CN211688132U - Aircraft bonnet strutting arrangement for fork truck - Google Patents

Aircraft bonnet strutting arrangement for fork truck Download PDF

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Publication number
CN211688132U
CN211688132U CN202020101152.1U CN202020101152U CN211688132U CN 211688132 U CN211688132 U CN 211688132U CN 202020101152 U CN202020101152 U CN 202020101152U CN 211688132 U CN211688132 U CN 211688132U
Authority
CN
China
Prior art keywords
rack
aircraft bonnet
connecting rod
gear
uide bushing
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Fee Related
Application number
CN202020101152.1U
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Chinese (zh)
Inventor
贺为利
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.)
Hengyang Yili Machinery Manufacturing Co ltd
Original Assignee
Hengyang Yili Machinery Manufacturing Co ltd
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 Hengyang Yili Machinery Manufacturing Co ltd filed Critical Hengyang Yili Machinery Manufacturing Co ltd
Priority to CN202020101152.1U priority Critical patent/CN211688132U/en
Application granted granted Critical
Publication of CN211688132U publication Critical patent/CN211688132U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a aircraft bonnet strutting arrangement for fork truck, including seting up the recess on the fork truck frame, the recess internal fixation has the grudging post, the dead axle rotates on the grudging post and is connected with the gear, be fixed with connecting rod one on the gear, the one end dead axle that the gear was kept away from to connecting rod one rotates the one end of connecting rod two, the other end and the aircraft bonnet of connecting rod two are articulated, the inside uide bushing that is fixed with of recess, and the uide bushing is located the right side of grudging post, sliding connection has the rack in the uide bushing, wheel and rack toothing is connected, accessible latched device fixed connection between rack and the uide bushing, the rack passes through spring one with the right side. This kind of aircraft bonnet strutting arrangement for fork truck makes things convenient for opening of aircraft bonnet, labour saving and time saving need not the location, and at the in-process that the aircraft bonnet was closed, compression spring makes a spring one hold power to when opening the aircraft bonnet next time, play the helping hand effect to the aircraft bonnet, and play the cushioning effect when closing the aircraft bonnet.

Description

Aircraft bonnet strutting arrangement for fork truck
Technical Field
The utility model relates to a fork truck aircraft bonnet field specifically is an aircraft bonnet strutting arrangement for fork truck.
Background
Current fork truck aircraft bonnet need support it with a bracing piece after opening, need hold up the aircraft bonnet with one hand at the in-process that uses the bracing piece, and the bracing piece is scratched from the frame on the other hand to aim at the button hole on the free end of bracing piece and the aircraft bonnet and peg graft, thereby accomplish the opening to the aircraft bonnet, this kind of operation process is harder, and is time-consuming moreover, and is very inconvenient to opening of aircraft bonnet.
To solve the above problems, we propose a hood supporting device for a forklift.
SUMMERY OF THE UTILITY MODEL
The to-be-solved technical problem of the utility model is to overcome prior art's defect, provide a aircraft bonnet strutting arrangement for fork truck, in order to solve above-mentioned technical problem, the utility model provides a following technical scheme:
the utility model relates to a aircraft bonnet strutting arrangement for fork truck, including seting up the recess on the fork truck frame, the recess internal fixation has the grudging post, the dead axle rotates on the grudging post and is connected with the gear, be fixed with connecting rod one on the gear, the one end dead axle that the gear was kept away from to connecting rod one rotates the one end of connecting rod two, the other end and the aircraft bonnet of connecting rod two are articulated, the inside uide bushing that is fixed with of recess, and the uide bushing is located the right side of grudging post, sliding connection has the rack in the uide bushing, wheel and rack toothing are connected, accessible latched device fixed connection between rack and the uide bushing, the rack passes through spring one with the right side wall of recess and is connected.
Preferably, the locking mechanism comprises a locking rod, the locking rod is connected to the guide sleeve in a sliding mode, and a shifting rod is fixed to one end, far away from the rack, of the locking rod.
Preferably, the deflector rod is connected with the outer side wall of the guide sleeve through a second spring.
Preferably, the locking mechanism further comprises a locking hole formed in the rack and located on one side wall of the tooth, and the locking rod can be inserted into the locking hole.
Preferably, a stopping block is fixed in the groove, the stopping block is positioned on the left side of the stand, and the left end of the rack can be in abutting contact with the stopping block.
Compared with the prior art, the utility model discloses the beneficial effect who reaches is: when the aircraft bonnet is opened, latched device carries out the hasp restriction to the rack, thereby through connecting rod one, connecting rod two and gear play the supporting role to the aircraft bonnet, time saving and labor saving, need not the location, and the opening of a pair of aircraft bonnet of rack and spring plays the additional act, save strength, at the in-process that the aircraft bonnet was closed, compression spring one makes spring one hold power, so that when opening the aircraft bonnet next time, play the helping hand effect to the aircraft bonnet, and play the cushioning effect when closing the aircraft bonnet, reduce the damage of impact energy to the frame when the aircraft bonnet was closed, improve the security, the aircraft bonnet is accomodate in the recess after closing connecting rod one and connecting rod two, save space.
Drawings
The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention. In the drawings:
fig. 1 is a schematic structural view of a retracted state of a hood supporting device for a forklift according to the present invention;
fig. 2 is a structural schematic view of a supporting state of the hood supporting device for a forklift according to the present invention;
fig. 3 is a schematic view of the cross-sectional structure a-a in fig. 2.
In the figure: 1-a groove; 2-erecting a frame; 3, a guide sleeve; 4-a rack; 5, a first spring; 6-gear; 7-connecting rod one; 8-connecting rod two; 9-locking bar; 10-a keyhole; 11-a deflector rod; 12-spring two; 13-stop block.
Detailed Description
The preferred embodiments of the present invention will be described in conjunction with the accompanying drawings, and it will be understood that they are presented herein only to illustrate and explain the present invention, and not to limit the present invention.
Examples
As shown in fig. 1-3, a aircraft bonnet strutting arrangement for fork truck, including seting up recess 1 on the fork truck frame, recess 1 internal fixation has grudging post 2, the dead axle rotates on grudging post 2 and is connected with gear 6, be fixed with connecting rod 7 on the gear 6, connecting rod 7 keeps away from the one end dead axle of gear 6 and rotates the one end of connecting rod two 8, the other end of connecting rod two 8 is articulated with the aircraft bonnet, and the opening of connecting rod one 7 and connecting rod two 8 is towards the direction that opens and shuts of aircraft bonnet, recess 1 is internal fixation has uide bushing 3, and uide bushing 3 is located the right side of grudging post 2, sliding connection has rack 4 in the uide bushing 3, gear 6 is connected with rack 4 meshing, accessible latched device fixed connection between rack 4 and the uide bushing 3, rack 4 is connected through spring one 5 with the right side wall of recess 1.
In this embodiment, the locking mechanism includes a lock rod 9, the lock rod 9 is slidably connected to the guide sleeve 3, and a shift lever 11 is fixed to one end of the lock rod 9 away from the rack 9.
In this embodiment, the shift lever 11 is connected to the outer side wall of the guide sleeve 3 through a second spring 12.
In this embodiment, the locking mechanism further includes a locking hole 10 formed in the rack 4 on a side wall of the tooth, and the locking rod 9 is insertable into the locking hole 10.
In this embodiment, a stopping block 13 is fixed in the groove 1, the stopping block 13 is located on the left side of the stand 2, the left end of the rack 4 can be in abutting contact with the stopping block 13, when the rack 4 is in abutting contact with the stopping block 13, the lock rod 9 is just inserted into the lock hole 10, an included angle between the first connecting rod 7 and the second connecting rod 8 is always smaller than 180 degrees, the first connecting rod 7 and the second connecting rod 8 are prevented from forming a dead point position, and normal closing of the hood is ensured.
The utility model discloses a principle and advantage: according to the hood supporting device for the forklift, as shown in fig. 1 and 2, when a hood is in a cover closing state, a first spring 5 is in a compression state, a second spring 12 is in a tension state, in the hood opening process, the hood is lifted, and an included angle between a second connecting rod 8 and a first connecting rod 7 is increased, so that a gear 6 is driven to rotate clockwise, the clockwise rotation of the gear 6 drives a rack 4 to move left under the action of a guide sleeve 3 through the gear transmission action of the gear 6 and teeth on the rack 4, the left thrust is applied to the rack 4 by the first spring 5 in the left moving process of the rack 4, the clockwise rotation of the gear 6 is facilitated, the hood is driven to open through the first connecting rod 7 and the second connecting rod 8, the hood opening assisting effect is achieved, and the strength is saved;
with the increase of the opening angle of the hood, the rack 4 gradually approaches the stopping block 13, when the rack 4 contacts the stopping block 13, as shown in fig. 3, the lock rod 9 is just opposite to the lock hole 10, and the lock rod 9 is inserted in the lock hole 10 under the action of the second spring 12, so that the left and right movement of the rack 4 is limited by the lock rod 9, and the gear 6 cannot rotate, namely, the included angle between the first rack 7 and the second rack 8 cannot be increased or decreased, the support of the hood is realized, the time and the labor are saved, and the positioning is not needed;
when needs close the lid to the aircraft bonnet and close, make locking lever 9 and lockhole 10 break away from through driving lever 11, do not play the restriction effect to rack 4, thereby under the effect of the aircraft bonnet dead weight, make the contained angle of connecting rod 7 and connecting rod two 8 diminish, and drive 6 anticlockwise rotations of gear, thereby make rack 4 move to the right, and compression spring 5 makes spring 5 hold power, so that when opening the aircraft bonnet next time, play the helping hand effect to the aircraft bonnet, and play the cushioning effect when closing the aircraft bonnet, reduce the damage of impact energy to the frame when the aircraft bonnet closes, improve the security, the aircraft bonnet is accomodate in recess 1 at closing back connecting rod 7 and connecting rod two 8, and the space is saved.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described in the foregoing embodiments, or equivalents may be substituted for elements thereof. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims (5)

1. The utility model provides a aircraft bonnet strutting arrangement for fork truck, includes recess (1) of seting up on the fork truck frame, its characterized in that: recess (1) internal fixation has grudging post (2), the dead axle rotates on grudging post (2) and is connected with gear (6), be fixed with connecting rod (7) on gear (6), the one end dead axle that gear (6) were kept away from in connecting rod (7) rotates the one end of connecting rod two (8), the other end and the aircraft bonnet of connecting rod two (8) are articulated, recess (1) inside is fixed with uide bushing (3), and uide bushing (3) are located the right side of grudging post (2), sliding connection has rack (4) in uide bushing (3), gear (6) are connected with rack (4) meshing, accessible latched device fixed connection between rack (4) and uide bushing (3), rack (4) are connected through spring (5) with the right side wall of recess (1).
2. The hood stay device for a forklift according to claim 1, wherein: the locking mechanism comprises a locking rod (9), the locking rod (9) is connected to the guide sleeve (3) in a sliding mode, and a shifting rod (11) is fixed to one end, far away from the rack (4), of the locking rod (9).
3. The hood stay device for a forklift according to claim 2, wherein: the driving lever (11) is connected with the outer side wall of the guide sleeve (3) through a second spring (12).
4. The hood stay device for a forklift according to claim 2, wherein: the locking mechanism further comprises a locking hole (10) formed in the rack (4) and located on the side wall of one side of the teeth, and the locking rod (9) can be inserted into the locking hole (10).
5. The hood stay device for a forklift according to claim 1, wherein: a stopping block (13) is fixed in the groove (1), the stopping block (13) is located on the left side of the stand (2), and the left end of the rack (4) can be in abutting-buckling contact with the stopping block (13).
CN202020101152.1U 2020-01-17 2020-01-17 Aircraft bonnet strutting arrangement for fork truck Expired - Fee Related CN211688132U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202020101152.1U CN211688132U (en) 2020-01-17 2020-01-17 Aircraft bonnet strutting arrangement for fork truck

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202020101152.1U CN211688132U (en) 2020-01-17 2020-01-17 Aircraft bonnet strutting arrangement for fork truck

Publications (1)

Publication Number Publication Date
CN211688132U true CN211688132U (en) 2020-10-16

Family

ID=72771467

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202020101152.1U Expired - Fee Related CN211688132U (en) 2020-01-17 2020-01-17 Aircraft bonnet strutting arrangement for fork truck

Country Status (1)

Country Link
CN (1) CN211688132U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112246375A (en) * 2020-10-30 2021-01-22 常州川刃办公设备有限公司 Automatic paper shredder with paper pressing device
CN112246419A (en) * 2020-10-30 2021-01-22 常州川刃办公设备有限公司 Gland for paper shredder

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112246375A (en) * 2020-10-30 2021-01-22 常州川刃办公设备有限公司 Automatic paper shredder with paper pressing device
CN112246419A (en) * 2020-10-30 2021-01-22 常州川刃办公设备有限公司 Gland for paper shredder
CN112246419B (en) * 2020-10-30 2024-05-10 常州川刃办公设备有限公司 Gland for paper shredder
CN112246375B (en) * 2020-10-30 2024-05-14 常州川刃办公设备有限公司 Automatic paper shredder with paper pressing device

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GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20201016

Termination date: 20220117