CN203358815U - Telescopic draw rod mechanism - Google Patents

Telescopic draw rod mechanism Download PDF

Info

Publication number
CN203358815U
CN203358815U CN 201320449037 CN201320449037U CN203358815U CN 203358815 U CN203358815 U CN 203358815U CN 201320449037 CN201320449037 CN 201320449037 CN 201320449037 U CN201320449037 U CN 201320449037U CN 203358815 U CN203358815 U CN 203358815U
Authority
CN
China
Prior art keywords
mounting bracket
hinge
sleeve
hatch cover
joint
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 - Lifetime
Application number
CN 201320449037
Other languages
Chinese (zh)
Inventor
张海涛
刘涛
姜瑛
赵俊海
张美荣
张永祥
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.)
China National Offshore Oil Corp CNOOC
Offshore Oil Engineering Co Ltd
702th Research Institute of CSIC
COOEC Subsea Technology Co Ltd
Original Assignee
SHENZHEN SEA OIL ENGINEERING UNDERWATER TECHNOLOGY CO LTD
China National Offshore Oil Corp CNOOC
Offshore Oil Engineering Co Ltd
702th Research Institute of CSIC
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 SHENZHEN SEA OIL ENGINEERING UNDERWATER TECHNOLOGY CO LTD, China National Offshore Oil Corp CNOOC, Offshore Oil Engineering Co Ltd, 702th Research Institute of CSIC filed Critical SHENZHEN SEA OIL ENGINEERING UNDERWATER TECHNOLOGY CO LTD
Priority to CN 201320449037 priority Critical patent/CN203358815U/en
Application granted granted Critical
Publication of CN203358815U publication Critical patent/CN203358815U/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Landscapes

  • Pivots And Pivotal Connections (AREA)

Abstract

The utility model relates to a telescopic draw rod mechanism which comprises a length-adjustable draw rod, a corner knuckle bearing, a cylindrical knuckle bushing and locking nuts, wherein the length-adjustable draw rod comprises a sleeve, and left and right eyelet bolt joints which are sleeved on the sleeve; the corner knuckle bearing is mounted together with the right eyelet bolt joint; the cylindrical knuckle bushing is mounted on the left eyelet bolt joint; the locking nuts are mounted at both ends of the sleeve and fix the left and right eyelet bolt joints in preset positions on the sleeve; a mounting bracket hinged on an upper-end supporting point and a mounting bracket hinged on a lower-end supporting point are respectively pivoted on the left and right eyelet bolt joints; and the mounting brackets and a right-angle rocker of a hatch deck are pivoted to form a whole, and the mounting brackets and the right-angle rocker together form a parallelogram structure in the transverse plane. According to the utility model, motion coordination can be performed on the hatch deck of a sea cabin in the opening/closing process of the hatch deck of the sea cabin, so that the motion track of the hatch deck of the sea cabin is always in a translational motion state; and the reliability and safety of an opening/closing mechanism of the hatch deck of the sea cabin are improved.

Description

Telescopic handle mechanism
Technical field
The utility model relates to drag link mechanism, relates in particular to a kind of Telescopic handle mechanism of the sea hatch cover opening/closing mechanism for space station, deep-sea or bathyscaph, submarine.
Background technology
Maritime cabin is remote underwater manipulation robot (Remotely Operated Vehicle, ROV) or single normobaric diving harness (Atmospheric Diving Suit, ADS), a trouble free service passage of turnover space station, deep-sea or bathyscaph, submarine, and sea hatch cover opening/closing mechanism is that robot (ROV) and single normobaric diving harness (ADS) are laid and the critical component reclaimed.It is to adopt two opposite opened hatch covers, and opens hatch cover with the mode of operation of outside translation respectively.
At present, state, inside and outsidely generally adopt convertible and sliding sea hatch cover opening/closing mechanism.Convertible hatch cover mechanism for opening/closing is to adopt two opposite opened hatch covers, and opens or closes hatch cover with mode of operation outside, inwardly upset respectively; And sliding hatch cover mechanism for opening/closing, to utilize the mode of operation that dragging track carries out slipping motion to be set on the outside face of space station, deep-sea to open or close hatch cover, when for robot (ROV), being laid under water and reclaiming, provide a servicesubway.
In existing translational sea hatch cover opening/closing mechanism, in order to keep hatch cover, opening, in closing course all the time in the translation state, adopted the space parallel four-bar mechanism, that is: by the right angle rocking arm, the geometric configuration of the space parallel four-bar mechanism that a pull bar and upper and lower four hinges installation fulcrum form, any position of its spatial four-bar mechanism is all parallelogram in the projection of Transverse plane, like this, just from geometrical property and the hinge of mechanism itself, install position of the fulcrum, guaranteed the path of motion of hatch cover, wherein, the articulationes cylindroideus lining is equipped with at the pull bar two ends, and its length is fixed.The shortcoming of its existence is as follows:
(1) due to right angle rocking arm and pull bar and by upper and lower four hinges, the four-bar mechanism that fulcrum forms to be installed be the space parallel four-bar mechanism, it requires four hinge axes of four-bar mechanism, spatially to meet very high parallelism requirement, otherwise, in hatch cover unlatching, closing course, there will be pull bar " stuck " phenomenon, last, cause hatch cover to rest on a certain position, can't open, closure;
(2) because pull bar (comprising: the upper and lower hinge of right angle rocking arm and pull bar is installed fulcrum) two ends are all to adopt the articulationes cylindroideus lining, and the articulationes cylindroideus lining only has a degree of freedom rotated along its axis direction, it can not be regulated the rotational freedom of other direction automatically, like this, just increased the difficulty in the processing of hatch cover mechanism for opening/closing and Installation and Debugging, simultaneously, also be unfavorable for care and maintenance in the future;
(3) length due to drag link mechanism is changeless, and therefore, it can not carry out length adjustment, can only be by adjusting the position that under pull bar, hinge is installed fulcrum, carry out the motor coordination relation of adjusting cabin lid mechanism for opening/closing, mounting process is unreasonable, the Operation and Maintenance inconvenience.
The utility model content
Main purpose of the present utility model is to overcome the above-mentioned shortcoming that prior art exists, and provide the Telescopic handle mechanism of an a kind of end with angle Zhi Guanjie, it can be in the hatch cover opening-closing process of maritime cabin, maritime cabin hatch cover is carried out to motor coordination, make maritime cabin hatch cover path of motion all the time in the motion of translation state; The pull bar that may occur " stuck " phenomenon, the reliability and the safety that have improved sea hatch cover opening/closing mechanism have been avoided at maritime cabin hatch cover in unlatching, closing motion process; Simultaneously, reduced processing and the setting accuracy of sea hatch cover opening/closing mechanism, be convenient to maintenance and safeguard.
The purpose of this utility model is realized by following technical scheme:
A kind of Telescopic handle mechanism, it is characterized in that: comprising: oscillating bearing, articulationes cylindroideus lining, jam nut are propped up in length-adjustable pull bar, angle, wherein, length-adjustable pull bar comprises: sleeve, be sleeved on the auris dextra ring bolt joint in sleeve one end and be sleeved on the left earrings screwed joint in the sleeve other end; This angle is propped up between the endoporus of outer ring by interference fit and auris dextra ring bolt joint of oscillating bearing and is installed together; This articulationes cylindroideus lining is arranged on left earrings screwed joint, and this jam nut is arranged on the two ends of sleeve, and auris dextra ring bolt joint and left earrings screwed joint is fixed on to the desired location of sleeve; Be articulated with respectively the mounting bracket of a upper and lower end fulcrum hinge on auris dextra ring bolt joint and left earrings screwed joint, the mounting bracket of this upper and lower end fulcrum hinge and the right angle rocking arm pivot joint of hatch cover are integrated, and at a parallelogram sturcutre of the common composition of Transverse plane.
The mounting bracket of described upper end fulcrum hinge is poor with the setting height(from bottom) of the mounting bracket of the fulcrum hinge that is positioned at rocking arm upper end, hatch cover right angle to be equated with the poor Δ h of setting height(from bottom) of the mounting bracket of hatch cover right angle rocking arm lower sustainer hinge with the mounting bracket of pull bar lower sustainer hinge; The mounting bracket of pull bar upper end fulcrum hinge equates with the transverse horizontal distance of the mounting bracket of hatch cover right angle rocking arm lower sustainer hinge with the mounting bracket of pull bar lower sustainer hinge with the transverse horizontal distance, delta L of the mounting bracket of rocking arm upper end, hatch cover right angle fulcrum hinge.
It is the spherical joint bearing that oscillating bearing is propped up at described angle.
Described articulationes cylindroideus lining is plain bearing.
The beneficial effects of the utility model:
(1) because the drag link mechanism hinge is installed fulcrum employing spherical joint bearing, and the degree of freedom (being commonly called as " universal hinge ") that the spherical joint bearing has three directions to rotate, like this, can open at hatch cover, in closing course, the lower hinge of pull bar is installed fulcrum can automatic position adjusting function, not there will be pull bar " stuck " phenomenon, guaranteed reliability and the safety of sea hatch cover opening/closing mechanism system;
(2) by right angle rocking arm and pull bar and upper and lower four hinges, installed during fulcrum formed the space parallel four-bar mechanism, wherein, the lower hinge of pull bar is installed fulcrum and is adopted the spherical joint bearing, like this, just processing and the setting accuracy of sea hatch cover opening/closing mechanism have been reduced, simultaneously, also be convenient to later maintenance and handling labor;
(3) what adopt due to the drag link mechanism two ends is left and right earrings screwed joint, like this, can carry out by the length of adjusting pull bar the running orbit of further adjusting cabin lid mechanism for opening/closing.And, after the pull bar length adjustment, directly use two left-right rotary nut lockings, easy to operate, mounting process is reasonable.
The accompanying drawing explanation:
Fig. 1 is the utility model profile schematic diagram.
Fig. 2 is the utility model cross-sectional schematic.
Fig. 3 is that the utility model lower end installation fulcrum hinge arrangement master looks schematic diagram.
Fig. 4 is that fulcrum hinge arrangement schematic top plan view is installed in the utility model lower end.
Fig. 5 is the utility model upper and lower end hinge fulcrum scheme of installation.
Major label description in figure:
Sleeve, 2. auris dextra ring bolt joint, 3. oscillating bearing, 4. left earrings screwed joint, 5. articulationes cylindroideus lining, 6. jam nut, 7. mounting bracket, 8. maritime cabin section structure, 9. mounting bracket, 10. hatch cover, 11. rocking arm lower ends, right angle, 12. rocking arm upper ends, right angle, 13. right angle rocking arms are propped up in angle.
The specific embodiment
As Figure 1-Figure 4, the utility model comprises: the mounting bracket 7 of oscillating bearing 3, articulationes cylindroideus lining 5, jam nut 6, lower sustainer hinge and the mounting bracket 9 of upper end fulcrum hinge are propped up in length-adjustable pull bar, angle, wherein, length-adjustable pull bar comprises: sleeve 1, be sleeved on the auris dextra ring bolt joint 2 in sleeve 1 one ends and be sleeved on the left earrings screwed joint 4 in sleeve 1 other end; Angle is propped up between the endoporus of outer ring by interference fit and auris dextra ring bolt joint 2 of oscillating bearing 3 and is installed togather; Owing to propping up oscillating bearing 3 and belong to the spherical joint bearing in angle, so the degree of freedom that has three directions to rotate, reduced processing and the setting accuracy of hatch cover mechanism for opening/closing effectively.Articulationes cylindroideus lining 5 mode with bolts is arranged on left earrings screwed joint 4, and jam nut 6 is arranged on the two ends of sleeve 1, and auris dextra ring bolt joint 2 and left earrings screwed joint 4 is fixed on to the desired location of sleeve 1; On auris dextra ring bolt joint 2 and left earrings screwed joint 4, adopt the bearing pin connection mode to be articulated with respectively a mounting bracket (7,9), the mounting bracket (7,9) of upper and lower end fulcrum hinge is in order to the right angle rocking arm pivot joint with hatch cover.
As in Figure 3-5, maritime cabin is the servicesubway of robot or single normobaric diving harness turnover space station, deep-sea, and maritime cabin section structure 8 is for the supporting construction of lower sustainer hinge mounting support 7 of the present utility model is installed; Right angle rocking arm 13 is the working loads (comprising weight) for supporting hatch cover 10, and it and the utility model form the space parallel four-bar mechanism jointly, with guarantee hatch cover 10 opening, in closing course all the time in the translation mode of operation.
During use, mounting bracket (9 by upper and lower end fulcrum hinge, 7) with the mounting bracket of the fulcrum hinge of the upper/lower terminal of the right angle rocking arm 11 of hatch cover 10, adopt the pivot joint of chain connection mode to be integrated respectively, and in " parallelogram " structure of the common composition of Transverse plane, that is: the mounting bracket 9 of upper end fulcrum hinge is poor with the setting height(from bottom) of the mounting bracket of the fulcrum hinge that is positioned at rocking arm upper end, hatch cover right angle 12 equates with the poor Δ h of setting height(from bottom) of the mounting bracket of rocking arm lower end, hatch cover right angle 11 fulcrum hinges with the mounting bracket 7 of pull bar lower sustainer hinge; The mounting bracket 9 of pull bar upper end fulcrum hinge equates with the transverse horizontal distance of the mounting bracket of rocking arm lower end, hatch cover right angle 11 fulcrum hinges with the mounting bracket 7 of pull bar lower sustainer hinge with the transverse horizontal distance, delta L of the mounting bracket of rocking arm upper end, hatch cover right angle 12 fulcrum hinges.
When the installation of hatch cover mechanism for opening/closing meets above condition, the geometric configuration of the spatial four-bar mechanism be comprised of 12, lower end 11, rocking arm upper end, right angle and upper and lower four hinges installation of pull bar fulcrum is all parallelogram on horizontal any position, like this, just from geometrical property and the hinge of mechanism itself, install position of the fulcrum, guaranteed the path of motion of hatch cover, that is: hatch cover in opening-closing process all in the translation state.
Oscillating bearing 3 is propped up for the spherical joint bearing in above-mentioned angle, and it has the rotational freedom of three directions; Articulationes cylindroideus lining 5 is plain bearing, and it only has a direction, that is: the rotational freedom of axis; Jam nut 6 is after the pull bar length adjustment, and it is locked, and has locking function.
The above, it is only preferred embodiment of the present utility model, not the utility model is done to any pro forma restriction, any simple modification, equivalent variations and modification that every foundation technical spirit of the present utility model is done above embodiment, all still belong in the scope of technical solutions of the utility model.

Claims (4)

1. a Telescopic handle mechanism, it is characterized in that: comprising: oscillating bearing, articulationes cylindroideus lining, jam nut are propped up in length-adjustable pull bar, angle, wherein, length-adjustable pull bar comprises: sleeve, be sleeved on the auris dextra ring bolt joint in sleeve one end and be sleeved on the left earrings screwed joint in the sleeve other end; This angle is propped up between the endoporus of outer ring by interference fit and auris dextra ring bolt joint of oscillating bearing and is installed together; This articulationes cylindroideus lining is arranged on left earrings screwed joint, and this jam nut is arranged on the two ends of sleeve, and auris dextra ring bolt joint and left earrings screwed joint is fixed on to the desired location of sleeve; Be articulated with respectively the mounting bracket of a upper and lower end fulcrum hinge on auris dextra ring bolt joint and left earrings screwed joint, the mounting bracket of this upper and lower end fulcrum hinge and the right angle rocking arm pivot joint of hatch cover are integrated, and at a parallelogram sturcutre of the common composition of Transverse plane.
2. Telescopic handle according to claim 1 mechanism, it is characterized in that: the mounting bracket of described upper end fulcrum hinge is poor with the setting height(from bottom) of the mounting bracket of the fulcrum hinge that is positioned at rocking arm upper end, hatch cover right angle to be equated with the poor Δ h of setting height(from bottom) of the mounting bracket of hatch cover right angle rocking arm lower sustainer hinge with the mounting bracket of pull bar lower sustainer hinge; The mounting bracket of pull bar upper end fulcrum hinge equates with the transverse horizontal distance of the mounting bracket of hatch cover right angle rocking arm lower sustainer hinge with the mounting bracket of pull bar lower sustainer hinge with the transverse horizontal distance, delta L of the mounting bracket of rocking arm upper end, hatch cover right angle fulcrum hinge.
3. Telescopic handle according to claim 1 mechanism, it is characterized in that: it is the spherical joint bearing that oscillating bearing is propped up at described angle.
4. Telescopic handle according to claim 1 mechanism, it is characterized in that: described articulationes cylindroideus lining is plain bearing.
CN 201320449037 2013-07-26 2013-07-26 Telescopic draw rod mechanism Expired - Lifetime CN203358815U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201320449037 CN203358815U (en) 2013-07-26 2013-07-26 Telescopic draw rod mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201320449037 CN203358815U (en) 2013-07-26 2013-07-26 Telescopic draw rod mechanism

Publications (1)

Publication Number Publication Date
CN203358815U true CN203358815U (en) 2013-12-25

Family

ID=49806613

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201320449037 Expired - Lifetime CN203358815U (en) 2013-07-26 2013-07-26 Telescopic draw rod mechanism

Country Status (1)

Country Link
CN (1) CN203358815U (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106828950A (en) * 2016-12-09 2017-06-13 上海航空电器有限公司 A kind of mounting structure of control board bracket
CN107685724A (en) * 2017-09-11 2018-02-13 杨志泉 Anti-lock brake mechanism and with the vehicle of the mechanism, anti-lock brake method
CN110053713A (en) * 2019-03-14 2019-07-26 哈尔滨工程大学 A kind of latent device hatchcover of spherical shape manned capsule
CN114889785A (en) * 2022-05-10 2022-08-12 哈尔滨工程大学 AUV underwater dry type storage device

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106828950A (en) * 2016-12-09 2017-06-13 上海航空电器有限公司 A kind of mounting structure of control board bracket
CN107685724A (en) * 2017-09-11 2018-02-13 杨志泉 Anti-lock brake mechanism and with the vehicle of the mechanism, anti-lock brake method
CN110053713A (en) * 2019-03-14 2019-07-26 哈尔滨工程大学 A kind of latent device hatchcover of spherical shape manned capsule
CN110053713B (en) * 2019-03-14 2020-12-08 哈尔滨工程大学 Spherical manned cabin submersible vehicle cover
CN114889785A (en) * 2022-05-10 2022-08-12 哈尔滨工程大学 AUV underwater dry type storage device
CN114889785B (en) * 2022-05-10 2023-09-29 哈尔滨工程大学 AUV (autonomous Underwater vehicle) underwater dry storage device

Similar Documents

Publication Publication Date Title
CN203358815U (en) Telescopic draw rod mechanism
US20070278345A1 (en) Device for articulating a door of a nacelle of an aircraft and nacelle provided with said articulation device
CN102514466B (en) Skylight of commercial vehicle
CN104290901B (en) Double-rocker transmission mechanism applicable to movable control surface of aerial vehicle
CN105064841B (en) A kind of torsion-beam-type passenger plane hatch door opens drive mechanism
CN105857568A (en) Intra-cabin and extra-cabin linkage type cabin door lock mechanism
CN109533237A (en) A kind of autonomous underwater robot lays recycling single-point lifting and only swings protective device
CN205277086U (en) Garbage truck back door locking mechanism
CN202518681U (en) Storage equipment and hand rail thereof
CN205499321U (en) Inside and outside coordinated type cabin door lock mechanism
CN103612717B (en) A kind of air assisted hatch board
CN201592714U (en) Opening and closing mechanism of motor train unit head end cover
CN205531998U (en) On lift a mechanism
US7273989B2 (en) Actuator safety attachment device
CN203321153U (en) Lower hinge device of aluminium alloy window
CN205440093U (en) Loading and unloading goods structure of refrigerator carriage
CN201009940Y (en) Unlocking mechanism of vehicle fuel tank door
CN203961542U (en) A kind of adjustable caging device of offroad vehicle escape window
CN206766141U (en) Front wall outer panel component and the vehicle using the component
CN203402810U (en) Anti-shedding hook
CN205370191U (en) Door is opened and close soon to hand wheel
CN204715989U (en) Translation pivoted arm structure and comprise its passenger car bin-gate
CN103527042B (en) Emergency evacuation door is with laying out turning-up devices outward and laying out the method for turning over outward
CN205502823U (en) Take limit function's quick dismantlement hinge
CN210264360U (en) Pneumatic automatic door

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CP01 Change in the name or title of a patent holder
CP01 Change in the name or title of a patent holder

Address after: 100010 Chaoyangmen North Street, Dongcheng District, Dongcheng District, Beijing

Co-patentee after: OFFSHORE OIL ENGINEERING Co.,Ltd.

Patentee after: CHINA NATIONAL OFFSHORE OIL Corp.

Co-patentee after: COOEC SUBSEA TECHNOLOGY Co.,Ltd.

Co-patentee after: No.702 Research Institute of China Shipbuilding Industry Corp.

Address before: 100010 Chaoyangmen North Street, Dongcheng District, Dongcheng District, Beijing

Co-patentee before: OFFSHORE OIL ENGINEERING Co.,Ltd.

Patentee before: CHINA NATIONAL OFFSHORE OIL Corp.

Co-patentee before: COOEC SUBSEA TECHNOLOGY Co.,Ltd.

Co-patentee before: No.702 Research Institute of China Shipbuilding Industry Corp.

CX01 Expiry of patent term
CX01 Expiry of patent term

Granted publication date: 20131225