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43results about How to "Shorten arm length" patented technology

All-optical logic gate with Michelson structure

The invention relates to an all-optical logic gate with a Michelson structure, which can be reused for realizing an AND gate, an OR gate, an NOT gate, an NAND gate, an NOR gate, an XOR gate and an XNOR gate as well as the reverse operation thereof, and also realizing a half-adder. The all-optical logic gate with a Michelson structure comprises two control optical signals, a synchronous optical detection signal and an output detection signal, wherein the two control optical signals are input into an arm (2) of symmetrical Michelson interferometers by a coupler (1); the synchronous optical detection signal is divided into two beams of equal light to be projected into the arm (2) and an arm (3) of the Michelson interferometers and used for outputting a reflecting output opening (4) for expressing the application of the logic result and a transmitting output opening (5) of the reverse operation; the output detection signal is results of the self-phase modulation of a detection optical signal, the intersection phase modulation of the two control optical signals on detection light and average intersection phase modulation on the detection light in two times of arm length and is expressed into a corresponding logic gate relation. The all-optical logic gate has the characteristic of self-phase modulation in the symmetrical Michelson interferometers, preferably the two arms adopt different nonlinear optical fibers and the input arm (2) of the control optical signals adopts a high nonlinear optical fiber.
Owner:UNIV OF ELECTRONICS SCI & TECH OF CHINA

Double-layered eight-rotor-wing unmanned aerial vehicle

The invention discloses a double-layered eight-rotor-wing unmanned aerial vehicle which comprises a body, four upper arms, four lower arms and eight flying mechanisms. The body comprises an upper platform and a lower platform; the four upper arms and the four lower arms are separately arranged on the upper platform and the lower platform; each of the lower arms comprises a first connecting rod, a folding mechanism and a second connecting rod which are successively connected; the eight flying mechanisms are separately arranged on the tail ends of the four upper arms and the four lower arms; each of the flying mechanisms comprises a brushless motor and a rotor wing fixedly connected to the output shaft of the brushless motor; and the rotating ranges of the rotor wings of the eight flying mechanisms are staggered for generating upward lift forces. By adopting a double-layered structure, the arm length of a common eight-rotor-wing unmanned aerial vehicle is reduced, the weight of the structure is alleviated, and the storage space is expanded; meanwhile, the double-layered eight-rotor-wing unmanned aerial vehicle is more stable to control, longer in time of endurance and higher in efficiency, and the safety of inner loads of the body is effectively guaranteed.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

Power thermocouple conversion element with long-range concentrated cooling mode

The invention discloses a power thermocouple conversion element with a long-range concentrated cooling mode and especially relates to a structure that has a longitudinal extension form and has a high temperature section, a boundary section, and a cooling section. The high temperature section is direction arranged in a heat source; a boundary section is delimitation between the heat source and a cold source; and the cooling section is arranged in the cold source. The whole element is packaged by a protection housing. A thermocouple set, a metal flow deflector and an electrothermal circuit are arranged in the thermocouple conversion element, wherein the thermocouple set are first in parallel connection and then is in series connection as well as the electrothermal circuit is connected with a transition conductor; and all cold junction nodes of the electrothermal circuit are concentrated at the cooling section of the thermocouple conversion element for cooling. According to the invention, a heat transfer process and a cooling process of a thermocouple conversion element are reinforced, so that it is beneficial to fully utilize energies of a heat source as well as to improve an outputpower and reduce costs; moreover, it is also beneficial to design and develop a compact thermoelectric conversion apparatus and to improve a power density index.
Owner:SOUTH CHINA UNIV OF TECH

Air spring three-way composite loading fatigue test device and method

ActiveCN108801622BAccurately reflect fatigueCheck fatigue lifeMachine part testingAir springGas spring
The invention provides an air spring three-way compound loading fatigue test device and method. The device comprises a support and is characterized by also comprising a transverse loading assembly forapplying a transverse dynamic load to an air spring, a vertical loading assembly for applying a vertical dynamic load to the air spring and a longitudinal biasing assembly for enabling the air springto generate longitudinal deformation, wherein the transverse loading assembly is arranged on the support in the forward and backward directions of the air spring; the longitudinal biasing assembly isarranged on the transverse loading assembly, and the locating position of the longitudinal biasing assembly on the transverse loading assembly can be adjusted; the air spring is arranged on the longitudinal biasing assembly; and the vertical loading assembly is arranged above the air spring in the vertical direction and is in contact with the air spring. The device and the method provided by theinvention can simulate the bearing condition in the actual operating condition of the air spring, accurately reflect the fatigue performance of the air spring and detect the fatigue life of the air spring, thereby providing reliable and accurate test processes and data for optimizing the structure of the air spring.
Owner:ZHUZHOU TIMES NEW MATERIALS TECH +1
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