CN108557107A - A kind of flywheel ejection system - Google Patents

A kind of flywheel ejection system Download PDF

Info

Publication number
CN108557107A
CN108557107A CN201711339676.3A CN201711339676A CN108557107A CN 108557107 A CN108557107 A CN 108557107A CN 201711339676 A CN201711339676 A CN 201711339676A CN 108557107 A CN108557107 A CN 108557107A
Authority
CN
China
Prior art keywords
flywheel
disc
gear
ejection system
reel
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
Application number
CN201711339676.3A
Other languages
Chinese (zh)
Inventor
雷静桃
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CN201711339676.3A priority Critical patent/CN108557107A/en
Publication of CN108557107A publication Critical patent/CN108557107A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00Ground or aircraft-carrier-deck installations
    • B64F1/04Ground or aircraft-carrier-deck installations for launching aircraft
    • B64F1/06Ground or aircraft-carrier-deck installations for launching aircraft using catapults

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Braking Arrangements (AREA)

Abstract

The present invention relates to carrier-based aircraft ejector technical fields, and in particular to a kind of flywheel ejection system.Including motor, Flywheel disc, selector and shuttle;The motor is located at the side of Flywheel disc, and for driving Flywheel disc to rotate, the selector is located at the other end of Flywheel disc;The Flywheel disc includes main body and Multilayer-tooth wheel disc, and the toothed disc is between main body and selector;The main body is a discoid metal derby, and the toothed disc includes the gear that several radiuses successively successively decrease;The selector includes manipulator and several capstan winches compatible with gear, and the manipulator is used to select the operation of the gear on different capstan winch cooperating teeth wheel discs;Beneficial effects of the present invention are:Coordinate capstan winch that can replace clutch in the case where function does not select meet demand by being used cooperatively Multilayer-tooth wheel disc, avoids conventional clutch there is a situation where overheating to occur, it is more durable.

Description

A kind of flywheel ejection system
Technical field
The present invention relates to carrier-based aircraft ejector technical fields, and in particular to a kind of flywheel ejection system.
Background technology
Carrier-borne aircraft on early stage battleship, heavy cruiser largely uses fly wheel energy storage type ejector, the boat of U.S.'s early stage Mother also uses flywheel energy storage ejector, and this ejector was technically more mature at that time, more powerful later Hydraulic catapult replaced.After World War II, jet-propelled carrier-borne aircraft has expedited the emergence of steam catapult to the ejection higher requirement of power, This technology continued to use for more than 50 years at present, was monopolized by the U.S. always.
While developing steam catapult the forties, the U.S. once carried out the flywheel energy storage ejector of ultra-large type and electronic The exploitation and experiment of ejector.Theoretically flywheel energy storage ejector can reach very high power, but because of (flywheel and cable winch Between) technical barrier of high-speed clutch cannot solve and be abandoned quickly.
If we can solve the problems, such as this, and can reactivate this simple in structure, flywheel ejection easy to use System.
Invention content
The technical problem to be solved by the present invention is to:There is provided a kind of high speed that can be solved between flywheel and cable winch from The flywheel ejection system of clutch heating problem.
In order to solve the above-mentioned technical problem, the technical solution adopted by the present invention is:A kind of flywheel ejection system is provided, it is described Flywheel ejection system is mounted on ship or needs on the object of short distance ejection, and the object includes track, including motor, flywheel Disk, selector and shuttle;The motor is located at the side of Flywheel disc, for driving Flywheel disc to rotate, the gear selection Device is located at the other end of Flywheel disc;The shuttle is located on track;
The Flywheel disc includes main body and Multilayer-tooth wheel disc, and the toothed disc is between main body and selector;Institute It is a discoid metal derby to state main body, and the toothed disc includes the gear that several radiuses successively successively decrease, the toothed disc One end that gear is relatively large in diameter is mounted in main body, and is co-axially mounted with main body;
The selector includes manipulator and several capstan winches compatible with gear, and the manipulator is for selecting The operation of gear on different capstan winch cooperating teeth wheel discs;
The capstan winch includes reel, bearing and stranded cable, and described stranded cable one end is connected on reel, and the other end is movably connected in On shuttle;The reel includes inside and outside, and the inside offers through-hole, and the through-hole is towards the side of Flywheel disc and tooth Wheel is adapted, and the bearing is connected in the other side of through-hole;It is additionally provided on the reel outer surface and is adapted with stranded cable Groove, and be provided at both ends with baffle;The shape of the through-hole is corresponding with gear;The bearing includes outer ring and inner ring, institute It states outer ring and the interior bone of reel is mutually fixed, the inner ring is the disk of the setting of not rounded straight slot;
The manipulator includes displacement arm and selection arm, and described selection arm one end is fixed in displacement arm, and the other end is then Free end, the free end are adapted with reel bearing inner race straight slot.
Further, in above-mentioned flywheel ejection system, the capstan winch further includes brake gear, and the brake gear includes card Pincers and brake disc, the clamp are fixed on bearing inner race, and the brake disc is fixed on capstan winch.
Further, in above-mentioned flywheel ejection system, the brake disc includes multiple through-holes and a plurality of water channel, the through-hole It is evenly distributed on brake disc, the water channel is in array distribution on brake disc.
Further, it in above-mentioned flywheel ejection system, is connected by umbilical connector between the shuttle and stranded cable.
Further, in above-mentioned flywheel ejection system, the both sides of the track are also equipped with being powered of being mutually parallel Electromagnetic path, the electromagnetic path are electrically connected with shuttle.
Further, in above-mentioned flywheel ejection system, the outer surface of the reel is in truncated cone-shaped, and outer surface coats There is one layer of nano-ceramic powder, the one end fits Flywheel disc that when use is relatively large in diameter.
Further, in above-mentioned flywheel ejection system, reinforcing rib is also equipped with inside the reel.
Further, in above-mentioned flywheel ejection system, the stranded cable includes clad, at least layer winding layer and wire rope core group At the winding layer is wrapped on wire rope core, and the clad is coated on outside winding layer;The winding layer is in a manner of spiral coiling Laminated is wrapped on wire rope core, and the winding direction of adjacent winding layer is opposite.
Further, in above-mentioned flywheel ejection system, the wire rope core by 12 strands or 36 bursts of carbon fiber rope twistings or It is knitted to form.
The beneficial effects of the present invention are:Coordinate capstan winch by being used cooperatively Multilayer-tooth wheel disc, does not select to meet in function In the case of demand, clutch can be replaced, avoid conventional clutch there is a situation where overheating to occur, and war is occurring When, Multilayer-tooth wheel disc coordinates the structure of capstan winch, is less likely to be damaged when being hit by a bullet, more durable relative to clutch, in some strand When disk or gear are damaged, it can directly use other capstan winches or gear to substitute, improve operational performance;Pass through multiple capstan winches Use, can quickly to multi rack aircraft carry out follow-through, meet the time demand in wartime.
Description of the drawings
Fig. 1 is a kind of structural schematic diagram of flywheel ejection system of the specific embodiment of the invention;
Fig. 2 is a kind of winch configurations front view of flywheel ejection system of the specific embodiment of the invention;
Fig. 3 is a kind of winch configurations left view of flywheel ejection system of the specific embodiment of the invention;
Fig. 4 is a kind of winch configurations right view of flywheel ejection system of the specific embodiment of the invention;
Label declaration:1, motor;2, Flywheel disc;21, main body;22, toothed disc;221, gear;3, capstan winch;31, reel; 311, through-hole;32, bearing;321, outer ring;322, inner ring;33, baffle.
Specific implementation mode
To explain the technical content, the achieved purpose and the effect of the present invention in detail, below in conjunction with embodiment and coordinate attached Figure is explained.
The design of most critical of the present invention is:Coordinate capstan winch by being used cooperatively Multilayer-tooth wheel disc, is not selected in function full In the case of sufficient demand, clutch can be replaced, avoid conventional clutch there is a situation where overheating to occur, it is more durable.
Fig. 1 to Fig. 4, a kind of flywheel ejection system are please referred to, the flywheel ejection system is mounted on ship or needs short On the object of journey ejection, the object includes track, including motor 1, Flywheel disc 2, selector and shuttle;The motor 1 Positioned at the side of Flywheel disc 2, for driving Flywheel disc 2 to rotate, the selector is located at the other end of Flywheel disc 2;It is described Shuttle is located on track;
The Flywheel disc 2 includes main body 21 and Multilayer-tooth wheel disc 22, and the toothed disc 22 is located at main body 21 and gear selection Between device;The main body 21 is a discoid metal derby, and the toothed disc 22 includes the tooth that several radiuses successively successively decrease Wheel 221, one end that 22 gear 221 of the toothed disc is relatively large in diameter is mounted in main body 21, and is co-axially mounted with main body 21;
The selector includes manipulator and several capstan winches 3 compatible with gear 221, and the manipulator is used for Select the operation of the gear 221 on different 3 cooperating teeth wheel discs 22 of capstan winch;
The capstan winch 3 includes reel 31, bearing 32 and stranded cable, and described stranded cable one end is connected on reel 31, and the other end is lived It is dynamic to be connected on shuttle;The reel 31 includes inside and outside, and the inside offers through-hole 311,311 direction of the through-hole The side of Flywheel disc 2 is adapted with gear 221, and the bearing 32 is connected in the other side of through-hole 311;Outside the reel 31 It is additionally provided with groove compatible with stranded cable on surface, and is provided at both ends with baffle 33;The shape and gear of the through-hole 311 221 is corresponding;The bearing 32 includes outer ring 321 and inner ring 322, and the outer ring 321 and 311 phase of interior bone of reel 31 are solid Fixed, the inner ring 322 is the disk of the setting of not rounded straight slot;
The manipulator includes displacement arm and selection arm, and described selection arm one end is fixed in displacement arm, and the other end is then Free end, the free end are adapted with 31 bearing of reel, 32 inner ring, 322 straight slot.
As can be seen from the above description, the course of work of the invention is:The flywheel ejection system, is constantly in working condition, Motor 1 drives Flywheel disc 2 to rotate, and is that Flywheel disc 2 is in a constant rotating speed section, when aircraft needs ejection, incites somebody to action Aircraft is fixed on shuttle, by judging in advance take-off weight, is twisted by the way that the selection arm selection of manipulator is suitable Disk 3, at this time stranded cable one end on capstan winch 3 be connected to shuttle;The moment of transmitting, displacement arm is by the tooth on capstan winch 3 and toothed disc 22 Wheel 221 carries out card and drives capstan winch 3 to rotate by Flywheel disc 2, scrolling stranded cable after driving the aircraft on shuttle to be launched, breaks The connection of shuttle and stranded cable is opened, immediately by shuttle return;Meanwhile the take-off weight of next aircraft is judged, it will roll up After good capstan winch 3 places, carries out new capstan winch 3 and selected.
As can be seen from the above description, the beneficial effects of the present invention are:Coordinate capstan winch by being used cooperatively Multilayer-tooth wheel disc 22 3, in the case where function does not select meet demand, clutch can be replaced, avoiding conventional clutch, there is a situation where overheat Occur, and when war occurs, the structure of the cooperation capstan winch 3 of Multilayer-tooth wheel disc 22 is less likely to be damaged when being hit by a bullet, relative to from Clutch, it is more durable, when some capstan winch 3 or gear 221 are damaged, it can directly use other capstan winches 3 or gear 221 It substitutes, improves operational performance;By the use of multiple capstan winches 3, can follow-through quickly be carried out to multi rack aircraft, met The time demand in wartime.
Further, the capstan winch 3 further includes brake gear, and the brake gear includes clamp and brake disc, the card Pincers are fixed on 32 inner ring 322 of bearing, and the brake disc is fixed on capstan winch 3.
As can be seen from the above description, by using brake gear, it can quickly be braked, be avoided in midway to capstan winch 3 Need groung device take off or after aircraft taken off, stranded cable disengages shuttle, and capstan winch 3 disengages Flywheel disc 2 so that Capstan winch 3 rotates under inertia, by brake gear, capstan winch 3 is made quickly to stop, and promotes working efficiency.
Further, the brake disc includes multiple through-holes 311 and a plurality of water channel, and the through-hole 311 is evenly distributed in On brake disc, the water channel is in array distribution on brake disc.
As can be seen from the above description, by using through-hole 311 and water channel, it can quickly be radiated, avoided to brake disc Because brake disc overheat leads to braking effect difference or brake failure, in wartime, this all may be fatal presence, to be promoted Flywheel ejection system overall performance.
Further, it is connected by umbilical connector between the shuttle and stranded cable.
As can be seen from the above description, shuttle and stranded cable are connected by umbilical connector, it can be in aircraft takeoff success When, today between stranded cable and shuttle is detached from, is avoided because the inertia of capstan winch 3 drives the movement of stranded cable, to drive shuttle Movement, can not brake, lead to the damage of shuttle.
Further, the both sides of the track are also equipped with the electromagnetic path being powered being mutually parallel, the electromagnetism rail Road is electrically connected with shuttle.
As can be seen from the above description, electromagnetic path is installed by the both sides in track, interacts using between track current The Ampere force of generation shuttle is accelerated, the vehicle launch for being fixed on shuttle is gone out;After battery has fired, by inverting electricity Pole can carry out deceleration return to shuttle.
Further, the outer surface of the reel 31 is in truncated cone-shaped, and outer surface is coated with one layer of nano-ceramic powder, The one end fits Flywheel disc 2 being relatively large in diameter when use.
As can be seen from the above description, it is in the reel 31 of truncated cone-shaped by using outer surface, can be suited to speed up and to take off Aircraft, to promote working efficiency;By coating your ceramic powder, stranded cable can be avoided to cause brokenly the surface of reel 31 It is bad, influence using effect.
Further, it is also equipped with reinforcing rib inside the reel 31.
As can be seen from the above description, by installing reinforcing rib, it can ensure that reel 31 is not allowed to be also easy to produce under high load capacity work Deformation, and influence working performance.
Further, the stranded cable includes that clad, at least layer winding layer and wire rope core composition, the winding layer are wrapped in rope On core, the clad is coated on outside winding layer;Winding layer laminated in a manner of spiral coiling is wrapped on wire rope core, and phase The winding direction of adjacent winding layer is opposite.
As can be seen from the above description, by using winding layer, the steam in air, or marine high humility, height are avoided The gas of salinity causes to corrode to wire rope core, avoids in use, and stranded cable is broken the generation for leading to accident.
Further, the wire rope core by 12 strands or 36 bursts of carbon fiber rope twistings or is knitted to form.
As can be seen from the above description, the wire rope core woven by multi-strand carbon fiber rope is capable of providing better load effect, simultaneously When sub-thread wire rope core somewhere being avoided to have flaw, stress is easy to concentrate, and causes service life short, is easy to cause the generation of accident.
Embodiment one
A kind of flywheel ejection system, the flywheel ejection system are mounted on ship or need on the object of short distance ejection, The object includes track, including motor, Flywheel disc, selector and shuttle;The motor is located at the side of Flywheel disc, uses In driving Flywheel disc rotation, the selector is located at the other end of Flywheel disc;The shuttle is located on track;
The Flywheel disc includes main body and Multilayer-tooth wheel disc, and the toothed disc is between main body and selector;Institute It is a discoid metal derby to state main body, and the toothed disc includes the gear that several radiuses successively successively decrease, the toothed disc One end that gear is relatively large in diameter is mounted in main body, and is co-axially mounted with main body;
The selector includes manipulator and several capstan winches compatible with gear, and the manipulator is for selecting The operation of gear on different capstan winch cooperating teeth wheel discs;
The capstan winch includes reel, bearing and stranded cable, and described stranded cable one end is connected on reel, and the other end is movably connected in On shuttle;The reel includes inside and outside, and the inside offers through-hole, and the through-hole is towards the side of Flywheel disc and tooth Wheel is adapted, and the bearing is connected in the other side of through-hole;It is additionally provided on the reel outer surface and is adapted with stranded cable Groove, and be provided at both ends with baffle;The shape of the through-hole is corresponding with gear;The bearing includes outer ring and inner ring, institute It states outer ring and the interior bone of reel is mutually fixed, the inner ring is the disk of the setting of not rounded straight slot;
The manipulator includes displacement arm and selection arm, and described selection arm one end is fixed in displacement arm, and the other end is then Free end, the free end are adapted with reel bearing inner race straight slot.
The capstan winch further includes brake gear, and the brake gear includes clamp and brake disc, and the clamp are fixed on axis It holds on inner ring, the brake disc is fixed on capstan winch.The brake disc includes multiple through-holes and a plurality of water channel, and the through-hole is uniform Be distributed on brake disc, the water channel in array distribution on brake disc.
It is connected by umbilical connector between the shuttle and stranded cable.The both sides of the track are also equipped with mutually flat The capable electromagnetic path being powered, the electromagnetic path are electrically connected with shuttle.
The outer surface of the reel is in truncated cone-shaped, and outer surface is coated with one layer of nano-ceramic powder, diameter when use Larger one end fits Flywheel disc.It is also equipped with reinforcing rib inside the reel.
The stranded cable includes clad, at least layer winding layer and wire rope core composition, and the winding layer is wrapped on wire rope core, described Clad is coated on outside winding layer;Winding layer laminated in a manner of spiral coiling is wrapped on wire rope core, and adjacent winding layer Winding direction it is opposite.The wire rope core is by 12 strands or 36 bursts of carbon fiber rope twistings or is knitted to form.
In conclusion a kind of flywheel ejection system provided by the invention, coordinates capstan winch by being used cooperatively Multilayer-tooth wheel disc, In the case where function does not select meet demand, clutch can be replaced, avoiding conventional clutch, there is a situation where overheat to send out It is raw, and when war occurs, the structure of Multilayer-tooth wheel disc cooperation capstan winch is less likely to be damaged when being hit by a bullet, relative to clutch, It is more durable, when some capstan winch or gear are damaged, it can directly use other capstan winches or gear to substitute, improve and fight Performance;By the use of multiple capstan winches, can follow-through quickly be carried out to multi rack aircraft, meet the time need in wartime It asks.
It by using brake gear, can quickly be braked to capstan winch, avoid needing groung device in midway It takes off or after aircraft taken off, stranded cable disengages shuttle, and capstan winch disengages Flywheel disc so that capstan winch rotates under inertia, leads to Brake gear is crossed, capstan winch is made quickly to stop, promotes working efficiency.
It by using through-hole and water channel, can quickly be radiated, avoided because brake disc overheat causes to brake disc Braking effect difference or brake failure, in wartime, this all may be fatal presence, to promote flywheel ejection system globality Energy.
Shuttle and stranded cable are connected by umbilical connector, it can be in aircraft takeoff success, by stranded cable and shuttle Between today be detached from, avoid because capstan winch inertia drive stranded cable movement can not brake, lead to drive the movement of shuttle Cause the damage of shuttle.
Electromagnetic path is installed by the both sides in track, it will using the Ampere force of the generation to interact between track current Shuttle accelerates, and the vehicle launch for being fixed on shuttle is gone out;After battery has fired, by invert electrode, can to shuttle into Row deceleration return.
It is in the reel of truncated cone-shaped by using outer surface, the aircraft to take off can be suited to speed up, to promote work Make efficiency;By coating your ceramic powder, stranded cable can be avoided to damage the surface of reel, influence using effect.
It by installation reinforcing rib, can ensure that reel is not allowed to be also easy to produce deformation under high load capacity work, and influence workability Energy.
By using winding layer, avoid the steam in air, or marine high humility, high salinity gas to wire rope core It causes to corrode, avoid in use, stranded cable is broken the generation for leading to accident.
The wire rope core woven by multi-strand carbon fiber rope is capable of providing better load effect, while avoiding sub-thread wire rope core When there is flaw at place, stress is easy to concentrate, and causes service life short, is easy to cause the generation of accident.
Example the above is only the implementation of the present invention is not intended to limit the scope of the invention, every to utilize this hair Equivalents made by bright specification and accompanying drawing content are applied directly or indirectly in relevant technical field, include similarly In the scope of patent protection of the present invention.

Claims (9)

1. a kind of flywheel ejection system, the flywheel ejection system is mounted on ship or needs on the object of short distance ejection, institute It includes track to state object, which is characterized in that including motor, Flywheel disc, selector and shuttle;The motor is located at Flywheel disc Side, for driving Flywheel disc to rotate, the selector is located at the other end of Flywheel disc;The shuttle is located at track On;
The Flywheel disc includes main body and Multilayer-tooth wheel disc, and the toothed disc is between main body and selector;The master Body is a discoid metal derby, and the toothed disc includes the gear that several radiuses successively successively decrease, tooth on the toothed disc The larger one end of wheel diameter is mounted in main body, and is co-axially mounted with main body;
The selector includes manipulator and several capstan winches compatible with gear, and the manipulator is for selecting difference Capstan winch cooperating teeth wheel disc on gear operation;
The capstan winch includes reel, bearing and stranded cable, and described stranded cable one end is connected on reel, and the other end is movably connected in shuttle On;The reel includes inside and outside, and the inside offers through-hole, and the through-hole is towards the side of Flywheel disc and gear phase Adaptation, the bearing are connected in the other side of through-hole;It is additionally provided on the reel outer surface compatible with stranded cable recessed Slot, and it is provided at both ends with baffle;The shape of the through-hole is corresponding with gear;The bearing includes outer ring and inner ring, described outer It encloses and is mutually fixed with the interior bone of reel, the inner ring is the disk of the setting of not rounded straight slot;
The manipulator includes displacement arm and selection arm, and described selection arm one end is fixed in displacement arm, and the other end is then freely End, the free end is adapted with reel bearing inner race straight slot.
2. flywheel ejection system according to claim 1, which is characterized in that the capstan winch further includes brake gear, described Brake gear includes clamp and brake disc, and the clamp are fixed on bearing inner race, and the brake disc is fixed on capstan winch.
3. flywheel ejection system according to claim 2, which is characterized in that the brake disc includes multiple through-holes and a plurality of Water channel, the through-hole are evenly distributed on brake disc, and the water channel is in array distribution on brake disc.
4. flywheel ejection system according to claim 1, which is characterized in that by taking off automatically between the shuttle and stranded cable Fall connector connection.
5. flywheel ejection system according to claim 1, which is characterized in that the both sides of the track are also equipped with mutually flat The capable electromagnetic path being powered, the electromagnetic path are electrically connected with shuttle.
6. flywheel ejection system according to claim 1, which is characterized in that the outer surface of the reel is in truncated cone-shaped, And outer surface is coated with one layer of nano-ceramic powder, the one end fits Flywheel disc that when use is relatively large in diameter.
7. flywheel ejection system according to claim 1, which is characterized in that be also equipped with reinforcing rib inside the reel.
8. flywheel ejection system according to claim 1, which is characterized in that the stranded cable includes that clad, at least layer twine Winding layer and wire rope core composition, the winding layer are wrapped on wire rope core, and the clad is coated on outside winding layer;The winding layer is with spiral shell Rotating coiling mode laminated is wrapped on wire rope core, and the winding direction of adjacent winding layer is opposite.
9. flywheel ejection system according to claim 8, which is characterized in that the wire rope core is by 12 strands or 36 strands of carbon Cordage twisting is knitted to form.
CN201711339676.3A 2017-12-14 2017-12-14 A kind of flywheel ejection system Pending CN108557107A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711339676.3A CN108557107A (en) 2017-12-14 2017-12-14 A kind of flywheel ejection system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711339676.3A CN108557107A (en) 2017-12-14 2017-12-14 A kind of flywheel ejection system

Publications (1)

Publication Number Publication Date
CN108557107A true CN108557107A (en) 2018-09-21

Family

ID=63529344

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201711339676.3A Pending CN108557107A (en) 2017-12-14 2017-12-14 A kind of flywheel ejection system

Country Status (1)

Country Link
CN (1) CN108557107A (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104097786A (en) * 2014-07-09 2014-10-15 吴炳选 Mechanical catapult for carrier-based aircraft
CN105151311A (en) * 2015-03-31 2015-12-16 北京道永科技有限公司 Catapult-assisted take-off device of aircraft and aircraft carrier

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104097786A (en) * 2014-07-09 2014-10-15 吴炳选 Mechanical catapult for carrier-based aircraft
CN105151311A (en) * 2015-03-31 2015-12-16 北京道永科技有限公司 Catapult-assisted take-off device of aircraft and aircraft carrier

Similar Documents

Publication Publication Date Title
JP6271420B2 (en) Dual-mode fiber optic cable system for remotely operated underwater work equipment
CN201927943U (en) Onboard electric stringing device for unmanned air vehicle
CN202499283U (en) Flywheel ejector
CN103482077A (en) Variable-torque electromagnetic damping type carrier-based aircraft landing arrester
CN111926878A (en) Synchronous electric loader of cable winch
CN105329408A (en) Marine anchor
CN108557107A (en) A kind of flywheel ejection system
CN206606366U (en) The device of two-level spring joint ejection carrier-borne aircraft
CN102040006A (en) Aircraft carrier ejector
US2659192A (en) Stranding machine
US4555898A (en) Apparatus for stranding armor wires about a cable core, and method implemented by the apparatus
CN104996373B (en) The special longline fishing fishing machine of fishing boat
CN105584639B (en) A kind of integrated disc type carrier landing stopping device and its method for arresting with clutch
CN106629251A (en) Pulling and coiling device
CN207503730U (en) A kind of stranded wire apparatus
CN105584638A (en) Integrated disc-type carrier aircraft landing arresting device and arresting method thereof
CN106169264B (en) Simulated training system is blocked in aircraft carrier ejection
CN102254633A (en) Conducting wire back-twisting mechanism of cabling device
CN107516561B (en) Cabling machine
CN109720941A (en) A kind of Wound-rotor type automatic deploying and retracting line mechanism
CN207009157U (en) A kind of cage winch stranded wire apparatus with protection mechanism
CN201749740U (en) Cantilevering single-twist machine
JP7074733B2 (en) Ship
CN104176266A (en) Winding dragging and take-off accelerating device for shipboard aircraft of aircraft carrier
CN115071435A (en) Energy storage control system and control method for pure electric vehicle

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
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20180921

WD01 Invention patent application deemed withdrawn after publication