy to a vehicle, such as an aircraft, that avoids plastic creep or crazing due to concentrated loads.
  • the apparatus includes first attachment components that are at least partially embedded within an injection-molded canopy and second attachment components that are connected to the canopy rail for attaching to the one or more first attachment components and thereby attaching the canopy to the canopy rail.
  • the first component includes a shaft with two ends and one or more knobs attached to the ends of the shaft.
  • the knobs are molded into the canopy, and the shaft is exposed within a cavity formed by the canopy. The cavity is opened at a base of the canopy.
  • the first component includes a hook at least partially embedded within the canopy. A portion of the hook protrudes from a base edge of the canopy.
  • FIG. 1 illustrates an injection-molded frameless canopy attached to a vehicle in accordance with the present invention
  • FIGS. 2 and 3 illustrate x-ray perspective views of a first embodiment for attaching the canopy to the vehicle
  • FIG. 4 illustrates a perspective view of a canopy that includes an attachment mechanism in accordance with the second embodiment of the present invention
  • FIG. 5 illustrates an exploded perspective view of the handrail attachment mechanism shown in FIG. 4;
  • FIG. 6 illustrates a cutaway side view of the canopy of FIG. 4 attached to a canopy rail
  • FIG. 7 illustrates a cutaway perspective view of the system shown in FIG. 6;
  • FIG. 8 illustrates a perspective view of an aircraft that includes the canopy shown in FIG. 4.
  • FIGS. 9 - 11 illustrate cutaway perspective views of a canopy that includes an attachment mechanism in accordance with a third embodiment of the present invention.
  • the present invention is an injection-molded canopy with canopy attachment devices that are inserted into the canopy during an injection molding process.
  • an exemplary canopy 20 attaches to a canopy rail 24 that surrounds a cockpit 26 of a vehicle 28 , such as an aircraft.
  • FIGS. 2 and 3 illustrate a first embodiment of an attachment device that is molded into an injection-molded canopy 30 .
  • the attachment device is suitably a hook 32 .
  • the hook 32 is substantially U-shaped.
  • a first section 34 of the hook 32 expands in length away from a centerline of the hook 30 .
  • a first section 34 is embedded within the canopy 30 during the injection molding process.
  • a second section 42 of the hook 32 is exposed below the canopy 30 .
  • the second section 42 includes a claw 44 and a U-shaped indent caused by the claw 44 and the first section 34 .
  • a canopy rail 50 includes a canopy-receiving channel 52 that receives the canopy 30 and the mounted hook 32 .
  • the canopy rail 50 is attached around a cockpit in a conventional manner.
  • One of the walls of the channel 52 suitably includes an inflatable seal 58 that is attached to a pneumatic or hydraulic system (not shown) that is included within the vehicle.
  • the inflatable seal 58 inflates when the canopy 30 is inserted into the channel 52 and locked in place in the canopy rail 50 .
  • the inflatable seal 58 provides a moisture and air pressure seal between the vehicle cockpit and the environment outside of the cockpit.
  • the canopy 30 is first inserted into the rail 50 .
  • the canopy 30 is moved by a support structure (not shown), thereby making contact between the U-shaped cutout of the hook 32 and a locking mechanism (not shown) that is included as part of the canopy rail 50 .
  • FIG. 4 illustrates a perspective view of a second embodiment of an attachment device that is embedded within a canopy 100 during an injection molding process.
  • the attachment mechanisms are imbedded handle devices 102 .
  • the imbedded handle devices 102 include a U-shaped handle 104 and two pair of handle end holders 106 .
  • Each pair of the handle end holders 106 includes a first part 106 a and a second part 106 b .
  • Each of the parts 106 a,b includes a cavity that forms a cavity 110 that receives an end of the handle 104 when the parts 106 a,b are combined.
  • the parts 106 a,b are attached to each other by a fastener 112 , such as without limitation a screw or a bolt, that is received through the first part 106 a and is securely mounted into the second part 106 b .
  • a fastener 112 such as without limitation a screw or a bolt
  • One or more securing pins 116 are received by respective pinholes in the first part 106 a and are received into receiving cavities (not shown) within the second part 106 b .
  • the pins 116 help reduce any rotational movement between the first and second parts 106 a,b .
  • other fastener mechanisms such as without limitation an adhesive, may be used for attaching the parts 106 a,b .
  • Each end of the handle 104 includes a top section 120 that is wider from a centerline point than a bottom section 122 .
  • the cavities 110 include chambers sized to receive each of the top and bottom sections 120 and 122 .
  • the end holders 106 are then inserted in a mold for the injection-molded canopy 100 such that when the molding of the canopy 100 is complete, the pairs of end holders 106 are surrounded by the molded canopy 100 and only the handles 104 protrude out of the base of the canopy 100 .
  • the parts 106 a,b are trapezoidal in shape with a first length at the side that includes the cavity 110 that is smaller than a second length of the side that is opposite the side that includes the cavity 110 . Therefore, because the parts 106 a,b are wider at a point that will be further embedded into the canopy 100 after the molding process, the canopy material that surrounds the parts 106 a,b holds the parts 106 a,b securely in place.
  • FIGS. 6 and 7 illustrate a non-limiting example of mechanisms for securing the handle 104 to a canopy rail 130 .
  • the canopy rail 130 includes a canopy receiving channel 132 that is formed by an interior wall 136 , a base 138 , and an exterior wall 134 .
  • the handle 104 passes through an opening 142 within the base 138 of the channel 132 .
  • the opening 142 suitably includes a cap 144 that is spring-loaded to be forced open by the handle 104 when the handle 104 passes through the opening 142 .
  • the cap 144 is suitably spring-hinged to the interior wall 136 underneath the base 138 .
  • the cap 144 keeps water and other particulates from entering an interior of the canopy rail 130 when the canopy 100 is in an open position.
  • the canopy rail 130 includes a handle-receiving hook 148 that rotates into position to grip the handle 104 once the handle 104 has fully penetrated the opening 142 .
  • the hook 148 is suitably operated by conventional electromechanical devices and is activated when a switch (not shown) indicates that the canopy 100 is in proper position within the canopy channel 132 .
  • the switch can be included within the cap 144 .
  • the hook 148 keeps the handle 104 within the rail 130 thereby securing the canopy 100 to the canopy rail 130 .
  • the exterior wall 134 of the canopy rail 130 includes an inflatable seal 150 along a wall of the channel 132 .
  • the seal 150 inflates by a pneumatic or hydraulic system (not shown) that is included within the vehicle once the canopy 100 is fully seated within the channel 132 .
  • the seal 150 provides a moisture and air pressure lock between the environment within the cockpit and outside of the cockpit.
  • FIG. 8 illustrates that the hooks 104 can be used to aide a pilot during ingress and egress from a cockpit 160 of an aircraft 170 .
  • FIGS. 9 - 11 illustrate perspective x-ray views of a third embodiment of the present invention.
  • An attachment device 200 is embedded within an injection-molded canopy 202 .
  • the attachment device 200 includes a shaft 204 with two knob ends 206 and 208 .
  • the attachment device 200 is inserted near the base of the canopy 202 .
  • the canopy 202 is molded so that the knob ends 206 and 208 are at least partially embedded within the canopy 202 and the shaft 204 has its longitudinal axis substantially perpendicular to a lengthwise axis of a cavity 210 .
  • the shaft 204 is approximately centered within the cavity 210 .
  • the cavity 210 is exposed at the base of the canopy 202 .
  • a canopy rail 220 includes a hook device 224 .
  • the hook device 224 is received by the cavity 210 . Then, either the canopy 202 , the hook device 224 , or the canopy rail 220 with the attached hook device 224 are slid so that the shaft 204 is received by the hook device 224 , thus locking the canopy 202 to the rail 220 .

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Mechanical Engineering (AREA)
  • Transportation (AREA)
  • Injection Moulding Of Plastics Or The Like (AREA)
  • Body Structure For Vehicles (AREA)

Abstract

An apparatus and method for latching a canopy to a vehicle, such as an aircraft, that avoids plastic creep and crazing due to concentrated loads is provided. The apparatus includes first attachment components that are at least partially embedded within an injection-molded canopy and second attachment components that are connected to the canopy rail for attaching to the one or more first attachment components and thereby attaching the canopy to the canopy rail.

Description

    RELATED APPLICATIONS
  • This invention relates to copending U.S. patent application Ser. No. `______, Attorney docket no. BOEI-1-1132, filed Feb. 13, 2002, U.S. patent application Ser. No. ______, Attorney docket no. BOEI-1-1133, filed Feb. 13, 2002, U.S. patent application Ser No. ______, Attorney docket no. BOEI-1-1138, filed Feb. 13, 2002, U.S. patent application Ser. No. ______, Attorney docket no. BOEI-1-1139, filed Feb. 13, 2002, and U.S. patent application Ser. No. ______, Attorney docket no. BOEI-1-1142, filed Feb. 13, 2002, all of which are hereby incorporated by reference.[0001]
  • GOVERNMENT LICENSE RIGHTS
  • [0002] This invention was made with Government support under U.S. Government contract F33615-97-2-3407 awarded by the U.S. Air Force. The Government has certain rights in this invention.
  • FIELD OF THE INVENTION
  • This invention relates generally to vehicles with canopies and, more specifically, to closing mechanisms for injection-molded canopies. [0003]
  • BACKGROUND OF THE INVENTION
  • Modern aircraft canopies contain many parts. A transparent portion of the canopy may be replaced several times during the life of an aircraft due to scratches and general deterioration. Replacement of the transparent portion entails frame disassembly and reassembly. This is time-consuming, labor intensive, and costly. [0004]
  • Attempts have been made to produce frameless aircraft canopies in order to simplify replacement of the transparent portion, among other reasons. However, a frame provides structural stiffness and strong, secure, attachment points for hinges and latches. As is known, the viable frameless canopy system must include a method for latching. Prior latching methods include a male hook or pin located on the aircraft structure or canopy frame and a female receiver on the canopy frame structure or aircraft structure respectively. Such discrete latching methods produce concentrated loads, which cause bearing stress in the transparency in the region of the latch. [0005]
  • Stress causes problems for transparencies. Glassy polymers craze at low stress levels. The effect of crazing on crack growth and localized failure is not well understood. Polymer transparencies yield at low stress levels and creep occurs after a fraction of service life. Cyclic, long-term loading, such as cockpit pressurization, induces creep and/or craze and reduces service life. Elevated temperatures, such as those experienced by high-speed aircraft, further increase the rate of creep and amplify the effect of crazing. [0006]
  • Therefore, there exists an unmet need to produce a latching system for an injection-molded canopy which avoids plastic creep or crazing due to concentrated loads yet securely holds the canopy in place. [0007]
  • SUMMARY OF THE INVENTION
  • The present invention provides an apparatus and method for latching a canopy to a vehicle, such as an aircraft, that avoids plastic creep or crazing due to concentrated loads. The apparatus includes first attachment components that are at least partially embedded within an injection-molded canopy and second attachment components that are connected to the canopy rail for attaching to the one or more first attachment components and thereby attaching the canopy to the canopy rail. [0008]
  • In another aspect of the invention, the first component includes a shaft with two ends and one or more knobs attached to the ends of the shaft. The knobs are molded into the canopy, and the shaft is exposed within a cavity formed by the canopy. The cavity is opened at a base of the canopy. [0009]
  • In still another aspect of the invention, the first component includes a hook at least partially embedded within the canopy. A portion of the hook protrudes from a base edge of the canopy.[0010]
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • The preferred and alternative embodiments of the present invention are described in detail below with reference to the following drawings. [0011]
  • FIG. 1 illustrates an injection-molded frameless canopy attached to a vehicle in accordance with the present invention; [0012]
  • FIGS. 2 and 3 illustrate x-ray perspective views of a first embodiment for attaching the canopy to the vehicle; [0013]
  • FIG. 4 illustrates a perspective view of a canopy that includes an attachment mechanism in accordance with the second embodiment of the present invention; [0014]
  • FIG. 5 illustrates an exploded perspective view of the handrail attachment mechanism shown in FIG. 4; [0015]
  • FIG. 6 illustrates a cutaway side view of the canopy of FIG. 4 attached to a canopy rail; [0016]
  • FIG. 7 illustrates a cutaway perspective view of the system shown in FIG. 6; [0017]
  • FIG. 8 illustrates a perspective view of an aircraft that includes the canopy shown in FIG. 4; and [0018]
  • FIGS. [0019] 9-11 illustrate cutaway perspective views of a canopy that includes an attachment mechanism in accordance with a third embodiment of the present invention.
  • DETAILED DESCRIPTION OF THE INVENTION
  • The present invention is an injection-molded canopy with canopy attachment devices that are inserted into the canopy during an injection molding process. As shown in FIG. 1, an [0020] exemplary canopy 20 attaches to a canopy rail 24 that surrounds a cockpit 26 of a vehicle 28, such as an aircraft.
  • FIGS. 2 and 3 illustrate a first embodiment of an attachment device that is molded into an injection-molded [0021] canopy 30. The attachment device is suitably a hook 32. The hook 32 is substantially U-shaped. A first section 34 of the hook 32 expands in length away from a centerline of the hook 30. A first section 34 is embedded within the canopy 30 during the injection molding process. A second section 42 of the hook 32 is exposed below the canopy 30. The second section 42 includes a claw 44 and a U-shaped indent caused by the claw 44 and the first section 34. When the injection-molded canopy 30 is fully formed around the first section 34, the material of the canopy 30 holds the hook 32 in place by putting pressure on the expanded edges of the first section 34.
  • A [0022] canopy rail 50 includes a canopy-receiving channel 52 that receives the canopy 30 and the mounted hook 32. The canopy rail 50 is attached around a cockpit in a conventional manner. One of the walls of the channel 52 suitably includes an inflatable seal 58 that is attached to a pneumatic or hydraulic system (not shown) that is included within the vehicle. The inflatable seal 58 inflates when the canopy 30 is inserted into the channel 52 and locked in place in the canopy rail 50. The inflatable seal 58 provides a moisture and air pressure seal between the vehicle cockpit and the environment outside of the cockpit.
  • In one embodiment, the [0023] canopy 30 is first inserted into the rail 50. The canopy 30 is moved by a support structure (not shown), thereby making contact between the U-shaped cutout of the hook 32 and a locking mechanism (not shown) that is included as part of the canopy rail 50. Co-pending patent application Ser. No. ______, Attorney Docket No. BOEI-1-1142, hereby incorporated by reference, illustrates a mechanism for receiving the hook 32 without requiring fore and aft motion of the canopy 30 when the canopy 30 is inserted into the channel 52.
  • FIG. 4 illustrates a perspective view of a second embodiment of an attachment device that is embedded within a [0024] canopy 100 during an injection molding process. In this embodiment, the attachment mechanisms are imbedded handle devices 102. As shown in FIG. 5, the imbedded handle devices 102 include a U-shaped handle 104 and two pair of handle end holders 106. Each pair of the handle end holders 106 includes a first part 106 a and a second part 106 b. Each of the parts 106 a,b includes a cavity that forms a cavity 110 that receives an end of the handle 104 when the parts 106 a,b are combined. The parts 106 a,b are attached to each other by a fastener 112, such as without limitation a screw or a bolt, that is received through the first part 106 a and is securely mounted into the second part 106 b. One or more securing pins 116 are received by respective pinholes in the first part 106 a and are received into receiving cavities (not shown) within the second part 106 b. The pins 116 help reduce any rotational movement between the first and second parts 106 a,b. It can be appreciated that other fastener mechanisms, such as without limitation an adhesive, may be used for attaching the parts 106 a,b. Each end of the handle 104 includes a top section 120 that is wider from a centerline point than a bottom section 122. The cavities 110 include chambers sized to receive each of the top and bottom sections 120 and 122. Thus, when each parts 106 a,b are coupled to each other with the ends of the handle 104 inserted within the cavities 110, the handle 104 is held securely by the pairs of handle end holders 106.
  • The [0025] end holders 106 are then inserted in a mold for the injection-molded canopy 100 such that when the molding of the canopy 100 is complete, the pairs of end holders 106 are surrounded by the molded canopy 100 and only the handles 104 protrude out of the base of the canopy 100. In this embodiment the parts 106 a,b; are trapezoidal in shape with a first length at the side that includes the cavity 110 that is smaller than a second length of the side that is opposite the side that includes the cavity 110. Therefore, because the parts 106 a,b are wider at a point that will be further embedded into the canopy 100 after the molding process, the canopy material that surrounds the parts 106 a,b holds the parts 106 a,b securely in place.
  • FIGS. 6 and 7 illustrate a non-limiting example of mechanisms for securing the [0026] handle 104 to a canopy rail 130. The canopy rail 130 includes a canopy receiving channel 132 that is formed by an interior wall 136, a base 138, and an exterior wall 134. When the canopy 100 is received within the canopy channel 132, the handle 104 passes through an opening 142 within the base 138 of the channel 132. The opening 142 suitably includes a cap 144 that is spring-loaded to be forced open by the handle 104 when the handle 104 passes through the opening 142. The cap 144 is suitably spring-hinged to the interior wall 136 underneath the base 138. The cap 144 keeps water and other particulates from entering an interior of the canopy rail 130 when the canopy 100 is in an open position. The canopy rail 130 includes a handle-receiving hook 148 that rotates into position to grip the handle 104 once the handle 104 has fully penetrated the opening 142. The hook 148 is suitably operated by conventional electromechanical devices and is activated when a switch (not shown) indicates that the canopy 100 is in proper position within the canopy channel 132. The switch can be included within the cap 144. The hook 148 keeps the handle 104 within the rail 130 thereby securing the canopy 100 to the canopy rail 130.
  • In one embodiment, the [0027] exterior wall 134 of the canopy rail 130 includes an inflatable seal 150 along a wall of the channel 132. The seal 150 inflates by a pneumatic or hydraulic system (not shown) that is included within the vehicle once the canopy 100 is fully seated within the channel 132. The seal 150 provides a moisture and air pressure lock between the environment within the cockpit and outside of the cockpit.
  • FIG. 8 illustrates that the [0028] hooks 104 can be used to aide a pilot during ingress and egress from a cockpit 160 of an aircraft 170.
  • FIGS. [0029] 9-11 illustrate perspective x-ray views of a third embodiment of the present invention. An attachment device 200 is embedded within an injection-molded canopy 202. The attachment device 200 includes a shaft 204 with two knob ends 206 and 208. During the injection-molding process of the canopy 202 the attachment device 200 is inserted near the base of the canopy 202. The canopy 202 is molded so that the knob ends 206 and 208 are at least partially embedded within the canopy 202 and the shaft 204 has its longitudinal axis substantially perpendicular to a lengthwise axis of a cavity 210. The shaft 204 is approximately centered within the cavity 210. The cavity 210 is exposed at the base of the canopy 202.
  • Referring to FIGS. 9 and 10, a [0030] canopy rail 220 includes a hook device 224. When the canopy 202 is closed onto the canopy rail 220, the hook device 224 is received by the cavity 210. Then, either the canopy 202, the hook device 224, or the canopy rail 220 with the attached hook device 224 are slid so that the shaft 204 is received by the hook device 224, thus locking the canopy 202 to the rail 220.
  • It can be appreciated that various other types of attachment mechanisms can be imbedded within an injection-molded canopy during canopy creation. [0031]
  • While the preferred embodiment of the invention has been illustrated and described, as noted above, many changes can be made without departing from the spirit and scope of the invention. Accordingly, the scope of the invention is not limited by the disclosure of the preferred embodiment. Instead, the invention should be determined entirely by reference to the claims that follow. [0032]

Claims (31)

What is claimed is:
1. An apparatus for attaching a canopy to a canopy rail, the apparatus comprising:
one or more first attachment components being at least partially embedded within an injection-molded canopy; and
one or more second attachment components being connected to the canopy rail for attaching to the one or more first attachment components and thereby attaching the canopy to the canopy rail.
2. The apparatus of claim 1, wherein at least one of the first attachment components includes:
at least one pair of base supports; and
a handle with one or more ends,
wherein the at least one pair of base supports are supported by the injection-molded canopy, and the combined base supports form a cavity that receives one end of the handle.
3. The apparatus of claim 2, further comprising a canopy rail that surrounds a cockpit of a vehicle, wherein the canopy rail includes a device for attaching to the handle when the canopy is positioned in a closed position with respect to the canopy rail.
4. The apparatus of claim 3, wherein the device includes an arm that rotates about a pivot point within the canopy rail.
5. The apparatus of claim 3, wherein the canopy rail includes a door for receiving the handle.
6. The apparatus of claim 5, wherein the door is biased to close when the canopy is an open position.
7. The apparatus of claim 1, wherein at least one of the first attachment components includes:
a shaft with two ends; and
one or more knobs attached to the ends of the shaft,
wherein the knobs are at least partially embedded into the canopy, the shaft is exposed within a cavity formed by the canopy, and the cavity is opened at a base of the canopy.
8. The apparatus of claim 7, further comprising a canopy rail including one or more hooks, wherein the canopy is positioned so that the hooks insert into the cavity, and wherein at least one of the canopy or the canopy rail being slid such that the hooks receive the shaft that is within the cavity.
9. The apparatus of claim 1, wherein at least one of the first attachment components includes a hook at least partially embedded within the canopy, wherein a portion of the hook protrudes from a base of the canopy.
10. The apparatus of claim 9, further comprising a canopy rail including one or more devices for receiving the hook.
11. A method for attaching a canopy to a canopy rail, the method comprising:
at least partially embedding a first component within the canopy; and
attaching the first component to a second component,
wherein the canopy rail includes the second component.
12. The method of claim 11, wherein the canopy includes an injection-molded canopy.
13. The method of claim 11, wherein at least partially embedding includes:
inserting an end of a handle between a pair of base supports;
attaching the pair of base supports to each other; and
embedding the pair of base supports within the canopy.
14. The method of claim 13, further comprising attaching the handle to a device within the canopy rail when the canopy is positioned in a closed position with respect to the canopy rail.
15. The method of claim 14, wherein the device includes an arm that rotates about a pivot point within the canopy rail.
16. The method of claim 14, wherein the canopy rail includes a door for receiving the handle.
17. The method of claim 16, wherein the door is biased to close when the canopy is an open position.
18. The method of claim 11, wherein at least one of the first components includes a shaft with two ends and one or more knobs attached to the ends of the shaft, and wherein at least partially embedding includes molding the knobs into the canopy with a cavity that includes the shaft.
19. The method of claim 18, wherein the canopy rail includes one or more hooks, the method further comprising:
inserting the one or more hooks into the cavity; and
sliding at least one of the canopy or the canopy rail in order for the hooks to receive the shaft that is within the cavity.
20. The method of claim 11, wherein at least partially embedding includes:
at least partially embedding a hook within the canopy,
wherein a portion of the hook protrudes from a base of the canopy.
21. The method of claim 20, wherein the canopy rail includes one or more devices for receiving the hook.
22. A canopy locking system comprising:
an injection-molded canopy including one or more first attachment components being at least partially embedded within an injection-molded canopy; and
a canopy rail including one or more second attachment components for attaching to the one or more first attachment components and thereby attaching the canopy to the canopy rail.
23. The system of claim 22, wherein at least one of the first attachment components includes:
at least one pair of base supports; and
a handle with one or more ends,
wherein the at least one pair of base supports are supported by the injection-molded canopy, and the combined base supports form a cavity that receives one end of the handle.
24. The system of claim 23, wherein the one or more second attachment components includes a device for attaching to the handle when the canopy is positioned in a closed position with respect to the canopy rail.
25. The system of claim 24, wherein the device includes an arm that rotates about a pivot point within the canopy rail.
26. The system of claim 24, wherein the canopy rail includes a door for receiving the handle.
27. The system of claim 26, wherein the door is biased to close when the canopy is an open position.
28. The system of claim 22, wherein at least one of the first attachment components includes:
a shaft with two ends; and
one or more knobs attached to the ends of the shaft,
wherein the knobs are at least partially embedded into the canopy, the shaft is exposed within a cavity formed by the canopy, and the cavity is opened at a base of the canopy.
29. The system of claim 28, wherein the canopy is positioned such that the hooks insert into the cavity, and wherein at least one of the canopy or the canopy rail being slid such that the hooks receive the shaft that is within the cavity.
30. The system of claim 22, wherein at least one of the first attachment components includes a hook at least partially embedded within the canopy, wherein a portion of the hook protrudes from a base of the canopy.
31. The system of claim 30, wherein the second attachment components include one or more devices for receiving the hook.
US10/367,064 2003-02-13 2003-02-13 Attachment apparatus for injection-molded frameless canopies Abandoned US20040159745A1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
US10/367,064 US20040159745A1 (en) 2003-02-13 2003-02-13 Attachment apparatus for injection-molded frameless canopies
PCT/US2004/003476 WO2005035359A2 (en) 2003-02-13 2004-02-06 Attachement apparatus for injection-molded frameless canopies
US10/960,144 US7040577B2 (en) 2003-02-13 2004-10-07 Attachment apparatus for injection-molded frameless canopies

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/367,064 US20040159745A1 (en) 2003-02-13 2003-02-13 Attachment apparatus for injection-molded frameless canopies

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US10/960,144 Continuation US7040577B2 (en) 2003-02-13 2004-10-07 Attachment apparatus for injection-molded frameless canopies

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US20040159745A1 true US20040159745A1 (en) 2004-08-19

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US10/367,064 Abandoned US20040159745A1 (en) 2003-02-13 2003-02-13 Attachment apparatus for injection-molded frameless canopies
US10/960,144 Expired - Lifetime US7040577B2 (en) 2003-02-13 2004-10-07 Attachment apparatus for injection-molded frameless canopies

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US20050247823A1 (en) * 2004-05-04 2005-11-10 Wood Jeffrey H Injection-molded polycarbonate door
US10589448B2 (en) 2013-09-30 2020-03-17 Mitsubishi Heavy Industries, Ltd. Injection molding method and injection molding device for transparent resin molded article
CN111661365A (en) * 2020-06-12 2020-09-15 南京航空航天大学 Constant-section pipe parallel jet type canopy heating loading test bed

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CN107487434B (en) * 2017-08-01 2020-05-15 中国航空工业集团公司西安飞机设计研究所 A fixed wing aircraft cockpit
WO2024155261A1 (en) * 2023-01-18 2024-07-25 Tusas- Turk Havacilik Ve Uzay Sanayii Anonim Sirketi A canopy mechanism

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US4964594A (en) * 1988-04-11 1990-10-23 Texstar, Inc. Blind fastener having special utility in the installation of transparencies in aircraft and the like
US5277384A (en) * 1991-11-04 1994-01-11 Texstar, Inc. Transparency quick seal system

Cited By (4)

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Publication number Priority date Publication date Assignee Title
US20050247823A1 (en) * 2004-05-04 2005-11-10 Wood Jeffrey H Injection-molded polycarbonate door
US10589448B2 (en) 2013-09-30 2020-03-17 Mitsubishi Heavy Industries, Ltd. Injection molding method and injection molding device for transparent resin molded article
US10759098B2 (en) 2013-09-30 2020-09-01 Mitsubishi Heavy Industries, Ltd. Injection molding method and injection molding device for transparent resin molded article
CN111661365A (en) * 2020-06-12 2020-09-15 南京航空航天大学 Constant-section pipe parallel jet type canopy heating loading test bed

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WO2005035359A3 (en) 2005-08-04
US7040577B2 (en) 2006-05-09
WO2005035359A2 (en) 2005-04-21
US20060054743A1 (en) 2006-03-16

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