CN2060905U - Rotary damping wing panel with the function of automatic developing - Google Patents

Rotary damping wing panel with the function of automatic developing Download PDF

Info

Publication number
CN2060905U
CN2060905U CN 89209750 CN89209750U CN2060905U CN 2060905 U CN2060905 U CN 2060905U CN 89209750 CN89209750 CN 89209750 CN 89209750 U CN89209750 U CN 89209750U CN 2060905 U CN2060905 U CN 2060905U
Authority
CN
China
Prior art keywords
wing
utility
model
type material
arbor
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 89209750
Other languages
Chinese (zh)
Inventor
王能任
张学勤
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.)
LIAOYANG AUTOMATION INSTRUMENT FACTORY
Original Assignee
LIAOYANG AUTOMATION INSTRUMENT FACTORY
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 LIAOYANG AUTOMATION INSTRUMENT FACTORY filed Critical LIAOYANG AUTOMATION INSTRUMENT FACTORY
Priority to CN 89209750 priority Critical patent/CN2060905U/en
Publication of CN2060905U publication Critical patent/CN2060905U/en
Expired - Lifetime legal-status Critical Current

Links

Images

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The utility model relates to the technical field of an instrument, particularly a rotary damping wing panel with the function of automatic expansion installed on a restricted rotation type material level controller (also called restricted rotation type material surface annunciator). The utility model is composed of a wing handle shaft, two wing panels, steel balls, springs, screw plugs, etc., wherein, the two wing panels can be rotated and stacked together and can automatically expand so that the connection between the restricted rotation type material level controller and a silo container can be changed into the connection in a pipe screw thread type, which provides conditions for small volume, light weight, low cost and easy assembly and disassembly for the controller. Simultaneously, the two wing panels of the utility model are in symmetric distribution with smooth rotation, which comparatively extends the service life of the restricted rotation type material surface controller. The width of each of the two wing panel can be designed according to the size of a pipe screw thread, and the length can be changed as required.

Description

Rotary damping wing panel with the function of automatic developing
The utility model relates to field of instrumentation technology, particularly a kind of gyrodamping fin that can launch automatically that (also claims blocking rotary type charge level signalling device, blocking rotary type level-sensing device) on the blocking rotary type charge level controller.
At present both at home and abroad the damping fin on the blocking rotary type charge level controller that uses is fixed, has single-blade, double-vane, four wings fixed as what U.S. thatch Nitor produced; Japan Toko Bussdan Co., Ltd. be that double-vane is fixed, these blocking rotary type charge level controllers, because of being subjected to the restriction of damping fin physical dimension, make itself and being connected of storage bin container mostly be the flange mode, thereby cause the big body weight of blocking rotary type charge level controller shape, high again, the loading and unloading inconvenience of cost.For this reason, the damping fin of the blocking rotary type charge level controller that U.S. thatch Nitor and Shanghai Automatic Instrument and Meter Factory No.5 produce just adopts the big knife-edge of single-blade fixed, changes charge level controller and being connected of storage bin container into screw-type.But such charge level controller is the one-sided distribution of single-blade because of the damping fin, and rotation is got up not steady, will inevitably shorten the serviceable life of charge level controller.
The utility model is intended to overcome the defective of above-mentioned prior art, for the blocking rotary type charge level controller a kind of novel structure is provided, make simple, easy to loading and unloading, the gyrodamping fin that can launch automatically.
For achieving the above object, the utility model is to be made of wing arbor, fin, steel ball, spring and plug etc.Wing arbor is hollow, the flat fork of groove milling in the middle of the one end is provided with, flat stick adorning two with two pins can rotating fin, an end of fin is circular-arc.The other end the inside car of wing arbor has screw thread, also is provided with a pin-and-hole.After in wing arbor hollow, a steel ball, a spring being housed, refill a plug.Screw plug, spring is pressed just to produce an axial force, promotes two fins by steel ball around pin revolution and launch, until two fins and wing arbor in vertical state.
The utility model compared with prior art advantage is a lot: two fins can turn round folded and can launch automatically again together, thereby got rid of the structure that blocking rotary type charge level controller and storage bin container must take the flange to be connected, what replace is the pipe thread connected mode, and this is blocking rotary type charge level controller reduced volume, weight reduction, reduces cost and created advantage.Two fins of the present utility model are symmetrical distribution, rotation steadily, stressed evenly, no impact shock has prolonged serviceable life of blocking rotary type charge level controller relatively.The width of two fins of the present utility model can be by the size design in a kind of pipe thread hole, and its length can change as required.The on-the-spot installation and removal of the utility model all make things convenient for.
Accompanying drawing is a structural representation of the present utility model.
Below in conjunction with accompanying drawing, further set forth embodiment of the present utility model.
Referring to accompanying drawing, the utility model is by hollow wing arbor 1, formations such as fin 7, steel ball 5, spring 4 and plug 3.The flat fork of groove milling in the middle of an end of wing arbor 1 is provided with, flat stick adorning two with two pins 6 can rotating fin 7, an end of fin 7 is circular-arc.The other end the inside car of wing arbor 1 has screw thread, also is provided with a pin-and-hole 2.After in wing arbor 1 hollow, steel ball 5, spring 4 being housed, refill a plug 3.
Tighten plug 3, spring 4 is compressed and just produces an axial force, promote the arc sections of two fins 7 by steel ball 5, two fins 7 are launched around pin 6 opposing revolutions respectively, until two fins 7 and wing arbor 1 in vertical state, two fins 7 are because of being subjected to the spacing stop of wing arbor 1 side.Two fins, 7 turning courses, the arc surface on the fin 7 contacts with steel ball all the time.When giving two fins 7 to closing up direction when applying torque, two fins 7 just turn round and folded and together around pin 6 respectively in opposite directions, are parastate with wing arbor 1.This moment, the circular arc position of two fins 7 made steel ball 5 produce an axial displacement, make spring 4 be compressed a corresponding displacement again, thereby the spring force that produces acted on two fins 7 again.When the external torque that applies disappears, two fins 7 are just under the effect of spring force and be expanded to extreme position automatically.During installation, earlier the bull stick of wing arbor 1 with the blocking rotary type charge level controller joined by pin-and-hole 2, with hand two fins 7 are closed up foldedly and together again, just launch automatically after making it pass threaded hole on the storage bin container sidewall, threaded connector is tightened got final product then.During dismounting, unclamp threaded connector after, as long as slightly firmly can make it withdraw from threaded hole outward once drawing.
The utility model is on probation in Liaoning Province Liaoyang Automatic Instrument Metre Factory, and effect is very good.

Claims (1)

  1. A kind of gyrodamping fin that can launch automatically is made of wing arbor (1), pin-and-hole (2), plug (3), spring (4), steel ball (5), pin (6), fin (7), it is characterized in that:
    1, wing arbor (1) is hollow, the flat fork of groove milling in the middle of the one end is provided with, flat stick adorning two with two pins (6) can rotating fin (7);
    2, at the other end the inside of wing arbor (1) car screw thread is arranged, also be provided with pin-and-hole (2) on the wing arbor (1);
    3, in wing arbor (1) hollow, steel ball (5), spring (4) and plug (3) are housed;
    4, an end of fin (7) is circular-arc.
CN 89209750 1989-11-24 1989-11-24 Rotary damping wing panel with the function of automatic developing Expired - Lifetime CN2060905U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 89209750 CN2060905U (en) 1989-11-24 1989-11-24 Rotary damping wing panel with the function of automatic developing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 89209750 CN2060905U (en) 1989-11-24 1989-11-24 Rotary damping wing panel with the function of automatic developing

Publications (1)

Publication Number Publication Date
CN2060905U true CN2060905U (en) 1990-08-22

Family

ID=4866260

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 89209750 Expired - Lifetime CN2060905U (en) 1989-11-24 1989-11-24 Rotary damping wing panel with the function of automatic developing

Country Status (1)

Country Link
CN (1) CN2060905U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103207627B (en) * 2012-01-16 2016-06-08 中国科学院工程热物理研究所 A kind of high temperature resistant clog-proof rotation stuff level switch

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103207627B (en) * 2012-01-16 2016-06-08 中国科学院工程热物理研究所 A kind of high temperature resistant clog-proof rotation stuff level switch

Similar Documents

Publication Publication Date Title
CN110411287B (en) Spiral sunken wing folding and unfolding mechanism
CN109737128A (en) Antitheft tightening assembly and removal tool special
CN2060905U (en) Rotary damping wing panel with the function of automatic developing
CN109624780A (en) One kind changing motor structure and electric car
CN210833270U (en) Synchronous transverse unfolding locking mechanism for submerged folding wings
CN110566606B (en) Speed reduction device for rotating part
CN204961802U (en) Electric automobile derailleur and parking mechanism thereof
CN201621216U (en) Spring-force driven dual-drum driving device with low driving speed
CN204431149U (en) Manual single floating cam torque screwdriver
CN205542968U (en) On -vehicle battery lock tightly installs
CN111319671A (en) Dislocation type connecting device for connecting steering wheel and shaft body for automobile
CN202878267U (en) Rotating type tool and fast installation chuck thereof
CN210137241U (en) Oil extraction pumping unit motor fixing device
CN207634509U (en) Outspreading sailboard of solar cell detent mechanism
CN112647788A (en) Novel electric parking door hinge
CN220322215U (en) Yin-yang angle square for constructional engineering
CN216078315U (en) Novel gas receiver test connector
CN111946404A (en) Gas-liquid driving type large-scale rotating device
CN205915912U (en) Vehicle suspension and leaf spring sells axle thereof
CN220356283U (en) Spherical shell plate curvature verification device
CN110620302B (en) Charging electrode structure of electric automobile
CN221097141U (en) Novel bolt head bolt
CN220540092U (en) Gear shaft with low oil consumption and stable connection
CN204302102U (en) Propellant powder determiner for compression strength
CN216077919U (en) Expansion type high-strength bolt fastener

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C14 Grant of patent or utility model
GR01 Patent grant
C17 Cessation of patent right
CX01 Expiry of patent term