Flying body safety belt device

Abstract

The utility model discloses a flying body safety belt device. The flying body safety belt device comprises a retractor, the retractor is connected with a shoulder strap, the shoulder strap is arranged in a herringbone structure, two sides of the bottom of the shoulder strap are connected with a waist belt, a lock catch part is installed between the waist belts on two sides, a waist belt adjuster is installed in the middle of the waist belt, and a fixing piece part is installed on the outer side of the waist belt. When an emergency situation occurs, a passenger can be firmly fixed on the seat, the passenger is prevented from being injured due to inertia, the safety and comfort in the flying process are greatly improved, it can be guaranteed that the safety belt can be conveniently pulled out and retracted under the normal situation, and the situation that the passenger feels uncomfortable due to the fact that the safety belt is too loose or too tight is avoided; the safety belt can be quickly locked in case of emergency, so that the safety of personnel is guaranteed, and the safety performance required by aerospace standard regulations is met.

Description

TECHNICAL FIELD

[0001] The utility model belongs to the technical field of flight body safety belt, specifically relates to a flight body safety belt device. BACKGROUND

[0002] With the rapid development of low-altitude flight economy, the safety belt currently used on the flight body is still the traditional four-point safety belt, which is composed of two shoulder straps and two waist straps, mainly plays a basic fixing role, prevents personnel from being thrown off the seat during the movement of the aircraft, the binding feeling of the body is strong, the comfort is poor, long-time use can make the user feel uncomfortable in the shoulder, chest and waist, passengers are easily injured by inertia when the aircraft takes off and lands and encounters airflow turbulence, passengers cannot be effectively protected from serious injury, therefore, a flight body safety belt device is urgently needed to solve the above problems. SUMMARY

[0003] In view of the problems in the above background art, the purpose of the utility model is to provide a flight body safety belt device.

[0004] To achieve the above technical purpose, the utility model adopts the following technical scheme:

[0005] A flight body safety belt device, comprising a winder, the winder is connected with a shoulder strap, the shoulder strap is arranged in a herringbone structure, the bottom of the shoulder strap is connected with a waist strap on both sides, a lock buckle part is installed between the waist straps on both sides, a waist strap adjuster is installed at the middle position of the waist strap, and a fixed sheet part is installed on the outside of the waist strap.

[0006] Further limited, the winder is provided with an inertial sensor. Such a structure design is convenient for checking abnormal acceleration change and improving safety.

[0007] Further limited, the winder comprises a frame, a mandrel is movably installed in the frame, the shoulder strap is arranged on the mandrel, a coil spring part is installed on one side of the frame, the coil spring part is connected with one side of the mandrel, a pawl is installed on the other side of the mandrel, the pawl is connected with a ratchet part, the ratchet part is connected with an inertial block, a belt inductance spring is installed on one side of the inertial block, a mechanical cover is connected with the other side of the belt inductance spring, and the mechanical cover is installed on the other side of the frame. Such a structure design is convenient for locking the shoulder strap, so as to firmly fix the passenger on the seat.

[0008] Further limited, the shoulder strap and the waist strap are fixedly connected through fixed sewing. Such a structure design is convenient for realizing fixed connection.

[0009] Further limited, the waistband includes a first waistband and a second waistband, the lock buckle component is installed between the first waistband on both sides, the shoulder strap fixing sewing is installed on the first waistband, the waistband adjuster is installed between the first waistband and the second waistband, and the fixed sheet component is installed on the second waistband. Such structure design is convenient for adjusting the waistband according to the body shape, and improves the comfort of use.

[0010] The utility model discloses the beneficial effect that:

[0011] 1. Provide better restraint effect, when the flying body encounters complex conditions such as bump, rapid acceleration, rapid deceleration or roll, this safety belt passes through the fixing point of double shoulder belt and double waistband, and passenger is firmly fixed on the seat, compared with traditional three-point safety belt, can more effectively limit the displacement of passenger's body, reduce the risk of passenger's injury due to inertia and forward, side turn or be thrown off the seat;

[0012] 2. Enhance safety, when the safety belt braid is quickly pulled, the retractor 1 will immediately lock the shoulder belt 2, and the passenger is firmly fixed on the seat, to prevent the passenger from being injured due to inertia, and the shoulder belt 2 and the waistband 3 are distributed on the shoulder and the hip of the human body, can better disperse the impact force, avoid the local serious injury caused by the excessive force of single point, like avoiding the safety belt to generate excessive compression to the fragile parts such as abdomen and cause serious injury;

[0013] 3. Improve comfort, since the retractor can adjust the tightness of the safety belt, can ensure that the safety belt maintains appropriate length when normally used, neither too long to make personnel activity range too large to affect flight safety, nor too short to limit necessary operation of personnel, in the flight process, the body of personnel can have a certain degree of activity space, such as slightly changing the sitting posture, stretching the hand to operate the instrument, and the like, and will not be too tight like traditional safety belt, improve the comfort when riding or operating the flying body. BRIEF DESCRIPTION OF DRAWINGS

[0014] The utility model can be further illustrated by the non-limiting embodiment shown in the accompanying drawings;

[0015] Figure 1 It is a structure schematic view of the flying body safety belt device of the utility model embodiment;

[0016] Figure 2 It is an explosion structure schematic view of the retractor of the flying body safety belt device of the utility model embodiment;

[0017] Figure 3 It is an explosion structure schematic view of the waistband of the flying body safety belt device of the utility model embodiment;

[0018] The main element symbol is explained as follows:

[0019] 1. Retractor; 2. Shoulder strap; 3. Waist belt; 4. Buckle assembly; 5. Waist belt adjuster; 6. Fixing plate assembly; 7. Frame; 8. Spindle; 9. Coil spring assembly; 10. Pawl; 11. Ratchet assembly; 12. Inertia block; 13. Belt spring; 14. Mechanical cover; 15. First waist belt; 16. Second waist belt. Detailed Implementation

[0020] To enable those skilled in the art to better understand this utility model, the technical solution of this utility model will be further described below in conjunction with the accompanying drawings and embodiments.

[0021] Example 1, such as Figure 1 As shown, a flight safety harness device includes a retractor 1 connected to a shoulder strap 2, the shoulder strap 2 being arranged in a herringbone shape, a waist belt 3 connected to the bottom two sides of the shoulder strap 2, a buckle component 4 installed between the two waist belts 3, a waist belt adjuster 5 installed in the middle of the waist belt 3, and a fixing piece component 6 installed on the outer side of the waist belt 3.

[0022] In this embodiment, when the aircraft encounters an emergency, such as rapid acceleration, deceleration, turbulence, or airflow impact, the retractor 1 will immediately lock the shoulder strap 2, preventing the shoulder strap 2 from being pulled out further, thus firmly securing the passenger to the seat and preventing injury to the passenger due to inertia, greatly improving safety and comfort during flight.

[0023] The seat belt adjuster 5 and retractor 1 can adjust the length and tightness of the seat belt according to the user's body size and clothing to ensure that the seat belt provides a reliable fixation effect without making the user feel overly restricted, thereby improving comfort.

[0024] This seatbelt securely fastens the user to the seat via a retractor 1 (shared by both shoulder straps) and two fixing components 6 (two at the hips). This method effectively restricts the user's body movement in all directions, whether forward, backward, left, right, or upward. When the aircraft accelerates, decelerates, turns, bumps, or encounters airflow, it prevents the user from slipping off the seat or colliding with surrounding objects. Furthermore, in the event of an emergency, such as sudden braking (which may occur during aircraft landing) or a collision, this seatbelt can evenly distribute the impact force on the body to the shoulder straps 2 and lap belts 3, providing particularly effective protection for the upper body.

[0025] Example 2, as Figure 1 As shown, this embodiment adds the following structure to the embodiment 1: an inertial sensor is installed inside the retractor 1.

[0026] In this embodiment, by setting the inertial sensor, when the flying body encounters an emergency situation, such as sudden acceleration, deceleration, jolt or encounters airflow impact, the inertial sensor in the retractor 1 can quickly detect abnormal acceleration change, and once the acceleration reaches the set threshold, the shoulder belt 2 will be immediately locked, so that the shoulder belt 2 cannot continue to be pulled out, and the passenger is firmly fixed on the seat, improving the safety of use.

[0027] As shown in Embodiment 3, Figure 2 The retractor 1 includes a frame 7, a mandrel 8 movably mounted in the frame 7, the shoulder belt 2 arranged on the mandrel 8, a coil spring component 9 mounted on one side of the frame 7, the coil spring component 9 connected to one side of the mandrel 8, a pawl 10 mounted on the other side of the mandrel 8, a ratchet component 11 connected to the pawl 10, an inertia block 12 connected to the ratchet component 11, a spring 13 mounted on one side of the inertia block 12, a mechanical cover 14 connected to the other side of the spring 13, and the mechanical cover 14 mounted on the other side of the frame 7.

[0028] In this embodiment, when the shoulder belt 2 is quickly pulled, the inertia block 12 moves relative to the ratchet component 11, and the inertia overcomes the resistance of the spring 13 to trigger the ratchet component 11 to lock the internal gear of the mechanical cover 14, thereby driving the pawl 10 to eccentrically move and lock with the gear of the frame 7, stopping the movement of the mandrel 8 and blocking the shoulder belt 2, thereby preventing the shoulder belt 2 from being continuously pulled out, so that the shoulder belt 2 is in a locked state, protecting the occupant, and the retractor 1 can recover the shoulder belt 2 through the coil spring component 9 to maintain a proper length for use.

[0029] As shown in Embodiment 4, Figure 1 The shoulder belt 2 and the waist belt 3 are fixedly connected by fixed sewing.

[0030] In this embodiment, during production, the shoulder belt 2 and the waist belt 3 are fixedly connected by fixed sewing, which is more convenient to process and stable in connection.

[0031] As shown in Embodiment 5, Figure 3 The waist belt 3 includes a first waist belt 15 and a second waist belt 16, the lock component 4 is mounted between the two first waist belts 15, the shoulder belt 2 is fixedly sewn on the first waist belt 15, the waist belt adjuster 5 is mounted between the first waist belt 15 and the second waist belt 16, and the fixed sheet component 6 is mounted on the second waist belt 16.

[0032] In the embodiment, the distance between the first waist belt 15 and the second waist belt 16 can be adjusted by the waist belt adjuster 5 when in use, the two first waist belts 15 can be connected by the buckle part 4, and the safety belt can be unfastened by the buckle part 4 in a short time, so as to quickly leave the seat and escape in an emergency.

[0033] The above embodiment only illustrates the principle and effect of the utility model, and is not used to limit the utility model. Any person skilled in the art can modify or change the above embodiment without departing from the spirit and category of the utility model. Therefore, all equivalent modifications or changes completed by those skilled in the art without departing from the spirit and technical thought disclosed by the utility model should be covered by the claims of the utility model.

Claims

1. A flight body safety belt apparatus characterized by: The utility model provides a kind of shoulder harness, including reel (1), the shoulder harness (2) is connected, the shoulder harness (2) is arranged in herringbone structure, the bottom of the shoulder harness (2) is connected with waistband (3), locking buckle component (4) is installed between two sides of waistband (3), waistband adjuster (5) is installed in the middle position of waistband (3), fixed sheet component (6) is installed on the outside of waistband (3).

2. A safety belt arrangement for a flight vehicle as defined in claim 1, characterized in that: Inertia sensor is installed in the reel (1).

3. A flight body harness according to claim 2, wherein: The reel (1) includes frame (7), the mandrel (8) is movably installed in the frame (7), the shoulder harness (2) is arranged on the mandrel (8), the reel spring component (9) is installed on one side of the frame (7), the reel spring component (9) is connected with one side of the mandrel (8), the pawl (10) is installed on the other side of the mandrel (8), the ratchet component (11) is connected with the pawl (10), the inertia block (12) is connected with the ratchet component (11), the inductance spring (13) is installed on one side of the inertia block (12), the mechanical cover (14) is connected with the other side of the inductance spring (13), the mechanical cover (14) is installed on the other side of the frame (7).

4. A safety belt arrangement for a flight vehicle as claimed in claim 3, wherein: The shoulder harness (2) and waistband (3) are fixedly connected by fixed sewing.

5. A flight body harness according to claim 4, wherein: The waistband (3) includes first waistband (15) and second waistband (16), the locking buckle component (4) is installed between two sides of the first waistband (15), the shoulder harness (2) is fixedly sewn on the first waistband (15), the waistband adjuster (5) is installed between the first waistband (15) and the second waistband (16), and the fixed sheet component (6) is installed on the second waistband (16).

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