CN104062071A - Vertical gyroscope assembly static balance debugger - Google Patents

Vertical gyroscope assembly static balance debugger Download PDF

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Publication number
CN104062071A
CN104062071A CN201410297968.5A CN201410297968A CN104062071A CN 104062071 A CN104062071 A CN 104062071A CN 201410297968 A CN201410297968 A CN 201410297968A CN 104062071 A CN104062071 A CN 104062071A
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CN
China
Prior art keywords
inner seat
base
inside casing
debugger
vertical gyro
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Granted
Application number
CN201410297968.5A
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Chinese (zh)
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CN104062071B (en
Inventor
王成猛
仵杨
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Bedik Lingyun (Yichang) Aircraft Maintenance and Engineering Corporation
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Lingyun (yichang) Aircraft Maintenance And Engineering Corp
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Abstract

The invention discloses a vertical gyroscope assembly static balance debugger which comprises a base, a bearing bracket, an inner seat, an adjusting screw and an inner frame. The base is a hollow rectangular body formed by rectangular side plates and a rectangular baseplate. Two sides of the base are provided with supporting plates for fixing the bearing bracket. The inner frame is fixed on the inner seat through a screw. The inner frame and the inner seat are placed onto the bearing bracket through protruded shafts which are arranged on two sides of the top portion of the inner seat and sleeved with bearings to make the inner seat and the inner frame which are connected to each other can be subjected to 360-angle free rotation around the protruded shafts in the base to form a balanced structure. According to the vertical gyroscope assembly static balance debugger provided in the invention, the vertical gyroscope assembly is installed between the inner seat and the inner frame which can be subjected to 360-angle free rotation around the protruded shafts, and the installation position of a gyroscope on the vertical gyroscope assembly is adjusted by adjusting the groove on the gyroscope shaft to make the vertical gyroscope assembly reaches the static balance requirement. According to the invention, advantages of simple structure and convenient utilization can be realized, and the debugging of static balance can be completed with only one assembly, so the working efficiency can be avoided, and the product destroy can be avoided.

Description

Vertical gyro assembly static equilibrium debugger
Technical field
The present invention relates to static equilibrium debugger, particularly the static equilibrium debugger of vertical gyro assembly.
Background technology
In the repairing of full attitude integration gyro, the static equilibrium debugging of vertical gyro assembly is an important link, and similar to all gyro sort products, the effect of debugging directly has influence on the repairing quality of product.In debug process, first just pack 30T gyro into vertical gyro assembly, then by other zero, assembly is installed to vertical gyro assembly, debug again the installation site of 30T gyro, to reach the requirement of static equilibrium debugging, after adjustment work completes, fastening 30T gyro, the assembly work of vertical gyro assembly completes.But due to the design reasons of product, in the time of the installation site of debugging 30T gyro, need to repeatedly repeat vertical gyro assembly to be installed in full attitude integration gyro in ring, the defective vertical gyro assembly that decomposites of static equilibrium, adjust the installation site of 30T gyro in vertical gyro assembly, again vertical gyro assembly is installed to the process in ring in full attitude integration gyro, such operation not only operation is numerous and diverse, waste time and energy and very easily artificial damage brush and conducting ring, after conducting ring damages, after vertical gyro assembly all must being decomposed, could change, workload is very large, have a strong impact on work efficiency.
Summary of the invention
Technical matters to be solved by this invention is to provide a kind of static equilibrium debugger of vertical gyro assembly, solve gyrounit in Installation and Debugging, because vertical gyro assembly static equilibrium debugging is defective, need to repeatedly repeat to install, decompose vertical gyro assembly and adjust the process of gyro at vertical gyro component mounting position.
For solving the problems of the technologies described above, the technical solution adopted in the present invention is: a kind of vertical gyro assembly static equilibrium debugger, vertical gyro assembly static equilibrium debugger comprises base, bearing bracket stand, inner seat, set screw and inside casing, base is the open-topped hollow, rectangular body being surrounded by rectangular side panels and rectangular base plate, base both sides are provided with the back up pad of stationary shaft bolster, inner seat is by annulus top board, the unlimited T-shaped post of hollow in both sides of inner seat side plate and base plate composition, inner seat side plate top is provided with protrusion axle, base plate is provided with the T-shaped hole circle cylinder that vertical gyro assembly is installed, inside casing is by annulus base plate, the T-shaped post of hollow that the both sides of inside casing side plate and top board composition are opened wide, top board is provided with T-shaped hole internal thread hole cylinder, set screw is located in T-shaped internal thread hole cylinder,
On inner seat annulus top board and inside casing annulus base plate, be equipped with connecting hole, bolt can be fixed on inside casing in inner seat through connecting hole, the protrusion axle of cover head bearing is placed on bearing bracket stand, interconnective inner seat and inside casing can be rotated freely around protruding axle 360 degree in base, and form a balanced structure.
Connecting hole on described inner seat annulus top board and inside casing annulus base plate is respectively four, is along the circumferential direction uniformly distributed.
Described bearing bracket stand is fixed by screws in the back up pad of base.
In described back up pad, be semiaxis bearing for the supporting base of spring bearing.
Described T-shaped internal thread hole top is provided with the internal thread of fastening adjustment screws.
Described set screw is N-shaped.
A kind of vertical gyro assembly static equilibrium debugger provided by the invention, vertical gyro assembly is arranged between the inner seat and inside casing that can rotate freely around protrusion axle, adjust the installation site of gyro at vertical gyro assembly by the groove of adjusting on gyroaxis, make vertical gyro assembly reach static equilibrium requirement.The present invention is simple in structure, easy to use, and once assembling can complete statically balanced debugging, has improved work efficiency, has avoided damage of product.
Brief description of the drawings
Below in conjunction with drawings and Examples, the invention will be further described:
Fig. 1 is structure vertical view of the present invention.
Fig. 2 is that the master of base 1 in the present invention looks schematic diagram.
Fig. 3 is the schematic top plan view of base 1 in the present invention.
Fig. 4 is the schematic side view of base 1 in the present invention.
Fig. 5 is the schematic top plan view of inner seat 3 in the present invention.
Fig. 6 is the A-A cut-away view of Fig. 5.
Fig. 7 is the schematic side view of inner seat 3 in the present invention.
Fig. 8 is the schematic top plan view of inside casing 5 in the present invention.
Fig. 9 is the B-B cut-away view of Fig. 8.
Figure 10 is that the master of axis bolster 2 of the present invention looks schematic diagram.
Figure 11 is the schematic side view of axis bolster 2 of the present invention.
Figure 12 is the structural representation of set screw 4 in the present invention.
In Fig. 1-12: base 1, bearing bracket stand 2, inner seat 3, set screw 4, inside casing 5, back up pad 6, connecting hole 7, T-shaped hole circle cylinder 8, protrudes axle 9, annulus top board 10, inner seat side plate 11, base plate 12, annulus base plate 13, inside casing side plate 14, top board 15, T-shaped internal thread hole cylinder 16.
Embodiment
As shown in Fig. 1-12, vertical gyro assembly static equilibrium debugger comprises base 1, bearing bracket stand 2, inner seat 3, set screw 4, inside casing 5 and the open-topped hollow, rectangular body of base 1 for being surrounded by rectangular side panels and rectangular base plate, base 1 both sides are provided with the back up pad 6 of stationary shaft bolster 2, inner seat 3 is by annulus top board 10, inner seat side plate 11 and base plate 12 form the T-shaped post of the unlimited hollow in both sides, inner seat side plate top is provided with protrudes axle 9, base plate 12 is provided with the T-shaped hole circle cylinder 8 that vertical gyro assembly is installed, inside casing 5 is by annulus base plate 13, inside casing side plate 14 and top board 15 form the T-shaped post of hollow that both sides are opened wide, on top board 15, establish T-shaped internal thread hole cylinder 16, set screw is located in T-shaped internal thread hole cylinder 16,
On inner seat 3 annulus top boards 10 and inside casing 5 annulus base plates 15, be equipped with connecting hole 7, bolt can be fixed on inside casing 5 in inner seat 3 through connecting hole 7, the protrusion axle 9 of cover head bearing is placed on bearing bracket stand 2, interconnective inner seat 3 and inside casing 5 can be rotated freely around protruding axle 9 360 degree in base 1, and form a balanced structure.
Structure thus, by bolt, inner seat 3 annulus top boards 10 are connected with inside casing 5 annulus base plates 15, make inner seat 3 and inside casing 5 be linked to be entirety, and the space that formation can be placed vertical gyro assembly between inner seat 3 and inside casing, bearing on the inner seat 3 and the inside casing 5 utilization protrusion axles 9 that are placed in base 1 is realized 360 degree around protrusion axle 9 and is rotated freely on back up pad 6 bearing seats, after rotation stops automatically, inner seat 3 and inside casing 5 can be in equilibrium states.After vertical gyro assembly is arranged between inner seat 3 and inside casing 5, by setting nut 4, vertical gyro assembly is adjusted in gap between inner seat and inside casing, finally realized the statically balanced debugging of vertical gyro assembly by adjusting the installation site of gyro in vertical gyro assembly.
T-shaped internal thread hole cylinder 16 on T-shaped hole circle cylinder 8 on inner seat 3 base plates 12 and inside casing 5 top boards 15 can make cover have the vertical gyro assembly two ends of bearing to be separately fixed in T-shaped hole circle cylinder 8 and T-shaped internal thread hole cylinder 16, and vertical gyro assembly can rotate freely by 360 degree by bearing in the space that inner seat 3 and inside casing 5 form.
Connecting hole 7 on described inner seat 3 annulus top boards 10 and inside casing 5 annulus base plates 15 is respectively four, is along the circumferential direction uniformly distributed.With the connecting hole 7 on annulus base plate 15, inner seat 3 and inside casing 5 are connected by screw to can make both be connected more firm stable by being evenly distributed on annulus top board 10.
Preferably, as shown in Fig. 2 and Figure 10, described bearing bracket stand 2 is fixed by screws in the back up pad 6 of base 1.Bearing bracket stand 2 design for disassemblies, facilitate the installation of bearing replacing and cleaning and inner seat 3 and inside casing 5.
In described back up pad 6, be semiaxis bearing for the supporting base of spring bearing.
As shown in Figure 9, described T-shaped internal thread hole 16 tops are provided with the internal thread of fastening adjustment screws 4.
As shown in figure 12, described set screw 4 is N-shaped.Vertical gyro assembly one end that the N-shaped design of set screw 4 is convenient to be equipped with bearing is placed in the T-shaped internal thread hole cylinder 16 of inside casing 5 top boards 15, and can realize the gap adjustment of vertical gyro assembly between inside casing 5 and inner seat 3 by rotation set screw 4.
The operation steps that uses this vertical gyro assembly static equilibrium debugger to carry out static equilibrium debugging is as follows:
First rotate inside casing 5 and inner seat 3, make inside casing 5 upwards, unclamp and connect four screws of inside casing 5 and inner seat 3 and take off inside casing, after being loaded onto to D1000095M02 bearing, vertical gyro assembly two ends pack static equilibrium adjustment exerciser inner seat into, vertical gyro assembly one end is fixed on the T-shaped hole circle cylinder 8 of inner seat 3 base plates 12, the other end is fixed on the T-shaped internal thread hole cylinder 16 of inside casing 5 top boards 15, then load onto inside casing also with four screw fastenings, again rotate inside casing and inner seat, vertical gyro assembly is horizontal, then rotate the set screw 4 in T-shaped internal thread hole cylinder 16 with screwdriver, making the gap of vertical gyro assembly between inside casing 5 and inner seat 3 is that the multiplex clearance test instrument of 0.018mm~0.025mm(is tested), now install.Static equilibrium is adjusted to exerciser to be placed on hummer, add 240mg technique counterweight at the rotor case upper cover of vertical gyro assembly, with the groove on screwdriver rotary gyro axle, regulate its installation site in vertical gyro assembly, make vertical gyro assembly balance and stability or two reverse directions in four orientation of horizontal and vertical position topple over speed and equate, completed statically balanced debugging.

Claims (6)

1. vertical gyro assembly static equilibrium debugger, it is characterized in that: vertical gyro assembly static equilibrium debugger comprises base (1), bearing bracket stand (2), inner seat (3), set screw (4) and inside casing (5), the open-topped hollow, rectangular body of base (1) for being surrounded by rectangular side panels and rectangular base plate, base (1) both sides are provided with the back up pad (6) of stationary shaft bolster (2), inner seat (3) is by annulus top board (10), the unlimited T-shaped post of hollow of inner seat side plate (11) and base plate (12) composition both sides, inner seat side plate (11) top is provided with protrudes axle (9), base plate (12) is provided with the T-shaped hole circle cylinder (8) that vertical gyro group instrument part is installed, inside casing (5) is by annulus base plate (13), the T-shaped post of hollow that inside casing side plate (14) and top board (15) composition both sides are opened wide, top board (15) is provided with T-shaped internal thread hole cylinder (16), set screw is located in T-shaped internal thread hole cylinder (16),
On inner seat (3) annulus top board (10) and inside casing (5) annulus base plate (15), be equipped with connecting hole (7), bolt is fixed on inside casing (5) in inner seat (3) through connecting hole (7), the protrusion axle (9) of cover head bearing is placed on bearing bracket stand (2), interconnective inner seat (3) and inside casing (5) can be rotated freely around protruding axle (9) 360 degree in base (1), and form a balanced structure.
2. vertical gyro assembly static equilibrium debugger according to claim 1, it is characterized in that: the connecting hole (7) on described inner seat (3) annulus top board (10) and inside casing (5) annulus base plate (15) is respectively four, is along the circumferential direction uniformly distributed.
3. vertical gyro assembly static equilibrium debugger according to claim 1, is characterized in that: described bearing bracket stand (2) is fixed by screws in the back up pad (6) of base (1).
4. according to the vertical gyro assembly static equilibrium debugger described in claim 1 or 3, it is characterized in that: described back up pad (6) is upper is semiaxis bearing for the supporting base of spring bearing.
5. vertical gyro assembly static equilibrium debugger according to claim 1, is characterized in that: described T-shaped internal thread hole (16) top is provided with the internal thread of fastening adjustment screws (4).
6. vertical gyro assembly static equilibrium debugger according to claim 1 or 5, is characterized in that: described set screw (4) is N-shaped.
CN201410297968.5A 2014-06-27 2014-06-27 Vertical gyroscope assembly static balance debugger Active CN104062071B (en)

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CN104062071B CN104062071B (en) 2016-08-17

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109163848A (en) * 2018-10-16 2019-01-08 中国船舶重工集团公司第七0七研究所 A method of adjustment float mass center

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2289205Y (en) * 1996-12-11 1998-08-26 唐世明 Two free degree attitude gyroscope
JPH11160183A (en) * 1997-11-28 1999-06-18 Shinko Electric Co Ltd Static balance measuring device
CN1435682A (en) * 2002-10-25 2003-08-13 贺良 Three-point weighing type static balance
CN1955706A (en) * 2005-10-24 2007-05-02 中国科学院电工研究所 Gyrosope spherical rotor three-D static balaming measuring method and device
CN204043855U (en) * 2014-06-27 2014-12-24 凌云(宜昌)飞机维修工程有限公司 Vertical gyro assembly static equilibrium debugger

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2289205Y (en) * 1996-12-11 1998-08-26 唐世明 Two free degree attitude gyroscope
JPH11160183A (en) * 1997-11-28 1999-06-18 Shinko Electric Co Ltd Static balance measuring device
CN1435682A (en) * 2002-10-25 2003-08-13 贺良 Three-point weighing type static balance
CN1955706A (en) * 2005-10-24 2007-05-02 中国科学院电工研究所 Gyrosope spherical rotor three-D static balaming measuring method and device
CN204043855U (en) * 2014-06-27 2014-12-24 凌云(宜昌)飞机维修工程有限公司 Vertical gyro assembly static equilibrium debugger

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109163848A (en) * 2018-10-16 2019-01-08 中国船舶重工集团公司第七0七研究所 A method of adjustment float mass center

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Effective date of registration: 20170213

Address after: 443007 Hubei city of Yichang Province in Xiaoting District Airport Road No. 17-1

Patentee after: Bedik Lingyun (Yichang) Aircraft Maintenance and Engineering Corporation

Address before: 180 No. 443007 Hubei city of Yichang province located in Xiaoting District Road

Patentee before: Lingyun (Yichang) Aircraft Maintenance and Engineering Corporation