CN210565726U - Quick-release hinge structure - Google Patents

Quick-release hinge structure Download PDF

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Publication number
CN210565726U
CN210565726U CN201921350258.9U CN201921350258U CN210565726U CN 210565726 U CN210565726 U CN 210565726U CN 201921350258 U CN201921350258 U CN 201921350258U CN 210565726 U CN210565726 U CN 210565726U
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China
Prior art keywords
buckle
hole
rotating shaft
arm
spring
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CN201921350258.9U
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Chinese (zh)
Inventor
于洪权
王佳兴
李世凯
王文鑫
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Beijing Andawell Aviation Equipment Co Ltd
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Beijing Andawell Aviation Equipment Co Ltd
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Priority to CN201921350258.9U priority Critical patent/CN210565726U/en
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Abstract

The utility model provides a quick-release hinge structure, which is characterized in that the structure comprises a base, a buckle unit and a hinge arm unit; the buckle unit comprises a buckle base body, a buckle ejector rod, a buckle spring and a buckle fixing rod; the hinge arm unit comprises a main hinge arm, an auxiliary hinge arm, a first rotating shaft, a second rotating shaft, a third rotating shaft, a left support arm spring and a right support arm spring. The utility model provides a quick-release hinge structure has following advantage: (1) the utility model discloses a quick-release hinge structure can realize the fast-assembling quick-release according to installation, dismantlement needs, has strengthened work efficiency greatly, has promoted the propulsion of job schedule. (2) The shock absorption device has a certain shock absorption effect, and is suitable for being applied to connection between equipment on the machine, which has certain requirements on shock absorption.

Description

Quick-release hinge structure
Technical Field
The utility model belongs to the technical field of mechanical structure, concretely relates to quick-release hinge structure.
Background
No matter the structure or the interior trim of the airplane is assembled by a plurality of parts, and a plurality of connection modes are hinge connection modes in the installation process, so that the two parts can rotate relatively. For example, a mounting frame for rotatably mounting onboard equipment such as oxygen equipment is generally required on an aircraft cabin frame, so as to realize the rotating action of the mounting frame for the onboard equipment relative to the aircraft cabin frame.
In the prior art, the conventional hinge structure is used in the following manner: two devices that need to be connected in rotation are respectively called a first device and a second device, and then: the fixed seat of the hinge structure is connected with the first equipment through a bolt, and the movable seat of the hinge structure is connected with the second equipment through a bolt, so that the hinge connection of the first equipment and the second equipment is realized. This connection mainly has the following problems: because first equipment and second equipment all need realize through bolted connection mode with hinge structure's assembly, consequently, installation and dismantlement process are loaded down with trivial details, can't realize quick installation and the dismantlement between first equipment and the second equipment.
SUMMERY OF THE UTILITY MODEL
To the defect that prior art exists, the utility model provides a quick-release hinge structure can effectively solve above-mentioned problem.
The utility model adopts the technical scheme as follows:
the utility model provides a quick-release hinge structure, which comprises a base 100, a buckle unit 200 and a hinge arm unit 300;
the buckle unit 200 comprises a buckle seat body 201, a buckle ejector rod 202, a buckle spring 203 and a buckle fixing rod 204;
the base 100 is provided with a clamping groove 101 along the X direction; the central part of the clamping groove 101 forms a placing space of the buckle base body 201; the base 100 is provided with a trapezoidal through hole 102 along the Y direction; one end of the trapezoidal through hole 102 is a large-diameter hole 1021, the other end of the trapezoidal through hole is a small-diameter hole 1022, and the small-diameter hole 1022 is communicated with the clamping groove 101; the buckle spring 203 is placed in the large-diameter hole 1021, one end of the buckle ejector rod 202 is located outside the large-diameter hole 1021, and the other end of the buckle ejector rod 202 passes through the buckle spring 203, then passes through the small-diameter hole 1022, and finally is fixed to the surface of the buckle base 201; the surface of the buckle seat body 201 is also fixedly provided with the buckle fixing rod 204, and the buckle fixing rod 204 is arranged in parallel with the buckle ejector rod 202;
the hinge arm unit 300 includes a main hinge arm 301, a sub hinge arm 302, a first rotating shaft 303, a second rotating shaft 304, a third rotating shaft 305, a left arm spring 306, and a right arm spring 307;
the auxiliary hinged arm 302 is provided with a bolt assembling hole 308 for fixing with first equipment; the auxiliary hinge arm 302 is rotatably connected with the main hinge arm 301 through the first rotating shaft 303; the main hinge arm 301 is provided with a left support arm 301A and a right support arm 301B which are symmetrical; a second rotating shaft assembling hole 304A matched with the second rotating shaft 304 is formed in the front side of the left support arm 301A and the right support arm 301B, a third rotating shaft through hole 305A is formed in the rear side of the left support arm 301A and the right support arm 301B, and the aperture of the third rotating shaft through hole 305A is larger than the shaft diameter of the third rotating shaft 305;
the two sides of the base 100 are respectively provided with a left vertical hole 103 and a right vertical hole 104; the left arm spring 306 is placed in the left vertical hole 103, and the right arm spring 307 is placed in the right vertical hole 104; after the second rotating shaft 304 passes through the second rotating shaft assembling hole 304A, both ends of the second rotating shaft 304 are assembled to the base 100, so that the main hinge arm 301 is rotatably connected with the base 100; after the third rotating shaft 305 passes through the third rotating shaft through hole 305A, both ends are assembled to the base 100;
the end of the left arm 301A presses into the left arm spring 306 of the left vertical hole 103, and the end of the right arm 301B presses into the right arm spring 307 of the right vertical hole 104.
Preferably, the third shaft through hole 305A is an elliptical through hole.
The utility model provides a quick-release hinge structure has following advantage:
1 the utility model discloses a quick-release hinge structure can realize the fast-assembling quick-release according to installation, dismantlement needs, has strengthened work efficiency greatly, has promoted the propulsion of job schedule.
2 has certain shock attenuation effect, is fit for being applied to the connection between the equipment that has certain requirement to the shock attenuation on the machine equipment.
Drawings
FIG. 1 is a perspective view of a quick release hinge construction;
FIG. 2 is a cross-sectional view of a quick release hinge structure;
FIG. 3 is another cross-sectional view of the quick release hinge structure;
FIG. 4 is a perspective view of the buckle unit;
FIG. 5 is a perspective view of the base;
FIG. 6 is a view showing the fitting relationship between the base and the latch unit;
fig. 7 is a perspective view of the hinge arm unit.
Detailed Description
In order to make the technical problem, technical solution and advantageous effects solved by the present invention more clearly understood, the following description is given in conjunction with the accompanying drawings and embodiments to further explain the present invention in detail. It should be understood that the specific embodiments described herein are for purposes of illustration only and are not intended to limit the invention.
The utility model provides a quick-release hinge structure can realize the fast-assembling quick-release according to installation, dismantlement needs, has strengthened work efficiency greatly, has promoted the propulsion of job schedule.
Referring to fig. 1, the quick release hinge structure includes a base 100, a buckle unit 200, and a hinge arm unit 300.
Two pieces of equipment which need to realize rotary connection are respectively called as first equipment and second equipment, and the first equipment is assumed to be an aircraft cabin framework; the second equipment is an installation frame for installing on-board equipment such as oxygen equipment, and a fixing plate is fixed on the aircraft cabin framework and provided with a through hole. Then, the fixing plate is clamped and fixed by the fastening unit 200 and the base 100 in an assembling manner through the matching of the base 100 and the fastening unit 200, and the hinge arm unit 300 is connected and fixed with the mounting frame through the bolt assembling holes 308 on the hinge arm unit 300. Therefore, the hinge connection between the aircraft cabin framework and the installation frame is realized, and therefore, the quick-release hinge structure provided by the application is only fixedly connected with the installation frame through bolts and fixedly connected with the aircraft cabin framework in a clamping connection mode, so that the installation and the disassembly are simple.
The buckle unit 200 and the hinge arm unit 300 will be described in detail below, respectively:
a fastening unit 200
The buckle unit 200 comprises a buckle seat body 201, a buckle ejector rod 202, a buckle spring 203 and a buckle fixing rod 204;
referring to fig. 5, the base 100 is provided with a card slot 101 along the X direction; referring to fig. 6, a central portion of the card slot 101 forms a placement space of the card seat 201; referring to fig. 2, the base 100 is provided with a trapezoidal through hole 102 along the Y direction; one end of the trapezoidal through hole 102 is a large-diameter hole 1021, the other end of the trapezoidal through hole is a small-diameter hole 1022, and the small-diameter hole 1022 is communicated with the clamping groove 101; the buckle spring 203 is placed in the large-diameter hole 1021, one end of the buckle ejector rod 202 is located outside the large-diameter hole 1021, and the other end of the buckle ejector rod 202 penetrates through the small-diameter hole 1022 after penetrating through the buckle spring 203 and is finally fixed on the surface of the buckle seat body 201; the surface of the buckle seat body 201 is also fixedly provided with a buckle fixing rod 204, and the buckle fixing rod 204 is arranged in parallel with the buckle top rod 202.
The principle of use of the snap unit 200 is:
when the assembly of fixed plate and quick-release hinge structure on the aircraft cabin skeleton needs to be realized, the use mode is: when no external force is applied to the snap ejector 202, the snap seat 201 is located in the middle of the snap groove 101 under the action of the snap spring 203, so as to snap the snap groove 101, which is the state shown in fig. 6.
Then, in the state of fig. 6, the buckle rod 202 is pushed leftward, the buckle rod 202 overcomes the acting force of the buckle spring 203 to compress the buckle spring 203, so as to move the buckle base 201 leftward, and further move the buckle base 201 away from the slot 101, and meanwhile, when the buckle base 201 moves leftward, the buckle rod 204 fixed on the buckle base 201 is also driven to move leftward, and further the buckle rod 204 is moved away from the slot 101.
At the moment, the quick-release hinge structure is moved, the fixing plate on the aircraft cabin framework is inserted into the clamping groove 101, and at the moment, the through hole formed in the fixing plate has the same height as the buckle fixing rod 204; then, the leftward pushing force on the snap rod 202 is released, and under the action of the snap spring 203, on the one hand, the snap fixing rod 204 moves rightward and is inserted into the through hole formed in the fixing plate, so as to limit and fix the fixing plate. On the other hand, the buckle base 201 moves rightwards, so that the fixing plate is clamped, and the clamping effect on the fixing plate is realized. Therefore, the quick-release hinge structure and the fixing plate are connected and fixed.
When the quick-release hinge structure needs to be disassembled, the buckle base body 201 is separated from the clamping groove 101 only by pushing the buckle ejector rod 202 leftwards, and meanwhile, the buckle fixing rod 204 is separated from the through hole formed in the fixing plate, so that the quick-release hinge structure can be taken down. Therefore, the quick-release hinge structure has the advantages of convenience and quickness in mounting and dismounting.
Two-hinged-arm unit 300
The hinge arm unit 300 includes a main hinge arm 301, a sub hinge arm 302, a first rotating shaft 303, a second rotating shaft 304, a third rotating shaft 305, a left arm spring 306, and a right arm spring 307;
referring to fig. 7, the auxiliary hinge arm 302 is provided with a bolt assembly hole 308 for fixing with a first device, so as to realize connection and fixation with a frame; the auxiliary hinge arm 302 is rotatably connected with the main hinge arm 301 through a first rotating shaft 303; the main hinge arm 301 has a left arm 301A and a right arm 301B that are symmetrical; a second rotating shaft assembly hole 304A matched with the second rotating shaft 304 is formed in the front side of the left support arm 301A and the right support arm 301B, a third rotating shaft through hole 305A is formed in the rear side of the left support arm 301A and the right support arm 301B, and the aperture of the third rotating shaft through hole 305A is larger than the shaft diameter of the third rotating shaft 305; for example, the third shaft through hole 305A is an elliptical through hole.
Referring to fig. 6, a left vertical hole 103 and a right vertical hole 104 are respectively formed at both sides of the base 100; a left arm spring 306 is arranged in the left vertical hole 103, and a right arm spring 307 is arranged in the right vertical hole 104; after the second rotating shaft 304 passes through the second rotating shaft assembling hole 304A, both ends are assembled to the base 100, so that the rotatable connection of the main hinged arm 301 and the base 100 is realized; after the third rotating shaft 305 passes through the third rotating shaft through hole 305A, both ends are assembled to the base 100; here, the second rotating shaft 304 mainly realizes the rotational connection of the main hinge arm 301 and the base 100. The third shaft through hole 305A is designed to be larger than the shaft diameter of the third shaft 305, for the purpose of: since the main hinge arm 301 has a movement margin with respect to the third rotation shaft 305, the device can achieve a shock-absorbing effect.
The end of the left arm 301A presses into the left arm spring 306 of the left vertical hole 103, and the end of the right arm 301B presses into the right arm spring 307 of the right vertical hole 104.
The left arm spring 306 and the right arm spring 307 are set to function as: first, the hinge arm unit 300 is opened by the elastic force of the left arm spring 306 and the right arm spring 307 without being applied with an external force. When the closing is needed, the hinge arm unit 300 is rotated to rotate around the second rotating shaft 304, and during the rotation of the hinge arm unit 300, the ends of the left arm 301A and the right arm 301B of the main hinge arm 301 respectively press down the left arm spring 306 and the right arm spring 307, so as to overcome the elastic forces of the left arm spring 306 and the right arm spring 307, and realize the closing action of the hinge arm unit 300. Secondly, the left support arm spring 306 and the right support arm spring 307 are arranged, so that the whole hinge structure has a certain damping effect and is suitable for being applied to connection between equipment on the machine, which has certain requirements on damping.
The utility model provides a quick-release hinge structure has following advantage:
1 the utility model discloses a quick-release hinge structure can realize the fast-assembling quick-release according to installation, dismantlement needs, has strengthened work efficiency greatly, has promoted the propulsion of job schedule.
2 has certain shock attenuation effect, is fit for being applied to the connection between the equipment that has certain requirement to the shock attenuation on the machine equipment.
The foregoing is only a preferred embodiment of the present invention, and it should be noted that, for those skilled in the art, a plurality of improvements and decorations can be made without departing from the principle of the present invention, and these improvements and decorations should also be viewed as the protection scope of the present invention.

Claims (2)

1. A quick-release hinge structure is characterized by comprising a base (100), a buckle unit (200) and a hinge arm unit (300);
the buckle unit (200) comprises a buckle base body (201), a buckle ejector rod (202), a buckle spring (203) and a buckle fixing rod (204);
the base (100) is provided with a clamping groove (101) along the X direction; the central part of the clamping groove (101) forms a placing space of the buckle base body (201); the base (100) is provided with a trapezoidal through hole (102) along the Y direction; one end of the trapezoidal through hole (102) is a large-diameter hole (1021), the other end of the trapezoidal through hole is a small-diameter hole (1022), and the small-diameter hole (1022) is communicated with the clamping groove (101); placing the buckle spring (203) in the large-diameter hole (1021), wherein one end of the buckle ejector rod (202) is positioned outside the large-diameter hole (1021), and the other end of the buckle ejector rod (202) passes through the small-diameter hole (1022) after passing through the buckle spring (203), and is finally fixed to the surface of the buckle seat body (201); the surface of the buckle seat body (201) is also fixedly provided with the buckle fixing rod (204), and the buckle fixing rod (204) is arranged in parallel with the buckle ejector rod (202);
the hinge arm unit (300) comprises a main hinge arm (301), an auxiliary hinge arm (302), a first rotating shaft (303), a second rotating shaft (304), a third rotating shaft (305), a left arm spring (306) and a right arm spring (307);
the auxiliary hinged arm (302) is provided with a bolt assembling hole (308) for fixing with first equipment; the auxiliary hinge arm (302) is rotatably connected with the main hinge arm (301) through the first rotating shaft (303); the main hinged arm (301) is provided with a left support arm (301A) and a right support arm (301B) which are symmetrical; a second rotating shaft assembling hole (304A) matched with the second rotating shaft (304) is formed in the front side of the left support arm (301A) and the right support arm (301B), a third rotating shaft through hole (305A) is formed in the rear side of the left support arm (301A) and the right support arm (301B), and the aperture of the third rotating shaft through hole (305A) is larger than the shaft diameter of the third rotating shaft (305);
the two sides of the base (100) are respectively provided with a left vertical hole (103) and a right vertical hole (104); the left support arm spring (306) is placed in the left vertical hole (103), and the right support arm spring (307) is placed in the right vertical hole (104); after the second rotating shaft (304) passes through the second rotating shaft assembling hole (304A), two ends of the second rotating shaft are assembled to the base (100), so that the main hinged arm (301) can be rotatably connected with the base (100); after the third rotating shaft (305) passes through the third rotating shaft through hole (305A), two ends of the third rotating shaft are assembled to the base (100);
the end of the left arm (301A) presses into the left arm spring (306) of the left vertical hole (103), and the end of the right arm (301B) presses into the right arm spring (307) of the right vertical hole (104).
2. The quick release hinge structure according to claim 1, wherein the third rotation shaft through hole (305A) is an oval through hole.
CN201921350258.9U 2019-08-20 2019-08-20 Quick-release hinge structure Active CN210565726U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201921350258.9U CN210565726U (en) 2019-08-20 2019-08-20 Quick-release hinge structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201921350258.9U CN210565726U (en) 2019-08-20 2019-08-20 Quick-release hinge structure

Publications (1)

Publication Number Publication Date
CN210565726U true CN210565726U (en) 2020-05-19

Family

ID=70632065

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201921350258.9U Active CN210565726U (en) 2019-08-20 2019-08-20 Quick-release hinge structure

Country Status (1)

Country Link
CN (1) CN210565726U (en)

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