Morris G Anderson

This inventor holds 37 USPTO granted patents and 5 published patent applications, plus 1 CIPO patent and 24 EPO patents, primarily in Gas Turbine Technology. Top assignee: Honeywell International Inc.. Active years: 2004-2025.

USPTO Granted Patents = 37 (Patent Applications = 5)

% Patents Active = 81.1

CIPO Patents = 1

EPO Patents = 24 (Patent Applications = 22)

Average Co-Inventor Count = 3.1

ph-index = 12

Forward Citations = 421(Granted Patents)

Location History:

Mesa, AZ (US) (2004 - 2023)
Phoenix, AZ (US) (2024)

Company Filing History:

37 out of 16,038

Honeywell International Inc.

patents

Years Active: 2004-2025

Loading Chart...

Areas of Expertise:

Gas Turbine Engine

Anti-Icing System

Air Data Probe

Thrust Reverser

Thermal Management

Particle Separator

Heating System

Flow Stabilization

Additive Manufacturing

Exhaust System

Variable Geometry Ejector

Cooling Systems

37 patents (USPTO):Sort by Forward CitationsExplore Patents

1. 12410750 - Shielded swirl gas turbine engine inlet anti-icing system (2025-09-09),

2. 11859523 - Muffler (2024-01-02),

3. 11674527 - Compressor ported shroud with particle separator (2023-06-13),

4. 11649056 - Thermally isolated sensor for gas turbine engine (2023-05-16),

5. 11609243 - Method of health management and assessment for a multi-function air data probe (2023-03-21),

6. 11560968 - Bleed valve with reduced noise (2023-01-24),

7. 11422153 - Air data probe replacement determination system (2022-08-23),

8. 11215631 - Multi-function air data probe having multi-hole ports used for determining angle of attack, total and static pressure values (2022-01-04),

9. 11105691 - Self-regulating heating system for a total air temperature probe (2021-08-31),

10. 11002222 - Systems and methods for thrust reverser with temperature and fluid management (2021-05-11),

11. 10648426 - Single row vane assembly for a thrust reverser (2020-05-12),

12. 10578638 - Arrangement of dams in air data probe (2020-03-03),

13. 10436649 - Icing resistance total temperature probe with integrated ejector (2019-10-08),

14. 10401229 - Systems and methods for icing resistant total air temperature probes (2019-09-03),

15. 10384787 - Forming an air data probe from a porous cover and brazing material (2019-08-20),

Title: Morris G. Anderson: Innovator in Exhaust and Gas Turbine Technology

Introduction

Morris G. Anderson, located in Mesa, AZ, is a prolific inventor recognized for his contributions to innovations within the fields of exhaust systems and gas turbine engines. With a remarkable portfolio of 36 patents, Anderson stands out as a significant figure in engineering and design.

Latest Patents

Anderson's recent inventions showcase his expertise and innovative thinking. One of his notable patents is a muffler design that features a housing defining multiple chambers. This innovative muffler includes nested protrusions that create a tortuous path for exhaust gases, effectively minimizing noise while enhancing performance. Additionally, his patent for a compressor ported shroud with a particle separator reveals a sophisticated design aimed at optimizing airflow in gas turbine engines. This shroud is equipped with a primary inlet and a port plenum, configured to manipulate fluid flow efficiently, thus contributing to improved engine performance.

Career Highlights

Working with Honeywell International Inc., Anderson has established himself as a key player in the engineering and technology sectors. His extensive work in developing innovative solutions not only enhances the performance of various systems but also reflects his deep understanding of engineering principles and the application of new technologies.

Collaborations

Throughout his career, Morris G. Anderson has collaborated with esteemed colleagues, including Grant A. Gordon and Yates Wong. These professional relationships have fostered an environment of creativity and shared expertise, leading to significant breakthroughs in product development and design.

Conclusion

Morris G. Anderson continues to inspire through his inventive spirit and dedication to advancing technology. His contributions to muffler and gas turbine technologies not only signify personal achievement but also represent a commitment to enhancing the efficiency and effectiveness of modern engineering solutions. As his work progresses, the industry looks forward to seeing more of his innovative inventions in the future.