Captive balloon with turbojet engine or self-pressurized burner
A technology of turbojet engine and tethered balloon, which is applied in the direction of balloon aircraft, etc., can solve the problems of high price and difficult processing and manufacturing, and achieve the effects of reducing manufacturing cost and use cost, reducing manufacturing process, and saving manufacturing cost
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment 1
[0031] A tethered balloon fitted with a self-pressurizing burner, such as figure 1 As shown, it includes a ground device, a spheroid 1 , and a cable 3 connecting the ground device and the spheroid 1 . The cable 3 is a hybrid cable containing a fuel delivery pipeline. Such as figure 2 As shown, the lower part of the sphere 1 is equipped with three self-pressurized burners 2 supplied with fuel by the fuel tank 13, and the air outlets of the respective booster burners are all communicated with the inside of the sphere 1 through a thermally insulated bleed air pipeline 9, so that Described spheroid 1 bottom is also equipped with pressure control valve 10, and spheroid 1 top is provided with the anti-collision lamp 6 that prevents other flying objects from colliding with it during flight and the deflation valve 14 that is used to discharge the hot air in spheroid 1 when reclaiming. The lower part of the sphere 1 is connected with a load compartment 4, and the sphere 1 is also pr...
Embodiment 2
[0039] A tethered balloon equipped with a turbojet engine, such as figure 1 As shown, it includes a ground device, a spheroid 1 , and a cable 3 connecting the ground device and the spheroid 1 . The cable 3 is a hybrid cable containing a fuel delivery pipeline. Such as figure 2 As shown, the lower part of the sphere 1 is equipped with three turbojet engines 2 supplied with fuel by the fuel tank 13, and the air outlets of each turbojet engine are all communicated with the interior of the sphere 1 through the thermally insulated bleed pipe 9, and the sphere 1 The bottom is also equipped with a pressure control valve 10, and the top of the spheroid 1 is provided with an anti-collision light 6 that prevents other flying objects from colliding with it during flight and an air release valve 14 for releasing heat in the spheroid 1 during recovery. The lower part of the sphere 1 is connected with a load compartment 4, and the sphere 1 is also provided with an air communication devic...
PUM
Login to View More Abstract
Description
Claims
Application Information
Login to View More 