CN109616843A - A kind of collecting ring chocking construction - Google Patents
A kind of collecting ring chocking construction Download PDFInfo
- Publication number
- CN109616843A CN109616843A CN201811492157.5A CN201811492157A CN109616843A CN 109616843 A CN109616843 A CN 109616843A CN 201811492157 A CN201811492157 A CN 201811492157A CN 109616843 A CN109616843 A CN 109616843A
- Authority
- CN
- China
- Prior art keywords
- collecting ring
- chocking construction
- sleeve
- vertical tube
- helicopter
- 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.)
- Pending
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Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R39/00—Rotary current collectors, distributors or interrupters
- H01R39/02—Details for dynamo electric machines
- H01R39/14—Fastenings of commutators or slip-rings to shafts
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- Toys (AREA)
Abstract
The invention belongs to helicopter design fields, and in particular to a kind of collecting ring chocking construction.For the fixed part of collecting ring, stopping effect and persistence are often not satisfactory the prior art.The present invention provides a kind of collecting ring chocking construction, prevent the conducting ring assemblies of collecting ring from rotating with Helicopter Main blade, in vertical tube on the sleeve insertion helicopter hanger disk of the collecting ring, the chocking construction has been arranged radially backing pin on sleeve, L-shaped groove is provided on the tube wall of vertical tube, after the shelves pin enters axially into the L-shaped groove, in blade rotation, the sleeve is by circumferential stop.Using collecting ring chocking construction of the invention, the conducting ring assemblies of collecting ring can be effectively prevent to rotate with Helicopter Main blade under the premise of not increasing volume.The present invention, which breaks the prior art, has thinking in the used of the field, plays excellent results beyond expection.
Description
Technical field
The invention belongs to helicopter design fields, and in particular to a kind of collecting ring chocking construction.
Background technique
To meet requirement of the helicopter under natural freezing environment, electric heating rotor need to be installed additional and prevent/deicing system, collection
Stream ring realizes the transmission of the power supply and signal from fixed position to rotation position, and chocking construction is to realize above-mentioned rotary transfer
Pith.For the fixed part of collecting ring, stopping effect and persistence are often not satisfactory the prior art.
Summary of the invention
The object of the present invention is to provide a kind of collecting ring chocking constructions, prevent the conducting ring assemblies of collecting ring with helicopter
Main blade rotates together, passes through the transmission of power supply and signal on the rotation realization machine of conducting ring assemblies and brush assembly of electric.
The technical scheme is that a kind of collecting ring chocking construction, the sleeve of the collecting ring is inserted into helicopter hanger
In vertical tube on disk, which has been arranged radially backing pin on sleeve, is provided with L-shaped groove on the tube wall of vertical tube, works as institute
It states after shelves pin enters axially into the L-shaped groove, in blade rotation, the sleeve is by circumferential stop.
The backing pin and sleeve connect in such a way that threaded connection and flaring riveting are combined.
The L-shaped groove has certain longitudinal depth, overcomes the assembly problem as caused by manufacturing tolerance.
When disk is hung in disassembly, vertical tube is limited by the backing pin on sleeve.
The invention has the advantages that backing pin is stuck in the L-shaped groove of riser upper end using collecting ring chocking construction of the invention,
It plays the role of stopper, the conducting ring assemblies of collecting ring can be effectively prevent with Helicopter Main blade under the premise of not increasing volume
It rotates together.The present invention, which breaks the prior art, has thinking in the used of the field, plays excellent results beyond expection.
Detailed description of the invention
Fig. 1 is the assembling schematic diagram of collecting ring chocking construction of the present invention;
Fig. 2 is the chocking construction enlarged drawing of Fig. 1;
Fig. 3 is the L-shaped groove schematic diagram on vertical tube.
Specific embodiment
The present invention is described in further details below.
With reference to FIG. 1 to FIG. 3.The sleeve 3 of collecting ring 4 is inserted into the vertical tube 1 on helicopter hanger disk, which is covering
It has been arranged radially backing pin 2 on cylinder 3, L-shaped groove is provided on the tube wall of vertical tube 1, after the shelves pin 2 enters axially into the L-shaped groove,
When blade rotation, the sleeve 3 of collecting ring 4 is by circumferential stop.
The backing pin 2 and sleeve 3 connect in such a way that threaded connection and flaring riveting are combined, and play the role of stopper, prevent
The conducting ring assemblies of collecting ring are rotated with Helicopter Main blade.
When work, conducting ring assemblies keep opposing stationary, brush assembly of electric with main reducing gear central axis by backing pin and vertical tube
It is fixed in rectification cover support members with outer cover etc. and is rotated with Helicopter Main blade.Pass through conducting ring assemblies and brush assembly of electric
Rotation realization machine on power supply and signal transmission.
Claims (4)
1. the sleeve (3) of a kind of collecting ring chocking construction, the collecting ring (4) is inserted into the vertical tube (1) on helicopter hanger disk,
It is characterized by: the chocking construction has been arranged radially backing pin (2) on sleeve (3), L shape is provided on the tube wall of vertical tube (1)
Slot, after the shelves pin (2) enters axially into the L-shaped groove, in blade rotation, the sleeve (3) is by circumferential stop.
2. collecting ring chocking construction according to claim 1, it is characterised in that: the backing pin (2) and sleeve (3) use spiral shell
The mode that line connection is combined with flaring riveting connects.
3. collecting ring chocking construction according to claim 1, it is characterised in that: the L-shaped groove has certain longitudinal direction deep
Degree, overcomes the assembly problem as caused by manufacturing tolerance.
4. collecting ring chocking construction according to claim 1, it is characterised in that: when disk is hung in disassembly, pass through sleeve (3)
On backing pin (2) vertical tube (1) is limited.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201811492157.5A CN109616843A (en) | 2018-12-07 | 2018-12-07 | A kind of collecting ring chocking construction |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201811492157.5A CN109616843A (en) | 2018-12-07 | 2018-12-07 | A kind of collecting ring chocking construction |
Publications (1)
Publication Number | Publication Date |
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CN109616843A true CN109616843A (en) | 2019-04-12 |
Family
ID=66008515
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201811492157.5A Pending CN109616843A (en) | 2018-12-07 | 2018-12-07 | A kind of collecting ring chocking construction |
Country Status (1)
Country | Link |
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CN (1) | CN109616843A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112896523A (en) * | 2020-12-25 | 2021-06-04 | 武汉航空仪表有限责任公司 | Main paddle collecting ring assembly and debugging method |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1127388B1 (en) * | 1999-08-27 | 2002-10-16 | Amphenol Corporation | Self-locking bayonet coupling mechanism |
CN202977356U (en) * | 2009-10-12 | 2013-06-05 | 珀金埃尔默健康科技有限公司 | Source module, mass spectrometer and instrument including the mass spectrometer, and end lens and complete equipment including the end lens |
CN203660172U (en) * | 2013-12-16 | 2014-06-18 | 浙江中杭电子有限公司 | Rapid self-locking pin-hole assembly |
CN107892012A (en) * | 2017-11-14 | 2018-04-10 | 农业部南京农业机械化研究所 | A kind of and supporting horizontal adhesive tape deployment mechanism of screw compressor |
CN108649386A (en) * | 2018-06-01 | 2018-10-12 | 广东广航科技有限公司 | Conductive connecting device |
-
2018
- 2018-12-07 CN CN201811492157.5A patent/CN109616843A/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1127388B1 (en) * | 1999-08-27 | 2002-10-16 | Amphenol Corporation | Self-locking bayonet coupling mechanism |
CN202977356U (en) * | 2009-10-12 | 2013-06-05 | 珀金埃尔默健康科技有限公司 | Source module, mass spectrometer and instrument including the mass spectrometer, and end lens and complete equipment including the end lens |
CN203660172U (en) * | 2013-12-16 | 2014-06-18 | 浙江中杭电子有限公司 | Rapid self-locking pin-hole assembly |
CN107892012A (en) * | 2017-11-14 | 2018-04-10 | 农业部南京农业机械化研究所 | A kind of and supporting horizontal adhesive tape deployment mechanism of screw compressor |
CN108649386A (en) * | 2018-06-01 | 2018-10-12 | 广东广航科技有限公司 | Conductive connecting device |
Non-Patent Citations (1)
Title |
---|
吴文涛 等: "直升机旋翼防除冰集流环设计", 《直升机技术》 * |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112896523A (en) * | 2020-12-25 | 2021-06-04 | 武汉航空仪表有限责任公司 | Main paddle collecting ring assembly and debugging method |
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Legal Events
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PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
RJ01 | Rejection of invention patent application after publication | ||
RJ01 | Rejection of invention patent application after publication |
Application publication date: 20190412 |