56 results about "Skin opening" patented technology

The invention relates to a method for creating a puncture wound for obtaining a sample of a body fluid from a body part in which a skin opening is created at a puncture site in the epidermis in a skin-opening step. Then, in a sample collection step a sample collection puncture is executed by using a puncture element with which the skin opening is deepened with the puncture element, thereby creating a puncture wound for obtaining the sample. The invention also relates to a handheld apparatus for implementing this method.

Described herein are systems, apparatus, and methods for precise placement and guidance of tools during surgery, particularly spinal surgery, using minimally invasive surgical techniques. Several minimally invasive approaches to spinal surgeries were conceived, percutaneous technique being one of them. This procedures looks to establish a skin opening as small as possible by accessing inner organs via needle-puncture of the skin. The percutaneous technique is used in conjunction with a robotic surgical system to further enhance advantages of manual percutaneous techniques by improving precision, usability and/or shortening surgery time by removal of redundant steps.

The invention discloses a cable stripping device. The device comprises a machine body base, an upper bracket, a guiding mechanism, a skin opening mechanism, a skin expanding mechanism, a peeling mechanism and a controller. The guiding mechanism, the skin opening mechanism, the skin expanding mechanism and the peeling mechanism are fixedly connected with the upper bracket and the machine body baseseparately; the guiding mechanism and the skin opening mechanism are controlled by the controller to work. When the stripping device works, after a cable passes through the guiding mechanism, the skinopening mechanism, the skin expanding mechanism and the peeling mechanism, a cable sheath is completely separated from a cable core. According to the stripping device, a wire diameter detecting device is arranged on the guiding mechanism, the controller adjusts the structure of the skin opening mechanism according to wire diameter parameters, the skin opening thickness is adjustable, and after skin opening is conducted on the cable, under the functions of the skin expanding mechanism and the peeling mechanism, the cable core is automatically stripped off from the cable sheath, so that automatic stripping operation of the cable is completed, and the cable stripping device is suitable for stripping operation of cables different in cable diameter.

An external fixation assembly includes a plurality of hollow pins that are inserted into a patient's bone. Each pin has an interior bore and a plurality of apertures extending through the pin wall from the bore. The pin may be coupled to a source of vacuum pressure operable to create reduced pressure in the tissue surrounding the pin. A cover is placed around the pin and sealed to provide a fluid-tight enclosure that maintains reduced pressure around the pin. A method for applying external fixation using the fixator pins described above includes the steps of inserting each pin through a skin opening, positioning the pin apertures near selected tissue, covering the skin opening with a sealed enclosure, connecting the pins to a source of vacuum pressure, and activating the source of vacuum pressure to create reduced pressure in the patient's tissue at or near the bone.

First House II is a self regulating, solar powered, air cycle machine. Thermo radiation and photovoltaic conversion interact proportionally to moderate [climatic] extremes. It incorporates the natural cycles for water, waste, garbage, household dirt and for air purification.

The interior cantilever post and beam skeleton, with innovative joinery, is sheathed in rigid non-biodegradable skin to form a permanent, low maintenance structure.

The interior and exterior geometry for radiant energy absorption also utilizes skin openings, temperature and pressure differentials to control air quality and flow. [Openings for doors], windows and holes are precision cut from the skin and [then] reinstalled to prevent unintentional convection, conduction or radiant energy loss.

Pre-manufactured interchangeable parts permit phased construction or expansion with no onsite waste or refuse. Structural materials are multifunctional and provide capabilities for energy independence with no need for municipal services over its unlimited service life.

For producing a skin opening for minimally invasive surgery an instrument is employed, comprising a grip (10) and a puncture awl (16). The puncture awl (16) is provided on the distal end of a grip (10), which distal end forms a stop surface (12), which limits the penetration depth of the puncture awl (16).

The invention relates to a peel opening device, in particular to a peel opening device for making dried tangerine peels from oranges. The technical problem to be solved is to provide the peeling opening device for making the dried tangerine peels from the oranges without manually peeling the oranges by people. According to the technical scheme, the peel opening device for making the dried tangerine peels from the oranges comprises: a fixing plate and a first fixing frame, and the first fixing frame is arranged in the middle of the fixing plate; the second fixing frame that is arranged on the fixing plate; the skin opening mechanism that is arranged on the fixing plate; and the feeding mechanism that is arranged on the first fixing frame. Through the arrangement of the clamping mechanism, a second sliding rod can better fix an orange under the action of a third spring, and the orange can be conveniently cut and peeled by a cutter; and by arranging the intermittent mechanism, the first rotating disc does not need to be manually controlled by people to rotate, and intermittent rotation of the first rotating disc is achieved.

The invention discloses a multifunctional cabin door ventilation opening device controlled through a cam. The device is provided with a cover plate arranged on a cabin door skin opening, wherein a rocking arm is arranged on the cover plate; a limiting component matched with the rocking arm is arranged at the front end of the rocking arm; the rear end of the rocking arm is fixedly connected to a rotating shaft component; the rotating shaft component is mounted on a supporting lug I and a supporting lug II; a rotating shaft is arranged at one edge on the periphery of the cabin door skin opening; a rocking arm lug I and a rocking arm lug II are respectively arranged at the two ends of the rotating arm component; one end of the rocking arm lug I and one end of the rocking arm lug II are respectively articulated with the two ends of the rotating shaft component; the other end of the rocking arm lug I and the other end of the rocking arm lug II are respectively articulated with the two ends of the rotating shaft; a driving pull rod is further arranged at the rear end of the rocking arm; one end of the driving pull rod is connected with the rear end part of the rocking arm; the other end of the driving pull rod extends to the driving part of the cam. The device realizes physical pressure relief in the condition that a cabin door is not completely closed, meanwhile realizes locking in the air during flight, and provides a low-cost and high-reliability solution for civil aircrafts.

The invention discloses a simple covering cap structure for a flexible skin opening of a solar unmanned aerial vehicle, and designs a carbon fiber simple covering cap structure aiming at the characteristic that the solar unmanned aerial vehicle in a near space adopts a flexible film as a film covering material. The simple covering cap structure is provided with upper, middle and lower layers of carbon sheets, and the three layers of carbon sheets are bonded and fixed; holes are formed in the three layers of carbon sheets, the holes in the middle layer are designed to be slightly larger, and gaps are formed between the upper and lower layers of carbon sheets. Furthermore, the covering cap is designed to be inserted into the hole of the middle layer, rapid disassembly and assembly of the covering cap are completed by simply pushing, pulling and rotating the covering cap, and the designed covering cap can be perfectly attached to the flexible skin and is extremely light in weight. The simple covering cap structure can be widely applied to the simple opening structure of the flexible skin.

The invention discloses a degradable skin expander. The skin expander comprises a bag which has the tissue regeneration inducing function and is made of an absorbable medical membrane; the absorbablemedical membrane is mainly made from degradable polyurethane, in the skin opening process, cells are promoted to crawl and grow through a membrane support to form incremental skin, and the skin expander can be used for skin grafting and scar repair. The skin expander has the advantages of being fast in skin growth, low in infection rate and high in wound healing speed, and no second operation is needed for removing the skin expander.

The invention belongs to the technical field of aircraft structures and relates to a quickly-disassembled rotary opening cover lock. The quickly-disassembled rotary opening cover lock comprises a lock seat, a lock tongue, a special-shaped pin, a spring and a steel ball. The lock tongue is connected to the lock seat through the special-shaped pin. The steel ball and the squeezed spring are installed in an annular groove of the lock seat. One side of the steel ball abuts against a groove of the lock tongue, and the other side of the steel ball makes contact with the squeezed spring. According to the quickly-disassembled rotary opening cover lock, an opening cover can be quickly opened and locked, the size of a lock body is small, and meanwhile the damage to the structure of the opening cover is small; the quickly-disassembled rotary opening cover lock can be applied to aircraft bodies, missile pylons and other skin opening covers.

The invention discloses an aircraft hardpoint sealing mechanism driven by motors. The aircraft hardpoint sealing mechanism comprises a casing (1), wherein a hanging frame hole (12) is formed in the casing (1), and two sealing plates (9) matched with the casing (1) in a rotating manner are mounted on the bottom surface of the outer sides of the casing (1) respectively and positioned on two sides of the hanging frame hole (12) respectively; a step motor (2) driving the sealing plates (9) to rotate and two opposite-transmitting type infrared sensors (4) positioned on two sides of the hanging frame hole (12) respectively are mounted on the inner side surface of the casing (1). The aircraft hardpoint sealing mechanism disclosed by the invention is simple in structure and convenient to use, when a hanging frame is mounted, the sealing plates are opened through a switch by ground staff, then the sealing plates are held in an open state, and when the hanging frame is released, the sealing mechanism is automatically closed, so that the aircraft hardpoint sealing mechanism is relatively convenient to use; because space for the sealing plates does not need to be reserved in the inner part of the casing, and plan view sizes of the sealing mechanism and a corresponding skin opening are small and slightly greater than sizes of the hanging frame, so that influence on the structural strength of the aircraft is small.

The invention belongs to the technical field of food, and particularly relates to flour special for dumplings and a preparing method thereof. Basic powder of the dumplings is prepared from, by mass, 5% of Jinan 17, 5% of Jining 16, 20% of 02-1 wheat, 20% of new wheat 26, 10% of 5766 and 40% of Canada wheat; the adding amount of salt accounts for 1% of the basic powder of the dumplings. According to the flour special for the dumplings and the preparing method thereof, all kinds of original wheat are compounded in proportion, any food additive is not required to be added into the dumpling flourprepared with the method, and prepared flour skins have good extensibility; dumplings made with the flour special for the dumplings are not prone to skin opening or skin breaking or soup muddying in the boiling process, and the boiled dumplings are put for a section of time and cannot be boned; noodle soup is clear and free of precipitation, the dumpling skins are pure white, bright, glossy and soft, and the dumplings are fine and smooth in taste, tasty and refreshing, and are not capable of sticking teeth and chewy during tasting.

The invention discloses a magnolia denudata grafting-planting method. The magnolia denudata grafting-planting method comprises the following steps that 1, stock treatment is performed, wherein movablemagnolia denudate which do not grow and have the height of 20 cm or below are selected as stocks, the grafting parts, having the diameter of 1 cm, of stock joints are sheared off, and the centers ofthe grafting parts are longitudinally hacked one time or crossly hacked two times; 2, cion treatment is performed, wherein each red-flower magnolia denudate branch with one or two full axillary buds is selected as a cion, and the bottom of each cion is cut into two cut faces identical in length; 3, grafting is performed, wherein the skin opening of each stock is prized up by using a cutter, and the cions are inserted into the stocks, the butt joint positions of the cions and the stocks are wrapped by using grafting films from bottom to top, binding is performed by adopting plastic ropes, and bed leaves are exposed in the outside. The magnolia denudata grafting-planting method is simple in operation, high in efficiency and high in survival rate, and the planting efficiency is improved.