18427086. PART-SPAN SHROUDS FOR PITCH CONTROLLED AIRCRAFTS simplified abstract (GENERAL ELECTRIC COMPANY)
Contents
PART-SPAN SHROUDS FOR PITCH CONTROLLED AIRCRAFTS
Organization Name
Inventor(s)
Nicholas J. Kray of Evendale OH (US)
Gary W. Bryant of West Chester OH (US)
PART-SPAN SHROUDS FOR PITCH CONTROLLED AIRCRAFTS - A simplified explanation of the abstract
This abstract first appeared for US patent application 18427086 titled 'PART-SPAN SHROUDS FOR PITCH CONTROLLED AIRCRAFTS
Simplified Explanation: This patent application discloses part-span shrouds for pitch controlled aircrafts, specifically in a gas turbine engine. The shroud includes tie rods and pins to connect different portions of the shroud to the pitch controlled airfoils.
Key Features and Innovation:
- Part-span shroud design for pitch controlled aircrafts
- Tie rods and pins used to connect different portions of the shroud
- Enables circumferential translation of the shroud
- Enhances the performance and efficiency of the gas turbine engine
Potential Applications: The technology can be applied in the aerospace industry for various aircrafts with pitch controlled airfoils. It can improve the aerodynamic performance and efficiency of gas turbine engines.
Problems Solved: The technology addresses the need for improved aerodynamic performance and efficiency in pitch controlled aircrafts. It provides a solution for connecting part-span shrouds to pitch controlled airfoils effectively.
Benefits:
- Enhanced aerodynamic performance
- Improved efficiency of gas turbine engines
- Increased reliability and durability of aircraft components
Commercial Applications: This technology can be utilized by aircraft manufacturers, airlines, and military organizations to enhance the performance and efficiency of their aircraft fleets. It can lead to cost savings and improved operational capabilities.
Prior Art: Readers can explore prior patents related to part-span shrouds, tie rods, and pitch controlled aircraft components to gain a deeper understanding of the existing technology in this field.
Frequently Updated Research: Stay updated on advancements in part-span shroud designs, tie rod technologies, and pitch controlled aircraft components to understand the latest developments in the aerospace industry.
Questions about Part-Span Shrouds: 1. How do part-span shrouds contribute to the aerodynamic performance of aircraft? 2. What are the key components of a part-span shroud system and how do they work together?
Original Abstract Submitted
Part-span shrouds for pitch controlled aircrafts are disclosed herein. An example A gas turbine engine disclosed herein includes a disk, a first pitch controlled airfoil coupled to the disk, a second pitch controlled airfoil coupled to the disk, the second pitch controlled airfoil circumferentially adjacent to the first pitch controlled airfoil, and a part-span shroud including a first portion extending from the first pitch controlled airfoil, the first portion including a slot, a second portion extending from the second pitch controlled airfoil towards the first pitch controlled airfoil, and a tie rod including a first end rotatably coupled to the first portion, and a second end rotatably coupled to the second portion, and a pin disposed in the slot, the pin coupling the first portion to the tie rod, the pin circumferentially translatable within the slot.
