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CN206342901U - A kind of recreation facility cockpit door lock mechanism - Google Patents

A kind of recreation facility cockpit door lock mechanism Download PDF

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Publication number
CN206342901U
CN206342901U CN201621444508.1U CN201621444508U CN206342901U CN 206342901 U CN206342901 U CN 206342901U CN 201621444508 U CN201621444508 U CN 201621444508U CN 206342901 U CN206342901 U CN 206342901U
Authority
CN
China
Prior art keywords
door
clutch component
bayonet lock
axle
clutch
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.)
Withdrawn - After Issue
Application number
CN201621444508.1U
Other languages
Chinese (zh)
Inventor
陈建生
胡兼
张斌
金晓俊
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.)
WENZHOU NANFANG AMUSEMENT RIDES CO Ltd
Original Assignee
WENZHOU NANFANG AMUSEMENT RIDES 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 WENZHOU NANFANG AMUSEMENT RIDES CO Ltd filed Critical WENZHOU NANFANG AMUSEMENT RIDES CO Ltd
Priority to CN201621444508.1U priority Critical patent/CN206342901U/en
Application granted granted Critical
Publication of CN206342901U publication Critical patent/CN206342901U/en
Withdrawn - After Issue legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model is related to a kind of recreation facility cockpit door lock mechanism.How mainly solve the cockpit door of large-scale recreation facility prevents passenger from being opened from inside and facilitates the problem of staff is opened.It is characterized in that:The lower end of the door body connector (1) is connected with first clutch component (4), the second clutch component (5) that can be slided up and down is set with main door axle (3), first clutch component (4) and the unidirectional end face ratchet (6) that mutually identical circle distribution is equipped with the corresponding end face of second clutch component (5), the lower end of second clutch component (5) is provided with spring (7), and second clutch component (5) is connected by cable wire (8) with pedal (9).The recreation facility cockpit door lock mechanism employs clutch, and cockpit door can be opened by visitor's self-locked and by staff, simple in construction, be occupied little space, safe and reliable, and cockpit door locks and opens easy to operate.

Description

A kind of recreation facility cockpit door lock mechanism
Technical field
The utility model is related to a kind of cockpit door locking device of large-scale recreation facility, and in particular to a kind of recreation facility seat Hatch door latch mechanism.
Background technology
In large-scale recreation facility, cockpit is the main carriers that visitor takes, and visitor is entered after cockpit, and cockpit door needs Locked, to ensure the safety of visitor, the cockpit for glass recreational machine of such as walking around.Existing cockpit door locking device generally uses seat Install lockset between hatch door and doorframe additional, locked and opened in outside by the staff of recreation ground, each cockpit door will Operation is locked and opened to progress manually, comparatively laborious.Therefore it provides one kind prevents passenger from being opened from inside and facilitates work Make the recreation facility cockpit door lock mechanism that personnel are opened, it is imperative.
Utility model content
In order to solve large-scale recreation facility cockpit door how to prevent passenger from inside open and facilitate staff to enter The problem of row is opened, the utility model provides a kind of recreation facility cockpit door lock mechanism, and the recreation facility cockpit door lock mechanism is adopted With clutch, cockpit door can prevent passenger from being opened from inside and facilitate staff to be opened, simple in construction, account for Small with space, safe and reliable, cockpit door locks and opens easy to operate.
The technical solution of the utility model is:It is solid that a kind of recreation facility cockpit door lock mechanism includes door body connector, door-hinge Reservation and main door axle, door body connector are mutually fixed with cockpit door, and lower end and the door-hinge fixed seat of main door axle are mutually fixed, door body connection Connected between part and door-hinge fixed seat by main door axle formation hinge, the lower end of the door body connector is connected with first clutch The second clutch component that can be slided up and down, first clutch component and second clutch group are set with component, main door axle The unidirectional end face ratchet of mutually identical circle distribution is equipped with the corresponding end face of part, the lower end of second clutch component is set There is spring, spring makes second clutch component have the elastic trend moved up, and second clutch component is by cable wire with stepping on Plate is connected;The side wall of the second clutch component is provided with neck, and one end of the neck is straight mouth, and the other end of neck is Domatic, the lower end of door body connector is provided with telescopic bayonet lock, and the external part of bayonet lock offsets with the side wall of second clutch component Touch, when stepping on pedal completely, bayonet lock is corresponding with neck, bayonet lock can be entered in neck along domatic when opening cockpit door.
The door body connector includes bearing block and overcoat, and main door axle runs through bearing block, set between main door axle and bearing block There is bearing, the upper end of main door axle is connected with the first tabletting group that can be slided up and down by general flat key, and the upper end of bearing block passes through Type thin flat key is connected with the second tabletting group that can be slided up and down, and the first tabletting group and the second tabletting group are mutually staggered; Gland, stage clip and locking nut are sequentially provided with above first tabletting group.
The lower end outer wall of the main door axle installs second clutch component by general flat key, during the lower end of main door axle is provided with Heart hole and its side wall are built-in with pull bar provided with bar hole, centre bore is oriented to, and the upper end of pull bar passes through pin and second clutch group Part is connected, and pin, which is located at, to be oriented in bar hole, the lower end connection cable wire of pull bar.
The main door axle is provided with the shaft shoulder, and the main door axle of shaft shoulder bottom is arranged on flange by general flat key, main door axle External part is fixed by round nut, and flange is mutually fixed with door-hinge fixed seat, and spring is located between the shaft shoulder and second clutch component.
The bayonet lock is arranged in bayonet lock set, bayonet lock set internal thread connection adjusting set, provided with card between adjusting set and bayonet lock Spring is sold, the external part of bayonet lock is spherical shape;Bayonet lock set is connected on door body connector by support.
The utility model has the advantages that:Due to taking above-mentioned technical proposal, first clutch component is employed The clutch constituted with second clutch component, cockpit door can prevent passenger from being opened from inside and facilitate staff to enter Row is opened, simple in construction, is occupied little space, safe and reliable, and cockpit door locks and opens easy to operate.
Brief description of the drawings
Accompanying drawing 1 is structure sectional view of the present utility model.
Accompanying drawing 2 is A-A structure sectional views in Fig. 1.
Accompanying drawing 3 is enlarged drawing at B in Fig. 1.
Accompanying drawing 4 is C-C structure sectional views in Fig. 3.
1- door body connector in figure, 2- door-hinge fixed seats, 3- main door axles, 4- first clutch components, 5- second clutches Component, 6- end face ratchets, 7- springs, 8- cable wires, 9- pedals, 10- necks, 11- bayonet locks, 12- bearing blocks, 13- overcoats, 14- axles Hold, 15- the first tabletting groups, 16- the second tabletting groups, 17- glands, 18- stage clips, 19- locking nuts, 20- centre bores, 21- is oriented to Bar hole, 22- pull bars, 23- pins, the 24- shaft shoulders, 25- flanges, 26- round nuts, 27- bayonet lock sets, 28- adjusting sets, 29- bayonet locks Spring, 30- supports.
Embodiment
The utility model is described in further detail below in conjunction with the accompanying drawings:
As shown in Fig. 1~Fig. 4, a kind of recreation facility cockpit door lock mechanism include door body connector 1, door-hinge fixed seat 2 and Main door axle 3, door body connector 1 is mutually fixed with cockpit door, and lower end and the door-hinge fixed seat 2 of main door axle 3 are mutually fixed, door body connector Connected between 1 and door-hinge fixed seat 2 by the formation hinge of main door axle 3, the lower end of the door body connector 1 is connected with the first clutch Be set with the second clutch component 5 that can be slided up and down on device assembly 4, main door axle 3, first clutch component 4 and second from The unidirectional end face ratchet 6 of mutually identical circle distribution, second clutch component are equipped with the corresponding end face of clutch component 5 5 lower end is provided with spring 7, and spring 7 makes second clutch component 5 have the elastic trend moved up, second clutch component 5 It is connected by cable wire 8 with pedal 9;The side wall of the second clutch component 5 is provided with neck 10, and one end of the neck 10 is Straight mouth, the other end of neck 10 is domatic, and the lower end of door body connector 1 is provided with telescopic bayonet lock 11, the external part of bayonet lock 11 Side wall with second clutch component 5 is inconsistent, when stepping on pedal 9 completely, and bayonet lock 11 is corresponding with neck 10, opens cockpit Bayonet lock 11 can be entered in neck 10 along domatic during door.Due to taking above-mentioned technical proposal, in use, by door body connector 1 Mutually fixed with cockpit door, door-hinge fixed seat 2 is fixed on cockpit body, when cockpit door is in opening, bayonet lock 11 is located at card In groove 10, second clutch component 5 is in released state with first clutch component 4, and when cockpit door is closed, bayonet lock 11 is with fellow disciple Body connector 1 is rotated, and bayonet lock 11 is slided to domatic one end of neck 10, and bayonet lock 11 is skidded off after neck 10, second clutch component 5 Move up and engaged with first clutch component 4 in the presence of spring 7, be i.e. first clutch component 4 and second clutch End face ratchet 6 on component 5 matches, now first clutch component 4 can only with respect to the one-directional rotation of second clutch component 5, Cockpit door can only be namely closed, but cockpit door can not be opened, cockpit door is closed to be locked out opening in place afterwards, in cockpit Visitor can not be out of cockpit by cockpit door opening.After recreation facility end of run, staff depresses pedal 9, and pedal 9 passes through steel The drawing second clutch of rope 8 component 5 is moved downward, and second clutch component 5 departs from first clutch component 4, cockpit door Latch-release, can now open cockpit door, cockpit door is when turning an angle, and bayonet lock 11 enters neck 10, by second from Clutch component 5 is locked, and lifting the second clutch component 5 of pedal 9 will not also move upwards, and cockpit door is opened, and visitor walks out cockpit, Next group visitor is waited to enter.The utility model employs the clutch that first clutch component 4 is constituted with second clutch component 5 Mechanism, cockpit door can prevent passenger from being opened from inside and facilitate staff to be opened, simple in construction, take empty Between it is small, it is safe and reliable, cockpit door locking and open easy to operate.
The door body connector 1 includes bearing block 12 and overcoat 13, and main door axle 3 runs through bearing block 12, main door axle 3 and bearing Bearing 14 is provided between seat 12, the upper end of main door axle 3 is connected with the first tabletting group 15 that can be slided up and down, axle by general flat key The upper end of bearing 12 is connected with the second tabletting group 16 that can be slided up and down, the first tabletting group 15 and second by type thin flat key Tabletting group 16 is mutually staggered;The top of first tabletting group 15 is sequentially provided with gland 17, stage clip 18 and locking nut 19.Pass through The frictional force between the first tabletting group 15 and the second tabletting group 16 is adjusted, enables the staying at random location of door body connector 1, makes again Cockpit door opens and closes effortless.
The lower end outer wall of the main door axle 3 installs second clutch component 5 by general flat key, and the lower end of main door axle 3 is set There is centre bore 20 and its side wall is built-in with pull bar 22 provided with bar hole 21, centre bore 20 is oriented to, the upper end of pull bar 22 passes through pin 23 are connected with second clutch component 5, and pin 23, which is located at, to be oriented in bar hole 21, the lower end connection cable wire 8 of pull bar 22.Pull bar 22 In centrally disposed hole 20, structure is compacter, is oriented to bar hole 21 and is oriented to and position-limiting action, makes second clutch component 5 It is at the position and bayonet lock 11 and the position of the locking of neck 10 engaged with first clutch component 4.
The main door axle 3 is provided with the shaft shoulder 24, and the main door axle 3 of the bottom of the shaft shoulder 24 is arranged on flange 25 by general flat key On, the external part of main door axle 3 is fixed by round nut 26, and flange 25 is mutually fixed with door-hinge fixed seat 2, spring 7 be located at the shaft shoulder 24 with Between second clutch component 5.The structure is easy to process and assembled.
The bayonet lock 11 is arranged in bayonet lock set 27, and bayonet lock covers 27 internal threads connection adjusting set 28, adjusting set 28 and bayonet lock Bayonet lock spring 29 is provided between 11, the external part of bayonet lock 11 is spherical shape;Bayonet lock set 27 is connected to door body by support 30 and connected On part 1.Beneficial to the flexible of bayonet lock 11, meanwhile, also will not be by jam when bayonet lock 11 skids off neck 10.

Claims (5)

1. a kind of recreation facility cockpit door lock mechanism, including door body connector (1), door-hinge fixed seat (2) and main door axle (3), door Body connector (1) is mutually fixed with cockpit door, and lower end and the door-hinge fixed seat (2) of main door axle (3) are mutually fixed, door body connector (1) It is connected between door-hinge fixed seat (2) by main door axle (3) formation hinge, it is characterised in that:Under the door body connector (1) End is connected with the second clutch component (5) that is set with and can slide up and down on first clutch component (4), main door axle (3), the One clutch pack (4) and the list that mutually identical circle distribution is equipped with the corresponding end face of second clutch component (5) To end face ratchet (6), the lower end of second clutch component (5) is provided with spring (7), and spring (7) has second clutch component (5) There is the elastic trend moved up, second clutch component (5) is connected by cable wire (8) with pedal (9);The second clutch The side wall of component (5) is provided with neck (10), and one end of the neck (10) is straight mouth, the other end of neck (10) be it is domatic, The lower end of door body connector (1) is provided with telescopic bayonet lock (11), external part and the second clutch component (5) of bayonet lock (11) Side wall is inconsistent, and when stepping on pedal (9) completely, bayonet lock (11) is corresponding with neck (10), bayonet lock (11) when opening cockpit door It can be entered along domatic in neck (10).
2. a kind of recreation facility cockpit door lock mechanism according to claim 1, it is characterised in that:The door body connector (1) bearing block (12) and overcoat (13) are included, main door axle (3) runs through bearing block (12), between main door axle (3) and bearing block (12) Provided with bearing (14), the upper end of main door axle (3) is connected with the first tabletting group (15) that can be slided up and down, bearing by general flat key The upper end of seat (12) is connected with the second tabletting group (16) that can be slided up and down by type thin flat key, the first tabletting group (15) with Second tabletting group (16) is mutually staggered;Gland (17), stage clip (18) and lock are sequentially provided with above first tabletting group (15) Tight nut (19).
3. a kind of recreation facility cockpit door lock mechanism according to claim 1 or 2, it is characterised in that:The main door axle (3) Lower end outer wall second clutch component (5) is installed by general flat key, the lower end of main door axle (3) provided with centre bore (20) and its Side wall is built-in with pull bar (22) provided with bar hole (21), centre bore (20) is oriented to, the upper end of pull bar (22) by pin (23) with Second clutch component (5) is connected, and pin (23), which is located at, to be oriented in bar hole (21), the lower end connection cable wire (8) of pull bar (22).
4. a kind of recreation facility cockpit door lock mechanism according to claim 3, it is characterised in that:On the main door axle (3) Provided with the shaft shoulder (24), the main door axle (3) of the shaft shoulder (24) bottom is arranged on flange (25) by general flat key, and main door axle (3) is stretched Go out end fixed by round nut (26), flange (25) is mutually fixed with door-hinge fixed seat (2), spring (7) is located at the shaft shoulder (24) and the Between two clutch packs (5).
5. a kind of recreation facility cockpit door lock mechanism according to claim 1 or 2, it is characterised in that:The bayonet lock (11) In bayonet lock set (27), bayonet lock set (27) internal thread connection adjusting set (28) is set between adjusting set (28) and bayonet lock (11) There is bayonet lock spring (29), the external part of bayonet lock (11) is spherical shape;Bayonet lock set (27) is connected to door body by support (30) and connected On part (1).
CN201621444508.1U 2016-12-27 2016-12-27 A kind of recreation facility cockpit door lock mechanism Withdrawn - After Issue CN206342901U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201621444508.1U CN206342901U (en) 2016-12-27 2016-12-27 A kind of recreation facility cockpit door lock mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201621444508.1U CN206342901U (en) 2016-12-27 2016-12-27 A kind of recreation facility cockpit door lock mechanism

Publications (1)

Publication Number Publication Date
CN206342901U true CN206342901U (en) 2017-07-21

Family

ID=59318074

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201621444508.1U Withdrawn - After Issue CN206342901U (en) 2016-12-27 2016-12-27 A kind of recreation facility cockpit door lock mechanism

Country Status (1)

Country Link
CN (1) CN206342901U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106474739A (en) * 2016-12-27 2017-03-08 温州南方游乐设备工程有限公司 A kind of recreation facility passenger cabin door lock mechanism
EP3871745A1 (en) 2020-02-28 2021-09-01 Poma Cabin provided with a device for locking and unlocking the doors and installation for transporting passengers comprising at least one such cabin

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106474739A (en) * 2016-12-27 2017-03-08 温州南方游乐设备工程有限公司 A kind of recreation facility passenger cabin door lock mechanism
EP3871745A1 (en) 2020-02-28 2021-09-01 Poma Cabin provided with a device for locking and unlocking the doors and installation for transporting passengers comprising at least one such cabin
FR3107653A1 (en) 2020-02-28 2021-09-03 Poma Cabin equipped with a device for locking and unlocking the doors and passenger transport installation comprising at least one such cabin

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Legal Events

Date Code Title Description
GR01 Patent grant
AV01 Patent right actively abandoned
AV01 Patent right actively abandoned

Granted publication date: 20170721

Effective date of abandoning: 20180622