CN111443584A

CN111443584A - Solar quartz watch for aviation

Info

Publication number: CN111443584A
Application number: CN202010302002.1A
Authority: CN
Inventors: 严晴
Original assignee: Individual
Current assignee: Individual
Priority date: 2020-04-16
Filing date: 2020-04-16
Publication date: 2020-07-24

Abstract

The invention relates to the technical field of watches, in particular to a solar quartz watch for aviation, which comprises a watchband and a watch head arranged on the watchband, wherein the watch head is sequentially provided with a watch head metal bottom cover, a watch head metal middle frame, a watch head fixing decoration ring and curved surface compression-resistant glass from bottom to top, a quartz mechanical movement, a radiation-proof isolation cabin curved surface dial plate, an annular second hand, an annular minute hand and an annular hour hand from bottom to top are sequentially arranged inside the watch head metal middle frame, the annular second hand, the annular minute hand and the annular hour hand are all rotationally connected in the watch head metal middle frame in a fixed-axis mode, and the quartz mechanical movement is respectively in transmission connection with the annular second hand, the annular minute hand and the annular hour hand through a lateral. This kind of solar energy quartz watch for aviation realizes changing traditional quartzy core vertically power output shaft into horizontal output shaft, reaches the purpose of timing more accurate, laborsaving, energy saving, promotes the efficiency that solar energy watch dish charges moreover greatly, increase of service life.

Description

Solar quartz watch for aviation

Technical Field

The invention relates to the technical field of watches, in particular to an aviation solar quartz watch.

Background

In daily life and work, the watch is an indispensable tool. The precision and the adaptability to the environment of the watch are equally important for people in special working environments, and particularly for aerospace workers, the watch needs to be capable of working accurately under various extreme conditions and simultaneously can adapt to the change among various environments, such as temperature, air pressure, radiation and the like. In 1970, in the emergency situation that Apollo No. 13 meets an accident in space, an oxygen storage tank on a service cabin explodes, and partial instruments in the cabin are damaged, a spaceman adopts an omega super-overlord wristwatch, so that the accuracy of correction orbit operation for 14 seconds is ensured, and the Aero-super-overlord wristwatch becomes the most critical ring for the spaceman to finally and safely return to the earth.

The existing watches for aerospace workers are all mechanical watches, complex movement of the existing watches must meet weightlessness conditions, particularly the outer space environment after the watches are taken out of a cabin, lubricating oil of the existing watches is not penetrated and solidified under the conditions of plus 120 degrees and minus 90 degrees, so that the normal work is ensured, the manufacturing cost of the space watch is extremely high, the watches are not suitable for batch production, and a lot of spaceworkers do not contact the space watch for the first time until the spacecrafts. Meanwhile, the mechanical watch needs to be wound, because the aerospace watch mostly cannot use an automatic winding mechanism due to the extreme working environment, the aerospace watch needs to be wound regularly, and the workload is greatly increased. The traditional quartz watch movement with lower cost can not adapt to the radiation of the outer space, which causes the abnormity of overlarge time deviation, and is very inconvenient. Aiming at the special environments of weightlessness, overweight and the like of aerospace, the traditional hour-minute second hand dial plate has a plurality of defects, the working environment of the traditional hour-minute second hand dial plate enables the inertia of a pointer to be very large, so that the pressure on a mechanical movement is very large, and the precision of the watch is easy to reduce.

In view of this, we propose a solar quartz watch for aviation.

Disclosure of Invention

The invention aims to provide an aviation solar quartz watch to solve the problems in the background technology.

In order to achieve the purpose, the invention provides the following technical scheme: a solar quartz watch for aviation comprises a watchband and a watch head arranged on the watchband, wherein the watch head is sequentially provided with a watch head metal bottom cover, a watch head metal middle frame, a watch head fixing decoration ring and curved surface compression-resistant glass from bottom to top, a quartz mechanical movement, an isolation cabin, a curved surface watch plate, an annular second hand, an annular minute hand and an annular hour hand from bottom to top are sequentially arranged inside the watch head metal middle frame, the annular second hand, the annular minute hand and the annular hour hand are all rotationally connected inside the watch head metal middle frame in a fixed-axis mode, the quartz mechanical movement is respectively in transmission connection with the annular second hand, the annular minute hand and the annular hour hand through a lateral transmission mechanism, a 12-hour noctilucent indicator mark is arranged on the side edge of the upper surface of the curved surface watch plate, a plurality of teeth are fixed on the side edges of the lower surfaces of the annular second hand, the annular minute hand and the annular hour, and the stopping mechanism and the lateral transmission mechanism are both arranged on the driving mechanism, and the driving mechanism is respectively in transmission connection with the stopping mechanism and the lateral transmission mechanism.

Preferably, the driving mechanism comprises a supporting disc fixed inside the gauge head metal middle frame, the fixed axis of the upper surface of the supporting disc is rotatably connected with a ring plate, the turntable is arranged on the inner side of the ring plate and can rotate on the fixed axis of the inner side of the ring plate, the gauge head metal middle frame, the supporting disc, the ring plate and the turntable share the central axis, the fixed axis at the center of the supporting disc is rotatably connected with a first rotating shaft, the first rotating shaft penetrates through the supporting disc, and one end, located on the upper surface of the supporting disc, of the first rotating shaft is fixedly connected with the turntable.

Preferably, a micro motor is fixed on the lower surface of the supporting disk, a bevel gear II is fixed on the output shaft end of the micro motor, a bevel gear III is fixed on one end of the rotating shaft I, which is located on the lower surface of the supporting disk, and the bevel gear II is in meshed connection with the bevel gear III.

Preferably, the upper surface of the ring plate is fixed with a plurality of first pin shafts and a plurality of second pin shafts, the number of the first pin shafts is the same as that of the second pin shafts, the plurality of first pin shafts and the plurality of second pin shafts are arranged at equal intervals along the circumferential direction of the ring plate, one pin shaft is located between every two adjacent second pin shafts, and the distance between the first pin shaft and the center of the ring plate is smaller relative to the second pin shaft.

Preferably, the lateral transmission mechanism comprises a second rotating shaft, the central axis of the second rotating shaft vertically points to the annular plate, the second rotating shaft is rotatably connected into the guide sleeve, the guide sleeve is fixed on the upper surface of the supporting disc, a first bevel gear is fixed at one end of the second rotating shaft vertically points to the annular plate, the first bevel gear is meshed with the gear ring and is connected with the gear ring, the gear ring is fixed at the outer side edge of the upper surface of the annular plate, a first twill gear, a second twill gear and a third twill gear are fixed at one end, far away from the annular plate, of the second rotating shaft, the first twill gear, the second twill gear and the third twill gear are respectively connected with the annular second hand.

Preferably, actuating mechanism still includes the driving lever, and the dead axle rotates on the driving lever and is connected with the axostylus axostyle, and the upper surface at the carousel is fixed to the axostylus axostyle, and the distance of axostylus axostyle and the carousel centre of a circle is greater than zero, and U-shaped groove one has been seted up to the one end of driving lever, and the bar groove has been seted up to the other end.

Preferably, the support disc is fixed with a fixing rod, the fixing rod is inserted into the strip-shaped groove, the fixing rod can slide in the strip-shaped groove, the first U-shaped groove can be inserted and buckled on the first pin shaft, and the first pin shaft can slide in the first U-shaped groove.

Preferably, the stopping mechanism comprises a guide groove fixed on the supporting disc, the guide groove and the fixing rod are located on two sides of the ring plate, an inserting rod is connected to the guide groove in a sliding mode and perpendicular to the central axis of the ring plate, a U-shaped groove II is formed in one end, pointing to the ring plate, of the inserting rod, the U-shaped groove II can be buckled on the pin shaft II in a inserting mode, and the pin shaft II can slide in the U-shaped groove II.

Preferably, one end of the inserted link far away from the annular plate is connected with one end of the connecting link in a fixed-axis rotating manner, and the other end of the connecting link is connected with the driving lever fixed-axis in a rotating manner.

Compared with the prior art, the invention has the beneficial effects that:

according to the invention, the surface area of the flexible solar watch dial is increased by adopting a pointer-free curved surface dial design, the charging efficiency of the solar watch dial is greatly improved, the service life is prolonged, meanwhile, the internal space of the watch head is increased for setting a radiation isolation region, the problem that a common quartz watch cannot be used for space dilemma is solved, and the overall process is simpler in structure, lower in cost and more fashionable in appearance design compared with the existing space watch;

according to the invention, the lateral transmission mechanism is driven by the driving mechanism to work, and the annular second hand, the annular minute hand and the annular hour hand are driven by the lateral transmission mechanism to rotate for timing, so that the power output shaft vertical to the traditional quartz movement is changed into a horizontal output shaft, and the annular pointer is driven by the helical gear to move, thereby achieving the purposes of saving labor and energy;

according to the invention, the stopping mechanism is driven by the driving mechanism to overcome the action of inertia force generated by the driving mechanism, so that the stopping function of the annular plate is realized, and the timing of the annular second hand, the annular minute hand and the annular hour hand is more accurate.

Drawings

FIG. 1 is an exploded view of the final assembly structure of the present invention;

FIG. 2 is a first top view of the quartz mechanical core structure of the present invention;

FIG. 3 is a second top view of the upper surface of the mechanical quartz movement structure of the present invention;

FIG. 4 is a third top view of the quartz mechanical core structure of the present invention;

FIG. 5 is a fourth top view of the upper surface of the mechanical quartz movement structure of the present invention;

fig. 6 is a bottom view of the lower surface of the mechanical quartz movement structure of the present invention.

In the figure: 1-watchband; 2-a gauge outfit metal bottom cover; 3-header metal middle frame; 4-quartz mechanical movement; 5-a lateral transmission mechanism; 6-radiation protection isolation cabin; 7-curved dial plate; a luminous indicator mark for 8-12 hours; 9-annular second hand; 10-annular minute hand; 11-annular hour hand; 12-dial fixing decorative ring; 13-curved surface compression resistant glass; 14-a support disc; 15-ring plate; 16-a gear ring; 17-a first pin shaft; 18-pin shaft II; 19-rotating the first shaft; 20-a turntable; 21-shaft rod; 22-a deflector rod; 23-a strip-shaped groove; 24-a fixation rod; 25-a guide groove; 26-a plunger; 27-a connecting rod; 28-a guide sleeve; 29-rotating shaft two; 30-bevel gear one; 31-a first twill gear; 32-twill gear two; 33-twill gear three; 34-a micro motor; 35-bevel gear two; 36-bevel gear three; 37-U-shaped clamping groove I; 38-U-shaped clamping groove II.

Detailed Description

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 obtained by a person skilled in the art without any inventive step based on the embodiments of the present invention, are within the scope of the present invention.

Referring to fig. 1 to 6, the present invention provides a technical solution: a solar quartz watch for aviation comprises a watchband 1 and a watch head arranged on the watchband 1, wherein the watch head is sequentially provided with a watch head metal bottom cover 2, a watch head metal middle frame 3, a watch head fixing decoration ring 12 and curved surface compression-resistant glass 13 from bottom to top, a quartz mechanical movement 4, an isolation cabin 6, a curved surface watch plate 7, an annular second hand 9, an annular minute hand 10 and an annular hour hand 11 are sequentially arranged in the watch head metal middle frame 3 from bottom to top, the annular second hand 9, the annular minute hand 10 and the annular hour hand 11 are all connected in the watch head metal middle frame 3 in a fixed-axis rotating manner, the quartz mechanical movement 4 is respectively connected with the annular second hand 9, the annular minute hand 10 and the annular hour hand 11 in a driving manner through a lateral transmission mechanism 5, a 12-hour noctilucent indicating mark 12 is arranged at the side edge of the upper surface of the curved surface watch plate 7, a plurality of teeth are fixed on the side edges of the lower surfaces of the annular second, the quartz mechanical movement 4 comprises a driving mechanism and a stopping mechanism, the stopping mechanism and the lateral transmission mechanism 5 are both arranged on the driving mechanism, and the driving mechanism is in transmission connection with the stopping mechanism and the lateral transmission mechanism 5 respectively.

In this embodiment, the isolation capsule 6 is a radiation-proof isolation capsule, an electronic part of the quartz movement is arranged in the radiation-proof isolation capsule 6, and meanwhile, the electronic part of the quartz movement is protected against the 100kard TID radiation performance requirement, so that the integral watch head has aerospace-grade sealing performance, and the integral process is convenient for batch manufacturing.

The design material of the radiation-proof isolation cabin adopts the existing radiation-proof isolation material manufacturing process, which is the prior art. The protection of the application is not provided here, so the radiation protection isolation material is not described in detail.

In this embodiment, in order to increase gauge outfit inner space, become curved surface 7 with traditional plane dial plate, the pointer axle of cancellation dial plate, whole curved surface dial plate 7 adopts for flexible solar energy material, curved surface dial plate 7 is the flexible solar cell of a curved surface in fact, turn into solar energy electric energy storage and provide power for quartzy mechanical movement, increase curved surface dial plate 7's usable floor area, 12 hours night light indicateing board 8 on the curved surface dial plate 7 has adopted the night light material, so that observe time in the environment that light is more weak.

In the embodiment, the pointer is changed from a central shaft to an annular pointer, the pointer is changed from a needle shape to an annular shape in time, minutes and seconds, the balance of the pointer is improved when the pointer loses gravity, and meanwhile, the annular pointer is made of a polytetrafluoroethylene composite self-lubricating material which meets the aerospace standard, so that the lubricant is prevented from being solidified and invalid in an extreme environment;

in the embodiment, a closed structure is arranged in a curved surface space below the curved surface dial 7 to protect an electronic circuit part of the quartz watch, the closed structure adopts barium sulfate, lead powder and other materials to meet the TID radiation performance requirement of resisting 100kard, the circuit part of the quartz watch core, such as a crystal oscillator and other materials, which meet the aviation class2/3 task level, so that the stable work under the extreme conditions of outer space and the like is ensured, and a CT L920F rechargeable lithium battery is adopted in the circuit part of the quartz watch core, so that the charging complementation can be carried out with the curved surface dial 7, and the service life is greatly prolonged;

in this embodiment, the whole gauge outfit cancels the time-adjusting crown, adjusts to leave the factory for the time correction of task customization each time, reduces the error, also prevents that outside personnel from using at will, reduces the crown simultaneously and can reduce overall cost and increase whole sealing performance.

In this embodiment, the meter head metal chassis 2 at the lowest inside of the meter head adopts a titanium metal cover plate with the back surface covered with a thermal insulation material, is sealed by aerospace-grade silica gel sealant, and is fixed at the bottom of the meter head metal middle frame 3 by four screws.

In this embodiment, gauge outfit metal center 3 uses all-metal ring shape structure to the inside wall sets up 3 annular track grooves and is used for 3 annular pointer movements, uses 3D printing technique to make simultaneously, under the prerequisite of guaranteeing the precision, reduce cost increases production speed.

In this embodiment, watchband 1 of wrist-watch adopts the preparation of high performance silica gel, and 1 inside lining of watchband and the inseparable interlock of double-colored integrated into one piece technology of outer lane adoption firmly wrap up the gauge outfit wholly, conveniently change watchband 1 or fixed position simultaneously.

In this embodiment, as shown in fig. 2 to 5, the driving mechanism includes a supporting disk 14 fixed inside the gauge outfit metal middle frame 3, a ring plate 15 is connected to the upper surface of the supporting disk 14 in a fixed-axis rotation manner, a rotating disk 20 is disposed inside the ring plate 15, the rotating disk 20 can rotate in the fixed-axis rotation manner inside the ring plate 15, the gauge outfit metal middle frame 3, the supporting disk 14, the ring plate 15 and the rotating disk 20 share a central axis, a first rotating shaft 19 is connected to the center of the supporting disk 14 in a fixed-axis rotation manner, the first rotating shaft 19 penetrates through the supporting disk 14, and one end of the first rotating shaft 19, which is located on the upper surface of the supporting disk 14, is fixedly connected to the.

In this embodiment, as shown in fig. 6, a micro motor 34 is fixed on the lower surface of the supporting disk 14, a second bevel gear 35 is fixed on the output shaft end of the micro motor 14, a third bevel gear 36 is fixed on one end of the first rotating shaft 19, which is located on the lower surface of the supporting disk 14, and the second bevel gear 35 and the third bevel gear 36 are in meshed connection.

In this embodiment, as shown in fig. 2 to 5, a plurality of first pin shafts 17 and a plurality of second pin shafts 18 are fixed on the upper surface of the ring plate 15, the number of the first pin shafts 17 is the same as that of the second pin shafts 18, the plurality of first pin shafts 17 and the plurality of second pin shafts 18 are all arranged at equal intervals along the circumferential direction of the ring plate 15, the first pin shafts 17 are located between two adjacent second pin shafts 18, and the distance from the first pin shafts 17 to the center of the ring plate 15 is smaller than that from the second pin shafts 18.

In this embodiment, as shown in fig. 2 to 5, the lateral transmission mechanism 5 includes a second rotating shaft 29, the second rotating shaft 29 is vertically directed to the central axis of the annular plate 15, the second rotating shaft 29 is connected to the guide sleeve 28 in a fixed-axis rotating manner, the guide sleeve 28 is fixed on the upper surface of the support disk 14, a first bevel gear 30 is fixed at one end of the second rotating shaft 29 directed to the annular plate 15, the first bevel gear 30 is engaged with the ring gear 16, the ring gear 16 is fixed on the outer side of the upper surface of the annular plate 15, a first twill gear 31, a second twill gear 32 and a third twill gear 33 are fixed at one end of the second rotating shaft 29 away from the annular plate 15, and the first twill gear 31, the second twill gear 32 and the third twill gear 33 are respectively connected to the teeth on the lower surface sides of.

In this embodiment, as shown in fig. 2 to 5, the driving mechanism further includes a shift lever 22, a fixed shaft on the shift lever 22 is rotatably connected to a shaft rod 21, the shaft rod 21 is fixed on the upper surface of the turntable 20, a distance between the shaft rod 21 and a circle center of the turntable 20 is greater than zero, one end of the shift lever 22 is provided with a U-shaped groove 37, the other end of the shift lever 22 is provided with a strip-shaped groove 23, and the shaft rod 21 is located between the U-shaped groove 37 and the strip-shaped.

In this embodiment, as shown in fig. 2 to 5, a fixing rod 24 is fixed on the supporting disk 14, the fixing rod 24 is inserted into the strip-shaped groove 23, the fixing rod 24 can slide in the strip-shaped groove 23, the first U-shaped groove 37 can be inserted and buckled on the first pin 17, and the first pin 17 can slide in the first U-shaped groove 37.

In this embodiment, as shown in fig. 2 to 5, the stopping mechanism includes a guide groove 25 fixed on the supporting disk 14, the guide groove 25 and the fixing rod 24 are located at two sides of the ring plate 15, an inserting rod 26 is slidably connected to the guide groove 25, the inserting rod 26 is perpendicular to the central axis of the ring plate 15, a U-shaped groove two 38 is formed at one end of the inserting rod 27, which points to the ring plate 15, the U-shaped groove two 38 can be inserted and buckled on the pin shaft two 18, and the pin shaft two 18 can slide in the U-shaped groove two 38.

In this embodiment, as shown in fig. 2 to 5, one end of the insertion rod 26 away from the ring plate 15 is connected to one end of a link 27 in a fixed-axis rotation manner, and the other end of the link 27 is connected to the shift lever 22 in a fixed-axis rotation manner.

When the solar quartz watch for aviation is used, the solar quartz watch for aviation comprises the following steps:

the method comprises the following steps: as shown in fig. 6, the curved dial 7 converts solar energy, and provides electric energy to the micro motor 34 through the electronic part, so that the micro motor 34 works, and drives the first rotating shaft 19 to rotate through the second bevel gear 35 and the third bevel gear 36 via the output shaft thereof, as shown in fig. 2 to 5, the first rotating shaft 19 is set to rotate counterclockwise, the first rotating shaft 19 synchronously drives the turntable 20 to rotate counterclockwise, so that the turntable 20 synchronously drives the shaft lever 21 to rotate counterclockwise, the shaft lever 21 synchronously drives the shift lever 22 to rotate counterclockwise around the turntable 20 during the counterclockwise rotation, because the right end of the shift lever 22 is limited by the fixing rod 24, the shift lever 22 makes a vertical movement around the fixing rod 24, and the shaft lever 21 drives the shift lever 22 to move horizontally, as shown in fig. 2, the shaft lever 21 drives the shift lever 22 to swing up to the highest point position, and starts to drive the shift lever 22 to swing downward, at this time, the first U-shaped groove 37 on the shift lever 22 is just in inserting and buckling contact with the first corresponding pin 17 on the ring plate 15, as shown in fig. 2 to 4, when the shaft lever 21 drives the shift lever 22 to swing from the highest point to the lowest point, in the process, the shift lever 22 applies downward pressure to the first corresponding pin 17, so that the first pin 17 moves downward in the vertical direction, the ring plate 15 is driven to rotate counterclockwise through the first pin 17, and when the shift lever 22 is at the lowest point, the first U-shaped groove 37 on the shift lever 22 is just separated from the first corresponding pin 17 on the ring plate 15;

as shown in fig. 4, 5 and 2, when the shaft lever 21 drives the shift lever 22 to swing from the lowest point position to the highest point position, at this time, since the first U-shaped groove 37 on the shift lever 22 is separated from and does not contact the first corresponding pin 17 on the ring plate 15, no force is generated, and therefore, the first pin 17 does not drive the ring plate 15 to rotate clockwise, so that the ring plate 15 rotates intermittently counterclockwise;

step two: in the process of anticlockwise rotation of the ring plate 15, the gear ring 16 is synchronously driven to anticlockwise rotate, the anticlockwise rotation of the gear ring 16 drives the rotating shaft II 29 to rotate through the bevel gear I30, so that the rotating shaft II 29 synchronously drives the twill gear I31, the twill gear II 32 and the twill gear III 33 to synchronously rotate, further, the annular second hand 9, the annular minute hand 10 and the annular hour hand 11 are driven to rotate through the tooth transmission action on the twill gear I31, the twill gear II 32 and the twill gear III 33 and the corresponding annular second hand 9, the annular minute hand 10 and the annular hour hand 11, the driving of the annular second hand 9, the annular minute hand 10 and the annular hour hand 11 is realized, the vertical power output shaft of the traditional quartz movement is changed into a horizontal output shaft, the annular hands are driven to move through the twill teeth, the purposes of labor saving and energy saving are achieved, and a balancing weight can be, the balance mechanism is used for balancing the gravity center offset generated when the lateral transmission mechanism 5 and the quartz mechanical movement 4 work, and further ensuring the gravity center balance of the whole meter head;

step three: as shown in fig. 2 and 3, when the shift lever 22 is at the highest point position, the U-shaped second groove 38 on the insert rod 26 is just separated from the second pin 18, so as to avoid blocking the rotation of the annular plate 15, when the shift lever 22 swings down to the position in fig. 3, the shaft rod 21 applies a leftward thrust to the shift lever 22 in the horizontal direction, so that the shift lever 22 applies a leftward thrust to the insert rod 26 through the connecting rod 27, and the insert rod 26 slides leftward in the guide groove 25, and when the shift lever 22 and the insert rod 26 are in the same straight line, the insert rod 26 is farthest away from the second pin 18;

as shown in fig. 3 and 4, in the process that the shift lever 22 swings down from the position in fig. 3 to the position in fig. 4, at this time, the shaft lever 21 applies a rightward pulling force to the shift lever 22 in the horizontal direction, so that the shift lever 22 applies a rightward pulling force to the insertion rod 26 through the connecting rod 27, and further the insertion rod 26 slides rightward in the guide groove 25, when the shift lever 22 swings down to the lowest point position, at this time, the U-shaped groove two 38 on the insertion rod 26 just contacts with the pin shaft two 18 in an insertion manner, and in the process that the swing rod 22 swings down completely, the insertion rod 22 and the pin shaft two 18 do not generate a force action, so that the shift lever 22 cannot be influenced to drive the ring plate 15 to rotate counterclockwise through the pin shaft one 17, and further the ring plate 15 is ensured to drive the ring;

as shown in fig. 4 and 5, when the shift lever 22 is at the lowest point position, the first U-shaped groove 37 on the shift lever 22 is just separated from the first pin 17 and does not contact, the driving force on the ring plate 15 stops being generated, when the shift lever 22 swings to the position in fig. 5, and the second U-shaped groove 38 on the insert rod 26 is just in inserting contact with the second pin 18, so that a blocking effect is generated on the second pin 18, so that the ring plate 15 cannot continue to rotate under the action of inertia force, in the process that the shift lever 22 swings from the position in fig. 4 to the position in fig. 5, as the shaft rod 21 horizontally applies a rightward pulling force on the shift lever 22, the shift lever 22 applies a rightward pulling force on the insert rod 26 through the connecting rod 27, so that the insert rod 26 slides rightward in the guide groove 25, and when the shift lever 22 and the insert rod 26 are in the same straight line, the insert rod 26 is at the moment, the insert rod 26;

as shown in fig. 5 and fig. 2, in the process that the shift lever 22 swings upward from the position in fig. 5 to the position in fig. 2, at this time, because the shaft lever 21 applies a leftward pushing force to the shift lever 22 in the horizontal direction, so that the shift lever 22 applies a leftward pushing force to the insertion rod 26 through the connecting rod 27, and further, the insertion rod 26 slides leftward in the guide groove 25, when the shift lever 22 swings upward to the highest position, at this time, the first U-shaped groove 37 on the shift lever 22 just makes plug contact with the first pin shaft 17, and the second U-shaped groove 38 on the insertion rod 26 just separates from and does not make contact with the second pin shaft 18, in the process that the swing rod 22 swings upward completely, the insertion rod 22 generates a blocking force to the second pin shaft 18, so that the ring plate 15 continues to rotate counterclockwise without the effect of inertia force, which plays a role of stopping the ring plate 15, and.

The foregoing shows and describes the general principles, essential features, and advantages of the invention. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, and the preferred embodiments of the present invention are described in the above embodiments and the description, and are not intended to limit the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims

1. The utility model provides an aviation is with quartzy table of solar energy, includes watchband (1) and the gauge outfit of setting on watchband (1), its characterized in that: the watch head is sequentially provided with a watch head metal bottom cover (2), a watch head metal middle frame (3), a dial plate fixing decoration ring (12) and curved surface compression-resistant glass (13) from bottom to top, a quartz mechanical movement (4), an isolation cabin (6), a curved surface dial plate (7), an annular second hand (9), an annular minute hand (10) and an annular hour hand (11) are sequentially arranged inside the watch head metal middle frame (3) from bottom to top, the annular second hand (9), the annular minute hand (10) and the annular hour hand (11) are all connected into the watch head metal middle frame (3) in a fixed-axis rotating mode, the quartz mechanical movement (4) is respectively connected with the annular second hand (9), the annular minute hand (10) and the annular hour hand (11) in a transmission mode through a lateral transmission mechanism (5), and a 12-hour noctilucent indicating mark (12) is arranged on the side edge of the upper surface of the curved surface;

a plurality of teeth are fixed on the side edges of the lower surfaces of the annular second hand (9), the annular minute hand (10) and the annular hour hand (11) at equal intervals along the circumferential direction;

the quartz mechanical movement (4) comprises a driving mechanism and a stopping mechanism, the stopping mechanism and the lateral transmission mechanism (5) are arranged on the driving mechanism, and the driving mechanism is in transmission connection with the stopping mechanism and the lateral transmission mechanism (5) respectively.

2. The solar quartz watch for aviation according to claim 1, wherein: actuating mechanism is including fixing support disc (14) inside gauge outfit metal center (3), the upper surface dead axle of support disc (14) rotates and is connected with crown plate (15), the inboard of crown plate (15) sets up carousel (20), and carousel (20) can rotate at the inboard dead axle of crown plate (15), gauge outfit metal center (3), support disc (14), crown plate (15) and carousel (20) sharing the central axis, the center department dead axle of support disc (14) rotates and is connected with pivot (19), and pivot (19) run through support disc (14), pivot (19) are located the one end and carousel (20) fixed connection of the upper surface of support disc (14).

3. The solar quartz watch for aviation according to claim 2, characterized in that: the lower surface of the supporting disk (14) is fixedly provided with a micro motor (34), the output shaft end of the micro motor (14) is fixedly provided with a second bevel gear (35), one end, located on the lower surface of the supporting disk (14), of the first rotating shaft (19) is fixedly provided with a third bevel gear (36), and the second bevel gear (35) is in meshed connection with the third bevel gear (36).

4. The solar quartz watch for aviation according to claim 2, characterized in that: the upper surface of the ring plate (15) is fixed with a plurality of first pin shafts (17) and a plurality of second pin shafts (18), the number of the first pin shafts (17) is the same as that of the second pin shafts (18), the first pin shafts (17) and the second pin shafts (18) are arranged at equal intervals along the circumference of the ring plate (15), the first pin shafts (17) are located at positions between the two adjacent pin shafts (18), and the distance between the first pin shafts (17) and the circle center of the ring plate (15) is smaller relative to the second pin shafts (18).

5. The solar quartz watch for aviation according to claim 4, wherein: the lateral transmission mechanism (5) comprises a second rotating shaft (29), the second rotating shaft (29) vertically points to the central axis of the annular plate (15), the second rotating shaft (29) is fixedly and rotatably connected in the guide sleeve (28), and the guide sleeve (28) is fixed on the upper surface of the support disc (14), a bevel gear I (30) is fixed at one end of the second rotating shaft (29) which points to the annular plate (15), the bevel gear I (30) is meshed with the gear ring (16), the gear ring (16) is fixed at the outer side edge of the upper surface of the ring plate (15), one end of the second rotating shaft (29) far away from the annular plate (15) is fixed with a first twill gear (31), a second twill gear (32) and a third twill gear (33), the first twill gear (31), the second twill gear (32) and the third twill gear (33) are in transmission connection with teeth on the lower surface side of the annular second hand (9), the annular minute hand (10) and the annular hour hand (11) respectively.

6. The solar quartz watch for aviation according to claim 4, wherein: the driving mechanism further comprises a driving lever (22), a fixed shaft is rotatably connected with a shaft lever (21) on the driving lever (22), the shaft lever (21) is fixed on the upper surface of the turntable (20), the distance between the shaft lever (21) and the circle center of the turntable (20) is greater than zero, a U-shaped groove I (37) is formed in one end of the driving lever (22), a strip-shaped groove (23) is formed in the other end of the driving lever, and the shaft lever (21) is located between the U-shaped groove I (37) and the strip-shaped groove (23).

7. The solar quartz watch for aviation according to claim 6, wherein: the fixing rod (24) is fixed on the supporting disc (14), the fixing rod (24) is inserted in the strip-shaped groove (23), the fixing rod (24) can slide in the strip-shaped groove (23), the first U-shaped groove (37) can be inserted and buckled on the first pin shaft (17), and the first pin shaft (17) can slide in the first U-shaped groove (37).

8. The solar quartz watch for aviation according to claim 7, wherein: stop mechanism including fixing guide way (25) on supporting disc (14), and guide way (25) and dead lever (24) are located the both sides of crown plate (15), sliding connection has inserted bar (26) on guide way (25) the central axis mutually perpendicular of inserted bar (26) and crown plate (15), U-shaped groove two (38) have been seted up to the one end of inserted bar (27) directional crown plate (15), U-shaped groove two (38) can be inserted and detained on round pin axle two (18), and round pin axle two (18) can slide in U-shaped groove two (38).

9. The solar quartz watch for aviation according to claim 8, wherein: one end of the inserted rod (26) far away from the annular plate (15) is fixedly and rotatably connected with one end of a connecting rod (27), and the other end of the connecting rod (27) is fixedly and rotatably connected with the shifting rod (22).