6results about "Supports/holding devices" patented technology

According to the invention, a seating device, in particular an aircraft seating device, for mounting in an aircraft, comprises a mounting unit (14a; 14b) having two spaced-apart seat feet (16a, 18a; 16b, 18b), a seat base (30a; 30b) having a seat floor (32a; 32b) and a backrest (34a; 34b), wherein the seat base (30a; 30b) is connected to the two seat feet (16a, 18a; 16b, 18b) in side regions (36a, 38a; 36b, 38b), and a bearing unit (40a; 40b) which pivotably connects the seat base (30a; 30b) to the seat feet (16a, 18a; 16b, 18b) in an upper region. attaches and with which the seat base (30a; 30b) can be pivoted between an upright sitting position and a maximum comfort position, with a locking device (42a; 42b) which is intended to secure the seat base (30a;30b) to lock at least in the upright sitting position and in the comfort position, wherein the locking device (42a; 42b) has at least one actuator (44a; 44b) which is attached below the seat base (32a; 32b) of the seat body (30a; 30b) and is designed to assist an adjustment of the seat body (30a; 30b) towards the comfort position, is proposed.;

The utility model relates to the field of aviation technology, concretely relates to a novel airplane seat with double functions of shock absorption and anti-crash, which comprises a seat back, a seat cushion and an energy absorption structure, the seat back is connected with the seat cushion, the energy absorption structure comprises horizontal wave springs, vertical wave springs and a partition, the horizontal wave springs comprise a plurality of wave spring units stacked together, each wave spring unit is composed of two wave-shaped plate bodies stacked and fixed, and each wave-shaped plate body is a continuous sinusoidal structure, the utility model integrates the functions of shock absorption and anti-crash in the same seat structure, in daily flight, the seat realizes the shock absorption function through the energy absorption structure, effectively buffers the vibration and improves the comfort of passengers, in a crash accident, the energy absorption structure absorbs energy and buffers through deformation, significantly reduces the impact force on passengers and improves the safety performance and applicable scenarios of the seat.

The invention relates to an aircraft seating device, in particular an aircraft pilot seating device, for mounting in an aircraft, comprising a mounting unit (14a; 14b) having two spaced-apart seat feet (16a, 18a; 16b, 18b), a seat base (30a; 30b) having a seat floor (32a; 32b) and a backrest (34a; 34b), wherein the seat base (30a; 30b) is connected to the two seat feet (16a, 18a; 16b, 18b) in side areas (36a, 38a; 36b, 38b), and a height adjustment device (100a; 100b) by means of which the seat base (30a; 30b) can be adjusted in height on the seat feet (16a, 18a; 16b, 18b). 18a; 16b, 18b) is attached.It is proposed that the height adjustment device (100a; 100b) has a gear unit (102a; 102b) by means of which the seat base (30a; 30b) can be continuously adjusted between a lower position and an upper position, wherein the gear unit (102a; 102b) has at least one adjustment gear (104a, 106a; 104b, 106b) which is functionally arranged between the seat base (30a; 30b) and the stand unit (14a; 14b).

The invention relates to an aircraft seat device, in particular an aircraft pilot seat device, for mounting in an aircraft, comprising a stand unit (14a; 14b), which has two mutually spaced seat feet (16a, 18a; 16b, 18b); a seat main part (30a; 30b), which has a seat base (32a; 32b) and a backrest (34a; 34b), the seat main part (30a; 30b) being connected, in lateral regions (36a, 38a; 36b, 38b), to the two seat feet (16a, 18a; 16b, 18b); and a height adjustment device (100a; 100b), by means of which the seat main part (30a; 30b) is attached to the seat feet (16a, 18a; 16b, 18b) at an adjustable height. According to the invention, the height adjustment device (100a; 100b) has a gear unit (102a; 102b), by means of which the seat main part (30a; 30b) can be continuously adjusted between a lower position and an upper position, the gear unit (102a; 102b) having at least one adjustment gear (104a, 106a; 104b, 106b) which is functionally positioned between the seat main part (30a; 30b) and the stand unit (14a; 14b).

The invention relates to a seat device, in particular an aircraft seat device, for mounting in an aircraft, comprising a stand unit (14a; 14b), which has two mutually spaced seat feet (16a, 18a; 16b, 18b); a seat main part (30a; 30b), which has a seat base (32a; 32b) and a backrest (34a; 34b), the seat main part (30a; 30b) being connected, in lateral regions (36a, 38a; 36b, 38b), to the two seat feet (16a, 18a; 16b, 18b); a bearing unit (40a; 40b) which pivotally connects the seat main part (30a; 30b), in an upper region, to the seat feet (16a, 18a; 16b, 18b) and by means of which the seat main part (30a; 30b) can be pivoted between an upright sitting position and a maximum comfort position; and a locking device (42a; 42b), which is designed to lock the seat main part (30a; 30b) at least in the upright sitting position and in the comfort position, the locking device (42a; 42b) having at least one actuator (44a; 44b), which is connected below the seat base (32a; 32b) of the seat main part (30a; 30b) and is designed to support an adjustment of the seat main part (30a; 30b) in the direction of the comfort position.

The application discloses a wearable three-cascade power single-person aircraft, which comprises a power system, an avionics system, a man-machine interaction system, a safety lifesaving system and a wearable fuselage; the power system adopts a three-cascade aerodynamic layout and is arranged in a triangle shape, wherein the two cascade units on the front side are arranged on the left and right sides of the wearable aircraft body at the same height, and the cascade unit on the back side is arranged at a height higher than that of the cascade units on the front side; the man-machine interaction system is arranged on the left side of the wearable fuselage and the head of the human body, and is used for manually controlling flight and monitoring flight state; and the safety lifesaving system is arranged on the upper part of the wearable fuselage and is used for guaranteeing the safety of the personnel in an emergency. The aircraft has the characteristics of compact structure, high stability, simple operation and good safety.