18184359. Inlet Cover Mechanism simplified abstract (The Boeing Company)
Contents
Inlet Cover Mechanism
Organization Name
Inventor(s)
Keith Ryan Hollen of Saint Charles MO (US)
Bryan Michael Loris of Saint Charles MO (US)
Nathan Matthew Knibb of Manchester MO (US)
Everett Ryan Eaton of Saint Charles MO (US)
Michael L. Oleshchuk of Saint Charles MO (US)
Inlet Cover Mechanism - A simplified explanation of the abstract
This abstract first appeared for US patent application 18184359 titled 'Inlet Cover Mechanism
Simplified Explanation: The patent application describes an inlet cover mechanism for an air-launched vehicle that allows for easy attachment and deployment of an inlet cover.
- The mechanism includes a quick release pin, a chassis, a collar, and a piston pin.
- The quick release pin is connected to the inlet cover, while the chassis is connected to the air-launched vehicle.
- The collar, connected to the chassis, can engage and disengage with the quick release pin.
- A piston pin within the chassis is designed to make contact with the quick release pin for operation.
Key Features and Innovation:
- Quick release pin for easy attachment and deployment of the inlet cover.
- Chassis and collar system for secure connection between the inlet cover and the air-launched vehicle.
- Piston pin mechanism for efficient operation of the inlet cover.
Potential Applications: The technology can be used in air-launched vehicles, drones, and other aerospace applications where inlet covers are necessary for aerodynamic purposes.
Problems Solved: The mechanism simplifies the process of attaching and deploying inlet covers on air-launched vehicles, improving efficiency and ease of use.
Benefits:
- Streamlined attachment and deployment process.
- Enhanced aerodynamic performance.
- Increased operational efficiency.
Commercial Applications: This technology could be valuable in the aerospace industry for manufacturers of air-launched vehicles, drones, and other aircraft where inlet covers are essential for optimal performance.
Questions about Inlet Cover Mechanism: 1. How does the quick release pin system improve the efficiency of attaching and deploying the inlet cover? 2. What are the potential cost-saving benefits of using this mechanism in aerospace applications?
Original Abstract Submitted
An inlet cover mechanism for an air launched vehicle includes a quick release pin, a chassis, a collar, and a piston pin. The inlet cover mechanism facilitates attachment and deployment of an inlet cover with the air launched vehicle. The quick release pin is connected to the inlet cover. The chassis is connected to the air launched vehicle. The collar is connected to the chassis and is releasably engageable with the quick release pin. The piston pin is slidably engaged within the chassis and is configured to contact the quick release pin.
