CN210027882U - Variable pitch propeller blade and propeller hub connecting device - Google Patents

Variable pitch propeller blade and propeller hub connecting device Download PDF

Info

Publication number
CN210027882U
CN210027882U CN201920743779.4U CN201920743779U CN210027882U CN 210027882 U CN210027882 U CN 210027882U CN 201920743779 U CN201920743779 U CN 201920743779U CN 210027882 U CN210027882 U CN 210027882U
Authority
CN
China
Prior art keywords
lasso
ferrule
paddle
neck
sleeve pipe
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
CN201920743779.4U
Other languages
Chinese (zh)
Inventor
南雍
潘新旗
李海山
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.)
Anhui Thatcher Aviation Technology Co Ltd
Original Assignee
Anhui Thatcher Aviation Technology Co Ltd
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 Anhui Thatcher Aviation Technology Co Ltd filed Critical Anhui Thatcher Aviation Technology Co Ltd
Priority to CN201920743779.4U priority Critical patent/CN210027882U/en
Application granted granted Critical
Publication of CN210027882U publication Critical patent/CN210027882U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Bridges Or Land Bridges (AREA)

Abstract

The utility model discloses a variable pitch propeller paddle and propeller hub connecting device, include: the paddle passes through coupling assembling and is connected with the propeller hub, and the blade root end of paddle includes the neck and is located the spacing pier nose of neck end department, and the propeller hub includes the lasso, and coupling assembling includes adjustment sleeve pipe and fastening nut, wherein: a limiting retainer ring integrally formed with the ferrule is arranged in the ferrule and between the two ends of the ferrule; the periphery of one end of the ferrule is provided with an external thread; the outer diameter of the adjusting sleeve is sequentially increased from one end to the other end; under the installation state, the neck at the paddle is cased to the adjustment sleeve pipe, and the path end of adjustment sleeve pipe is towards spacing mound head, and spacing mound head is held by the external screw thread place of lasso and is stretched into in the lasso and support and lean on with spacing retaining ring, and the adjustment sleeve pipe supports with the inner wall of lasso and supports and lean on, and fastening nut suit is in the outside of lasso and with the external screw thread threaded connection on the lasso. The utility model discloses can effectively improve fastness and the reliability that paddle and propeller hub are connected.

Description

Variable pitch propeller blade and propeller hub connecting device
Technical Field
The utility model relates to an aeronautical equipment technical field especially relates to a variable pitch propeller paddle and propeller hub connecting device.
Background
As an important component of an aircraft, propellers are subjected to vibratory stresses from the engine and the air flow during operation, as well as to high bending stresses and great centrifugal stresses, which are complex and great stresses that cause the propeller system to operate at all times with the risk that mechanical failure may lead to a force landing or to violent vibrations sufficient to damage the aircraft. At present, however, most of the propellers and the propeller hub in the market are connected only by means of compression friction, and the blades are mostly of carbon fiber structures, the forming dimensional tolerance of the blades cannot be as precise as that of metal, the propellers bear vibration stress from an engine and airflow during the operation, and simultaneously bear high bending stress and huge centrifugal stress, and the complex and huge stress causes the propeller system to always have risks during the operation, the safety and the reliability of the propellers are reduced, and even safety accidents are caused.
SUMMERY OF THE UTILITY MODEL
Based on the technical problem that exists among the above-mentioned background art, the utility model provides a variable pitch propeller paddle and propeller hub connecting device.
The utility model provides a pair of displacement propeller paddle and propeller hub connecting device, include: the paddle passes through coupling assembling and is connected with the propeller hub, the blade root end of paddle includes the neck and is located the spacing pier nose of neck end department, the propeller hub includes the lasso, coupling assembling is including adjusting sleeve pipe and fastening nut, wherein:
a limiting retainer ring integrally formed with the ferrule is arranged in the ferrule and between the two ends of the ferrule; the periphery of one end of the ferrule is provided with an external thread; the outer diameter of the adjusting sleeve is sequentially increased from one end to the other end; under the installation state, the neck at the paddle is cased to the adjustment sleeve pipe, and the path end of adjustment sleeve pipe is towards spacing mound head, and spacing mound head is held by the external screw thread place of lasso and is stretched into in the lasso and support and lean on with spacing retaining ring, and the adjustment sleeve pipe supports with the inner wall of lasso and supports and lean on, and fastening nut suit is in the outside of lasso and with the external screw thread threaded connection on the lasso.
Preferably, the ferrule is provided with at least two cutting grooves axially extending from one end close to the external thread to one end far away from the external thread, and the cutting grooves are uniformly distributed around the circumference of the ferrule.
Preferably, the port edge of fastening nut one end is equipped with the thrust retaining ring of turning over to its inboard, and under the installation condition, the one end that the adjustment sleeve pipe kept away from spacing pier nose leans on with the thrust retaining ring.
Preferably, the outer edge of the large-diameter end of the adjusting sleeve is provided with a flanging.
Preferably, the limiting pier head and the neck are in smooth transition.
The utility model discloses in, through setting up the adjusting sleeve at the paddle neck to the dimensional tolerance who utilizes adjusting sleeve's tapering change adjusting paddle neck, and it is fixed with paddle and lasso locking to utilize fastening nut, thereby realizes that the paddle is fixed with the propeller hub, and this connected mode can effectively improve the fastness and the reliability that paddle and propeller hub are connected.
Drawings
Fig. 1 is a schematic structural view of a connecting device for a variable pitch propeller blade and a hub according to the present invention.
Detailed Description
The technical solution of the present invention will be described in detail by the following embodiments.
As shown in fig. 1, fig. 1 is a schematic structural diagram of a device for connecting a variable pitch propeller blade and a hub according to the present invention.
Referring to fig. 1, the utility model provides a variable pitch propeller blade and propeller hub connecting device, include: the paddle 1 is connected with the propeller hub through the connecting assembly, the blade root end of the paddle 1 comprises a neck and a limiting pier head located at the end of the neck, and the limiting pier head and the neck are in smooth transition. The hub comprises a ferrule 2, the connection assembly comprising an adjustment sleeve 3 and a fastening nut 4, wherein: a limiting retainer ring 21 which is integrally formed with the ferrule 2 is arranged in the ferrule 2 and between the two ends of the ferrule; the periphery of one end of the ferrule 2 is provided with an external thread; the outer diameter of the adjusting sleeve 3 is sequentially increased from one end to the other end; under the installation state, adjustment sleeve 3 suit is at the neck of paddle 1, and adjustment sleeve 3's minor diameter end (the minimum one end of suit sleeve 3 external diameter promptly) is towards spacing pier nose, and spacing pier nose is held by the external screw thread of lasso 2 and is stretched into in the lasso 2 and lean on with spacing retaining ring 21, and adjustment sleeve 3 supports with the inner wall of lasso 2 and supports, and fastening nut 4 suit is in the outside of lasso 2 and with the external screw thread threaded connection on the lasso 2.
By the way, the utility model discloses a set up adjusting sleeve 3 at 1 neck of paddle to the dimensional tolerance of 1 neck of tapering change adjustment paddle that utilizes adjusting sleeve 3, and utilize fastening nut 4 fixed with paddle 1 and 2 locks of lasso, thereby realize that paddle 1 is fixed with the propeller hub, and this connected mode can effectively improve the fastness and the reliability that paddle 1 and propeller hub are connected.
In addition, in this embodiment, the ferrule 2 is provided with at least two cutting grooves extending axially from one end close to the external thread to one end far away from the external thread, the cutting grooves are uniformly distributed around the circumference of the ferrule 2, and the arrangement of the structure enables the inner diameter of the end where the external thread of the ferrule 2 is located to have a movable deformation space, so that connection is facilitated and the connection firmness is further improved.
In this embodiment, the port edge of one end of the fastening nut 4 is provided with the thrust retaining ring 41 which is turned over towards the inner side thereof, and in the installation state, one end of the adjusting sleeve 3, which is far away from the limiting pier head, abuts against the thrust retaining ring 41, so that the adjusting sleeve 3 is prevented from moving in the working process, and the stability of the sleeving sleeve 3 in the working process is ensured. And in order to further increase the contact area between the thrust retaining ring 41 and the adjusting sleeve 3, the embodiment is provided with a flanging at the outer edge of the large-diameter end of the adjusting sleeve 3.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.

Claims (5)

1. A variable pitch propeller blade and hub attachment apparatus comprising: blade (1) is connected with the propeller hub through coupling assembling, the blade root end of blade (1) includes the neck and is located the spacing pier nose of neck end department, the propeller hub includes lasso (2), coupling assembling is including adjusting sleeve pipe (3) and fastening nut (4), wherein:
a limiting retainer ring (21) which is integrally formed with the ferrule (2) is arranged in the ferrule and between the two ends of the ferrule; the periphery of one end of the ferrule (2) is provided with an external thread; the outer diameter of the adjusting sleeve (3) is sequentially increased from one end to the other end; under the installation state, adjustment sleeve pipe (3) suit is at the neck of paddle (1), and the path end of adjustment sleeve pipe (3) is towards spacing pier nose, and spacing pier nose is held by the external screw thread of lasso (2) and is stretched into in lasso (2) and support with spacing retaining ring (21) and lean on, and adjustment sleeve pipe (3) support with the inner wall of lasso (2) and support and lean on, and fastening nut (4) suit is in the outside of lasso (2) and with the external screw thread threaded connection on lasso (2).
2. A pitch propeller blade to hub connection according to claim 1, wherein the collar (2) is provided with at least two slots extending axially from an end close to its external thread to an end remote from the external thread, each slot being circumferentially distributed around the collar (2).
3. The device for connecting the blades and the hub of the variable pitch propeller according to claim 1, wherein a thrust retaining ring (41) which is turned over towards the inner side of the fastening nut (4) is arranged at the port edge of one end of the fastening nut, and in the installation state, one end of the adjusting sleeve (3) far away from the limiting pier head abuts against the thrust retaining ring (41).
4. A variable pitch propeller blade to hub connection as claimed in claim 3 wherein the adjustment sleeve (3) is provided with a flange at the outer rim of the large diameter end.
5. The variable pitch propeller blade to hub connection as recited in any one of claims 1 to 4, wherein the limiting pier head smoothly transitions into the neck.
CN201920743779.4U 2019-05-22 2019-05-22 Variable pitch propeller blade and propeller hub connecting device Active CN210027882U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201920743779.4U CN210027882U (en) 2019-05-22 2019-05-22 Variable pitch propeller blade and propeller hub connecting device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201920743779.4U CN210027882U (en) 2019-05-22 2019-05-22 Variable pitch propeller blade and propeller hub connecting device

Publications (1)

Publication Number Publication Date
CN210027882U true CN210027882U (en) 2020-02-07

Family

ID=69367245

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201920743779.4U Active CN210027882U (en) 2019-05-22 2019-05-22 Variable pitch propeller blade and propeller hub connecting device

Country Status (1)

Country Link
CN (1) CN210027882U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110127036A (en) * 2019-05-22 2019-08-16 安徽卓尔航空科技有限公司 A kind of variable-pitch propeller blade and propeller hub attachment device
CN112937837A (en) * 2021-02-05 2021-06-11 安徽羲禾航空科技有限公司 Variable pitch propeller

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110127036A (en) * 2019-05-22 2019-08-16 安徽卓尔航空科技有限公司 A kind of variable-pitch propeller blade and propeller hub attachment device
CN112937837A (en) * 2021-02-05 2021-06-11 安徽羲禾航空科技有限公司 Variable pitch propeller
CN112937837B (en) * 2021-02-05 2024-01-05 安徽羲禾航空科技有限公司 Pitch-variable propeller

Similar Documents

Publication Publication Date Title
CN210027882U (en) Variable pitch propeller blade and propeller hub connecting device
JP4648645B2 (en) Method and apparatus for mounting a gas turbine engine
US11851157B2 (en) Aircraft turbine engine comprising variable-pitch propeller blades
EP3069989B1 (en) Lightweight propeller blade with improved retention capacity
US10507904B2 (en) Snap fit nose cone assembly
US10352238B2 (en) Nose cone assembly without fasteners
US9938000B2 (en) Air propeller blade pivot in the shape of a spherical cap
US10717516B2 (en) Composite propulsor blade support structure and system
US11161598B2 (en) Transfer bearing collapsing device
US9963237B2 (en) Latch hooks, latch housings, and latch assemblies
EP4083434A1 (en) Cabin air compressor shaft and tie rod support
RU2682206C2 (en) Isostatic suspension of a turbojet by rear double support
EP3318737A1 (en) Low weight nose cone assembly
US10132241B2 (en) Method of producing suspension for a structure in a turbojet engine using a hyperstatic trellis with pre-stressed link elements
EP4086179A1 (en) Nacelle inlet structures, engine assemblies and vehicles including the same, and related methods
CN110127036A (en) A kind of variable-pitch propeller blade and propeller hub attachment device
US11077954B2 (en) Connection assembly for mounting engine and engine mounting system comprising the same
US11572889B2 (en) Blade pivot of adjustable orientation and of reduced bulk for a turbomachine fan hub
US11993365B2 (en) Aircraft turbine engine comprising variable-pitch propeller blades
US10583913B2 (en) Stud push out mount for a turbine engine spinner assembly having a spinner push out stud joint connecting through a counterbore of a spinner bolt hole
CN210034116U (en) D-head bolt and aircraft engine
US11440670B2 (en) Suspension device
CN111361732A (en) Main rotor hub overall design of unmanned helicopter
CN221541989U (en) Supporting structure of unmanned aerial vehicle kuppe
CN209305820U (en) High temperature heat dissipation unmanned plane propeller

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant