CN204300281U - A kind of gear crack-stop structure - Google Patents

A kind of gear crack-stop structure Download PDF

Info

Publication number
CN204300281U
CN204300281U CN201420684873.4U CN201420684873U CN204300281U CN 204300281 U CN204300281 U CN 204300281U CN 201420684873 U CN201420684873 U CN 201420684873U CN 204300281 U CN204300281 U CN 204300281U
Authority
CN
China
Prior art keywords
gear
piece
gear piece
crack
mechanical
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.)
Active
Application number
CN201420684873.4U
Other languages
Chinese (zh)
Inventor
刘莹莹
刘向
董林渊
姚成法
任鹏杰
田磊
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.)
No 618 Research Institute of China Aviation Industry
Original Assignee
No 618 Research Institute of China Aviation Industry
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 No 618 Research Institute of China Aviation Industry filed Critical No 618 Research Institute of China Aviation Industry
Priority to CN201420684873.4U priority Critical patent/CN204300281U/en
Application granted granted Critical
Publication of CN204300281U publication Critical patent/CN204300281U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Gears, Cams (AREA)

Abstract

The utility model belongs to mechanical designing technique, relates to a kind of gear crack-stop structure.It comprises the first gear piece (1), gear piece (2), gear (3).It is characterized in that, first gear piece (1) with identical parameters is connected by certain Placement with gear piece (2), forms a driving gear; Gear (3) comprises the identical gear piece of two panels parameter; First gear piece (1) and gear piece (2) engage with two gear pieces of gear (3) respectively, form driving mechanism.The utility model is in mechanical transmission, driving gear crackle causes gear capacity to decline, gear life is caused sharply to decline, even there is the fault mode that gear breaking, transmission system are stuck, a kind of mechanical structure form preventing gear crack from spreading is proposed, realize the design of transmission system mechanical redundancy, reduce transmission system mission failure rate, improve auxiliary products reliability.

Description

A kind of gear crack-stop structure
Technical field
The utility model belongs to mechanical designing technique, relates to a kind of gear crack-stop structure.
Background technique
At present, aircraft rudder surface actuator adopts hydraulic product mostly, but along with the development of electric aircraft, electronic product replaces hydraulic product to become trend.Solve the mechanical remaining problem of electronic product transmission part, improve reliable transmission, thus improve mission reliability, ensure flight safety, become electronic product and replaced one of bottleneck of hydraulic product operating aircraft main rudder face development.
Model utility content
The purpose of this utility model is: propose a kind of gear crack-stop structure, realizes the design of transmission system mechanical redundancy, reduces transmission system mission failure rate, improve auxiliary products reliability.
The technical solution of the utility model is: a kind of gear crack-stop structure, comprises the first gear piece 1, gear piece 2, gear 3, and first gear piece 1 with identical gear parameter is connected with gear piece 2, forms a driving gear; Gear 3 is also driving gear, comprises the gear piece of the identical gear parameter of two panels; First gear piece 1 and gear piece 2 engage with two gear pieces of gear 3 respectively, form driving mechanism.
Preferably, between the first gear piece 1, gear piece 2, and be separated type between gear 3 two panels gear piece, adopt spline or bolt mode to connect.
Preferably, gear 3 two panels gear piece is formed in one.
The utility model has the advantages that: the utility model, by each driving gear is designed to two panels toothing, realizes the mechanical redundancy design of transmission system, improves reliable transmission, thus improve mission reliability, promote flight safety further.Often organize driving gear and be two redundancy design, realize a slice gear crack, do not affect whole transmission system reliable operation.
Accompanying drawing explanation
Fig. 1 is the front view of the utility model structure;
Fig. 2 is the sectional view in the utility model structure A-A face.
Embodiment
Below the utility model is described in further details.
See Fig. 1 and Fig. 2, a kind of gear crack-stop structure, comprises the first gear piece 1, gear piece 2, gear 3, and first gear piece 1 with identical gear parameter is connected with gear piece 2, forms a driving gear; Gear 3 is also driving gear, comprises the gear piece of the identical gear parameter of two panels; First gear piece 1 and gear piece 2 engage with two gear pieces of gear 3 respectively, form driving mechanism.
Between first gear piece 1, gear piece 2, and be separated type between gear 3 two panels gear piece, adopt spline or bolt mode to connect.
In addition, the two panels gear piece of gear 3 also can be designed as one-body molded.
The utility model is often organized driving gear and is two redundancy design, realizes a slice gear crack, does not affect whole transmission system reliable operation.

Claims (3)

1. a gear crack-stop structure, comprise the first gear piece (1), gear piece (2), gear (3), it is characterized in that, first gear piece (1) with identical gear parameter is connected with gear piece (2), forms a driving gear; Gear (3) is also driving gear, comprises the gear piece of the identical gear parameter of two panels; First gear piece (1) and gear piece (2) engage with two gear pieces of gear (3) respectively, form driving mechanism.
2. gear crack-stop structure according to claim 1, is characterized in that: between the first gear piece (1), gear piece (2), and is separated type between gear (3) two panels gear piece, adopts spline or bolt mode to connect.
3. gear crack-stop structure according to claim 1, is characterized in that: gear (3) two panels gear piece is formed in one.
CN201420684873.4U 2014-11-14 2014-11-14 A kind of gear crack-stop structure Active CN204300281U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420684873.4U CN204300281U (en) 2014-11-14 2014-11-14 A kind of gear crack-stop structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420684873.4U CN204300281U (en) 2014-11-14 2014-11-14 A kind of gear crack-stop structure

Publications (1)

Publication Number Publication Date
CN204300281U true CN204300281U (en) 2015-04-29

Family

ID=53105822

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201420684873.4U Active CN204300281U (en) 2014-11-14 2014-11-14 A kind of gear crack-stop structure

Country Status (1)

Country Link
CN (1) CN204300281U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3324078A1 (en) * 2016-11-21 2018-05-23 Ratier-Figeac SAS Gearbox assembly

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3324078A1 (en) * 2016-11-21 2018-05-23 Ratier-Figeac SAS Gearbox assembly
US10759518B2 (en) 2016-11-21 2020-09-01 Ratier-Figeac Sas Gearbox assembly

Similar Documents

Publication Publication Date Title
WO2010134921A8 (en) Differential pitch control to optimize co-rotating stacked rotor performance
CN204300281U (en) A kind of gear crack-stop structure
CN102543503B (en) Electromagnetic clutch for electric on/off operating mechanism of electric switch
CN204279926U (en) A kind of Brattice type multi-rotor aerocraft alighting gear with guide functions
CN202394737U (en) Electromagnetic clutch for electrical switching on/off operation mechanism of electric switch
CN203602304U (en) Safety brake
CN204140681U (en) A kind of large model membranous disc connecting structure
CN204677692U (en) A kind of worm gear structure
CN102374320A (en) Dual-purpose cutoff valve
CN203998877U (en) A kind of permanent moment of torsion plane Cao rotating head mechanism
CN204403215U (en) A kind of friction plate structure
CN204724263U (en) The electronic slow transmission device of a kind of grinding machine
CN203808022U (en) Long-life gate hoist system
CN202690723U (en) Improved coal feeder crank
CN104315237A (en) Partially rotary type valve electric device
CN203161985U (en) Joint reducer with double input mechanisms
CN201539627U (en) Valve lever pin protection mechanism
CN203051454U (en) Splined shaft
CN205190645U (en) A gear reducer for mould conveyor
CN204201233U (en) A kind of metal link rod for the transmission of pumped storage power station position signal
CN204149847U (en) Tritruck engine installation structure
CN204372101U (en) A kind of main gear shaft assembly of high-efficient automatic twisted chain machine
CN204403119U (en) A kind of reinforcing type bar linkage structure
CN204403455U (en) Prevent cracking gas from returning the axial rotary safety check of gas
CN204155782U (en) Ring main unit motor-operating mechanism

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant