CN112713475A - Helicopter collector ring cable assembly - Google Patents
Helicopter collector ring cable assembly Download PDFInfo
- Publication number
- CN112713475A CN112713475A CN202011490446.9A CN202011490446A CN112713475A CN 112713475 A CN112713475 A CN 112713475A CN 202011490446 A CN202011490446 A CN 202011490446A CN 112713475 A CN112713475 A CN 112713475A
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- CN
- China
- Prior art keywords
- sheath
- helicopter
- cable assembly
- diameter
- variable
- 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
Links
- 239000000853 adhesive Substances 0.000 claims abstract description 5
- 230000001070 adhesive effect Effects 0.000 claims abstract description 5
- 238000005452 bending Methods 0.000 claims description 7
- 210000001503 joint Anatomy 0.000 claims description 6
- 238000009434 installation Methods 0.000 claims description 5
- 239000002131 composite material Substances 0.000 claims description 3
- 239000003292 glue Substances 0.000 claims description 3
- 239000002184 metal Substances 0.000 claims description 3
- 239000004033 plastic Substances 0.000 claims description 3
- 239000011248 coating agent Substances 0.000 claims 1
- 238000000576 coating method Methods 0.000 claims 1
- 230000002265 prevention Effects 0.000 abstract description 2
- 238000005299 abrasion Methods 0.000 description 8
- 239000004020 conductor Substances 0.000 description 2
- 206010066054 Dysmorphism Diseases 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 238000006748 scratching Methods 0.000 description 1
- 230000002393 scratching effect Effects 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Images
Classifications
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R31/00—Coupling parts supported only by co-operation with counterpart
- H01R31/06—Intermediate parts for linking two coupling parts, e.g. adapter
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/12—De-icing or preventing icing on exterior surfaces of aircraft by electric heating
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
- H01R13/46—Bases; Cases
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Details Of Connecting Devices For Male And Female Coupling (AREA)
Abstract
The invention belongs to the technical field of helicopter rotor deicing prevention and particularly relates to a helicopter collector ring cable assembly. The end part of a collecting ring cable assembly of the helicopter adopts a connecting structure of a plug (1) and a tail accessory (2), wherein the plug (1) at the far end of the cable assembly is connected with a blade, the plug (1) at the near end of the cable assembly is connected with equipment and rotates along with the blade, an adhesive (6) is coated inside the tail accessory to bond a lead (4), a sheath (3) is sleeved outside the lead (4), two ends of the sheath are sleeved on the tail accessory (2) and fixed through clamping wires (5), and the sheath is a variable-diameter sheath. The invention can reliably transmit power and signals under the working condition of rotating along with the paddle, and has the characteristics of simple structure, good manual assembly, high cable reliability and independent replacement.
Description
The technical field is as follows: the invention belongs to the technical field of helicopter rotor deicing prevention and relates to a helicopter collector ring cable assembly.
Background art: because the collecting ring cable works along with the rotation of the helicopter blades, the collecting ring cable for transmitting the power and signals of the blades is obviously subjected to centrifugal action, and the abrasion problem easily occurs to each layer structure of the cable after the collecting ring cable is used for a period of time. In addition, in order to adapt to the variable pitch of the blade, a free movable section is reserved on the cable, so that the cable is not conveniently and completely fixed on the blade structure, the service environment of the cable is severe, and the problem of cable abrasion is more prominent. In order to ensure the reliability of long-term use, a suitable cable structure needs to be designed.
The invention content is as follows:
the purpose of the invention is as follows: in view of the above-mentioned state of the art, it is an object of the present invention to provide a helicopter slip ring cable assembly that solves the problem of the cable being prone to wear when working with the rotation of the blade.
The above object of the present invention is achieved by the following technical solutions:
the end of the helicopter collector ring cable assembly is in a structure that a plug 1 and a tail accessory 2 are connected, wherein the plug 1 at the far end of the cable assembly is connected with a blade, the plug 1 at the near end of the cable assembly is connected with equipment and rotates along with the blade, an adhesive 6 is coated inside the tail accessory to bond a lead 4, the outer part of the lead 4 is sleeved with a sheath 3, two ends of the sheath are sleeved on the tail accessory 2 and fixed through a clamping wire 5, and the sheath is a variable-diameter sheath.
The diameter-variable sheath is thick at two ends and thin in the middle, wherein the end part is thick, so that stress can be well released at the joint of the diameter-variable sheath and the plug, abrasion is reduced, the middle part is thin, the weight of the diameter-variable sheath is small, and the centrifugal force of the cable can be effectively reduced.
The variable-diameter sheath 3 is of a special-shaped structure, the two ends of the variable-diameter sheath are of circular structures, the middle of the variable-diameter sheath is of a flat structure, and free moving sections are reserved in the variable-diameter sheath, so that the variable-diameter sheath can adapt to blade variable distances, cables are suitable for severe applicable environments, and the problem of abrasion of few cables is solved.
The bending angle of the variable-diameter sheath after being installed is 90-140 degrees, and the variable-diameter sheath is of a flat structure, so that the bending resistance of the cable at the position can be effectively improved, and the cable is prevented from being abraded.
The proportion range of the thickness to the width of the flat body of the variable-diameter sheath is 1: 4-1: 2, so that the bending resistance can be effectively improved while the internal cable is effectively stored, the cable is protected, and abrasion is avoided.
The inner diameter of the variable-diameter sheath is smaller than that of the tail accessory, so that contact abrasion of a lead at a tail accessory leading-out end when the thick end is bent after the machine is installed can be effectively avoided.
The variable-diameter sheath is a rubber sleeve or a composite material sleeve or a plastic sleeve, and the clamping wires are round metal wires, so that the sheath is effectively fixed.
The wire is of an independent structure and is arranged in a bending mode, and the centrifugal force of the sheath can be effectively prevented from being transmitted to the wire.
Be provided with the encapsulating hole on the tail annex, this encapsulating hole is close to the plug and communicates inside cavity to it is fixed effectively to carry out the veneer to inside cable conductor, avoids inside too much inflow sheath simultaneously.
The tail accessory and the sheath are provided with annular groove structures for butt joint, and the internal thread structures for butt joint are arranged at the plug, so that the cable is integrally and effectively fixed, and the structural stability is guaranteed.
And a plurality of anti-loosening screws are arranged at the connecting end of the tail accessory and the plug.
The invention has the technical effects that: according to the invention, by adopting the design of the variable-diameter sheath on the cable, the protection performance of the cable can be effectively improved, so that the cable can reliably transmit power and signals under the working condition of rotating along with the paddle, and the cable has the characteristics of simple structure, good manual assembly, high reliability and independent replacement.
Description of the drawings:
fig. 1 is a schematic structural view of a cable assembly of the present invention.
Wherein: 1: plug, 2: tail accessory, 3: rubber sleeve, 4: wire, 5: wire, 6: adhesive, 7: and (6) filling glue holes.
The specific implementation mode is as follows:
the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Example 1:
a helicopter slip ring cable assembly characterized by: the end part adopts a plug 1 and tail accessory 2 connecting structure, wherein the plug 1 at the far end of the cable assembly is connected with the paddle, the plug 1 at the near end is connected with equipment, the plug rotates along with the paddle, an adhesive 6 is coated inside the tail accessory to be bonded with a wire 4, a sheath 3 is sleeved outside the wire 4, two ends of the sheath are sleeved on the tail accessory 2 and fixed through a clamping wire 5, and the sheath is a variable-diameter sheath.
The diameter-variable sheath 3 is thick at two ends and thin in the middle, the diameter of the end part is 36mm, and the diameter of the middle part is 24mm, so that the variable-pitch propeller blade can adapt to variable pitch, rotary work and abrasion are reduced.
The diameter-variable sheath 3 is a rubber sleeve or a composite material sleeve or a plastic sleeve.
The clamping wire 5 is a round metal wire made of 1Cr18Ni9Ti stainless steel and is reliably fixed without scratching the sheath.
The inner diameter of the variable-diameter sheath 3 is 10mm, the inner diameter of the tail accessory is 12mm, and contact abrasion between a wire of the cable at the bent position of the tail accessory and the tail accessory after the cable is installed can be effectively avoided.
The total number of the wires 4 is 6, the wires and the outer sheath are of independent structures and are arranged in a bending mode inside the outer sheath, and the centrifugal force of the sheath can be prevented from being transmitted to the wires.
The tail accessory and the sheath are provided with 1 annular groove structure for butt joint, and the tail accessory and the plug are provided with internal thread structures for butt joint.
The tail accessory is provided with a glue filling hole 7 close to the plug, and the inner cable conductor is glued and fixed, and excessive flowing into the sheath is avoided.
The end of the tail accessory 2 connected with the plug is provided with 3 anti-loosening screws, so that the tail accessory is prevented from loosening under the action of centrifugal force.
Through assembling cable one end earlier, carry out wire and plug connection, installation tail annex, encapsulating in proper order, install the sheath, then assemble the cable other end, carry out wire and plug connection, installation tail annex, installation sheath, encapsulating in proper order, can realize better manual assembly nature.
Both ends of the cable are plugs, so that the cable can be quickly detached from equipment and blades and can be independently replaced.
Example 2:
this embodiment is similar to embodiment 1, only oversheath dysmorphism structure is the cylinder structure for both ends, and the centre is the flat body structure, and wherein, the flat body structure of centre is located cable installation back bend angle and is 110 departments, and flat body structure thickness is 16mm, and the width is 38mm, consequently can effectively accomodate the cable wire simultaneously, the flat body structure of its broad can effectively improve the wear resistance of cable to adapt to different paddle displacement.
The foregoing is merely a detailed description of the embodiments of the present invention, and some of the conventional techniques are not detailed. The scope of the present invention is not limited thereto, and any changes or substitutions that can be easily made by those skilled in the art within the technical scope of the present invention will be covered by the scope of the present invention. The protection scope of the present invention shall be subject to the protection scope of the claims.
Claims (10)
1. A helicopter slip ring cable assembly characterized by: the tip adopts plug (1) and tail annex (2) connection structure, and wherein, plug (1) and the paddle of cable subassembly distal end are connected, and plug (1) and the equipment connection of near-end are rotatory along with the paddle, at inside coating adhesive (6) bonding wire (4) of tail annex, wire (4) outside suit sheath (3), the sheath both ends suit is on tail annex (2), and is fixed through card silk (5), just the sheath is the variable diameter sheath.
2. A helicopter slip ring cable assembly according to claim 1 wherein: the diameter-variable sheath (3) is thick at two ends and thin in the middle.
3. A helicopter slip ring cable assembly according to claim 1 wherein: the diameter-variable sheath (3) is of a special-shaped structure, two ends of the diameter-variable sheath are of circular structures, and the middle of the diameter-variable sheath is of a flat structure.
4. A helicopter slip ring cable assembly according to claim 3, wherein: the bending angle of the diameter-variable sheath (3) is 90-140 degrees after the installation is a flat structure.
5. A helicopter slip ring cable assembly according to claim 3, wherein: the ratio of the thickness to the width of the flat body of the variable-diameter sheath (3) is 1: 4-1: 2.
6. A helicopter slip ring cable assembly according to claim 5, wherein: the inner diameter of the variable-diameter sheath (3) is smaller than that of the tail accessory (2).
7. A helicopter slip ring cable assembly according to claim 6 wherein: the diameter-variable sheath (3) is a rubber sleeve or a composite material sleeve or a plastic sleeve, and the clamping wires are round metal wires.
8. A helicopter slip ring cable assembly according to claim 1 wherein: the lead (4) is of an independent structure and is arranged in a bending mode.
9. A helicopter slip ring cable assembly according to claim 1 wherein: and a glue filling hole (7) is formed in the tail accessory, is close to the plug and is communicated with the inner cavity.
10. A helicopter slip ring cable assembly according to claim 9 wherein: the tail accessory (2) and the sheath are provided with annular groove structures for butt joint, and the plug and the tail accessory are provided with internal thread structures for butt joint.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011490446.9A CN112713475A (en) | 2020-12-16 | 2020-12-16 | Helicopter collector ring cable assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011490446.9A CN112713475A (en) | 2020-12-16 | 2020-12-16 | Helicopter collector ring cable assembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112713475A true CN112713475A (en) | 2021-04-27 |
Family
ID=75543437
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011490446.9A Pending CN112713475A (en) | 2020-12-16 | 2020-12-16 | Helicopter collector ring cable assembly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112713475A (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1487937A (en) * | 1921-12-10 | 1924-03-25 | Iorne A Griffin | Extension cord |
| US4664459A (en) * | 1984-11-01 | 1987-05-12 | Raytheon Company | Noiseless solid conductor flexible cable |
| US20130183003A1 (en) * | 2012-01-18 | 2013-07-18 | Stillwater Trust | Pressure-Balanced Subsea Junction Box and Cable Termination Apparatus and Method |
| CN206849536U (en) * | 2017-04-10 | 2018-01-05 | 沈阳兴华航空电器有限责任公司 | A kind of aircraft nose wheel turning cable |
| CN207490192U (en) * | 2017-12-06 | 2018-06-12 | 四川永贵科技有限公司 | A kind of submersible watertight cable connector integrally vulcanized |
| CN109599217A (en) * | 2018-12-07 | 2019-04-09 | 武汉航空仪表有限责任公司 | One kind can the high-speed rotating construction of cable |
| CN208889347U (en) * | 2018-09-19 | 2019-05-21 | 沈阳兴华航空电器有限责任公司 | A kind of engine cable |
| CN110517815A (en) * | 2019-08-23 | 2019-11-29 | 沈阳兴华航空电器有限责任公司 | A kind of ship-borne engine lightweight cable of resistance to ocean structure |
-
2020
- 2020-12-16 CN CN202011490446.9A patent/CN112713475A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1487937A (en) * | 1921-12-10 | 1924-03-25 | Iorne A Griffin | Extension cord |
| US4664459A (en) * | 1984-11-01 | 1987-05-12 | Raytheon Company | Noiseless solid conductor flexible cable |
| US20130183003A1 (en) * | 2012-01-18 | 2013-07-18 | Stillwater Trust | Pressure-Balanced Subsea Junction Box and Cable Termination Apparatus and Method |
| CN206849536U (en) * | 2017-04-10 | 2018-01-05 | 沈阳兴华航空电器有限责任公司 | A kind of aircraft nose wheel turning cable |
| CN207490192U (en) * | 2017-12-06 | 2018-06-12 | 四川永贵科技有限公司 | A kind of submersible watertight cable connector integrally vulcanized |
| CN208889347U (en) * | 2018-09-19 | 2019-05-21 | 沈阳兴华航空电器有限责任公司 | A kind of engine cable |
| CN109599217A (en) * | 2018-12-07 | 2019-04-09 | 武汉航空仪表有限责任公司 | One kind can the high-speed rotating construction of cable |
| CN110517815A (en) * | 2019-08-23 | 2019-11-29 | 沈阳兴华航空电器有限责任公司 | A kind of ship-borne engine lightweight cable of resistance to ocean structure |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 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: 20210427 |