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Richard Perryman Phones & Addresses

  • 9853 Willowick Ave, Fort Worth, TX 76108 (817) 367-7113
  • 4108 Glenwood Ct, Fort Worth, TX 76109 (817) 740-7954
  • 717 Carette Dr, Fort Worth, TX 76108
  • White Settlement, TX
  • 1152 W Lake Dr, Weatherford, TX 76087 (817) 367-7113
  • Nocona, TX
  • Euless, TX

Work

Company: Haley Properties LLC Address: 8065 Mexico Rd Phones: (314) 952-2540

Specialities

Buyer's Agent • Listing Agent

Professional Records

Real Estate Brokers

Richard Perryman Photo 1

Richard Perryman, St. Peters MO

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Specialties:
Buyer's Agent
Listing Agent
Work:
Haley Properties LLC
8065 Mexico Rd
(314) 952-2540 (Office)

Medicine Doctors

Richard Perryman Photo 2

Richard Perryman

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Specialties:
Congenital Cardiac Surgery (Thoracic Surgery), General Surgery
Work:
Memorial Physician GroupJoe Dimaggio Childrens Heart
1150 N 35 Ave STE 575, Hollywood, FL 33021
(954) 265-6939 (phone), (954) 983-5052 (fax)
Languages:
English
Spanish
Description:
Dr. Perryman works in Hollywood, FL and specializes in Congenital Cardiac Surgery (Thoracic Surgery) and General Surgery. Dr. Perryman is affiliated with Memorial Regional Hospital and Plantation General Hospital.

Business Records

Name / Title
Company / Classification
Phones & Addresses
Richard Perryman
Treasurer , Director
J. D. May Charities, Inc

Publications

Us Patents

System And Method For Adjustable Ballast

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US Patent:
20210061447, Mar 4, 2021
Filed:
Aug 29, 2019
Appl. No.:
16/555515
Inventors:
- Fort Worth TX, US
Richard Theodore PERRYMAN - Fort Worth TX, US
Nathan Craig CLARK - Arlington TX, US
Joshua Andrew EMRICH - Grapevine TX, US
Yann LAVALLEE - St-Hippolyte, CA
Ralph Michael GANNARELLI - Keller TX, US
Assignee:
Bell Textron Inc. - Fort Worth TX
International Classification:
B64C 17/00
Abstract:
A movable ballast system for an aircraft includes first and second ballast docks secured to the aircraft. The first ballast dock includes a first housing and a first ballast tray secured within the first housing. The first ballast tray includes a plurality of channels. The second ballast dock is positioned aft of a CG of the aircraft and includes a second housing and a second ballast tray secured within the second housing. The second ballast tray includes a plurality of channels. The movable ballast system includes a plurality of movable ballasts, each movable ballast of the plurality of movable ballasts being configured to fit within at least one channel of each of the plurality of channels of the first and second ballast trays.

System And Method For Adjustable Ballast

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US Patent:
20210061448, Mar 4, 2021
Filed:
Jun 11, 2020
Appl. No.:
16/899295
Inventors:
- Fort Worth TX, US
Richard Theodore PERRYMAN - Fort Worth TX, US
Nathan Craig CLARK - Arlington TX, US
Joshua Andrew EMRICH - Grapevine TX, US
Yann LAVALLEE - St-Hippolyte, CA
Ralph Michael GANNARELLI - Keller TX, US
Assignee:
Bell Textron Inc. - Fort Worth TX
International Classification:
B64C 17/08
Abstract:
A movable ballast system for an aircraft includes first and second ballast docks secured to the aircraft. The first ballast dock includes a first housing and a first ballast tray and a first stop plate secured within the first housing. The first ballast tray includes a plurality of channels. The second ballast dock is positioned aft of a CG of the aircraft and includes a second housing and a second ballast tray and a second stop plate secured within the second housing. The second ballast tray includes a plurality of channels. The movable ballast system includes a plurality of movable ballasts, each movable ballast of the plurality of movable ballasts being configured to fit within at least one channel of each of the plurality of channels of the first and second ballast trays.

System And Method For Adjustable Ballast

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US Patent:
20210064061, Mar 4, 2021
Filed:
Aug 29, 2019
Appl. No.:
16/555655
Inventors:
- Fort Worth TX, US
Richard Theodore PERRYMAN - Fort Worth TX, US
Nathan Craig CLARK - Arlington TX, US
Joshua Andrew EMRICH - Grapevine TX, US
Yann LAVALLEE - St-Hippolyte, CA
Ralph Michael GANNARELLI - Keller TX, US
Assignee:
Bell Textron Inc. - Fort Worth TX
International Classification:
G05D 1/08
B64C 17/08
Abstract:
A method of adjusting a center of gravity (CG) of an aircraft includes: inputting at least one load parameter into a flight computer, determining, via a processer of the flight computer, the CG of the aircraft. Responsive to a determination by the processor that the CG is outside of a CG envelope, moving at least a first movable ballast of a plurality of movable ballasts from a first ballast dock to a second ballast dock to move the CG toward the CG envelope. Each of the first and second ballast docks may include a housing and a first ballast tray secured within the housing and comprising a plurality of channels.

Flexible Aircraft Seat Configurations

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US Patent:
20200122839, Apr 23, 2020
Filed:
Dec 17, 2019
Appl. No.:
16/717739
Inventors:
- Fort Worth TX, US
Richard Theodore Perryman - Fort Worth TX, US
Darrell W. Wilkerson - Arlington TX, US
Bobby Howard Mosier - Keller TX, US
Joseph Daniel Leachman - Keller TX, US
William D. Dennison - Grapevine TX, US
Assignee:
Bell Helicopter Textron Inc. - Fort Worth TX
International Classification:
B64D 11/06
B64C 1/18
Abstract:
In one embodiment, an apparatus may comprise: a floor panel for a rotorcraft; one or more puck fasteners in the floor panel, wherein each puck fastener comprises an attachment fitting and a plurality of internal flanges, wherein the plurality of internal flanges within each puck fastener are adjacent; and one or more seating fixtures coupled to the floor panel using the one or more puck fasteners.

Puck Attachment Mechanism For Flexible Aircraft Configuration

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US Patent:
20180194451, Jul 12, 2018
Filed:
Jan 12, 2017
Appl. No.:
15/405246
Inventors:
- Fort Worth TX, US
Carl A. May - Mansfield TX, US
Richard Theodore Perryman - Fort Worth TX, US
Michael Stephen Deslatte - Saginaw TX, US
International Classification:
B64C 1/20
B64D 11/06
B64C 1/22
Abstract:
In one embodiment, an apparatus may comprise an attachment device configured to be embedded in a structure, wherein the attachment device comprises: a body comprising a first flange and a second flange, wherein the body is configured such that the first flange and the second flange are coupled together internally within the body when the attachment device is embedded in the structure; an attachment fitting for coupling a component to the structure in which the attachment device is embedded.

Flexible Foldover Seat Configurations For Emergency Egress Of Aircraft

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US Patent:
20180194473, Jul 12, 2018
Filed:
Jan 12, 2017
Appl. No.:
15/405284
Inventors:
- Fort Worth TX, US
Ross D. Cosby - Mansfield TX, US
Carl A. May - Mansfield TX, US
Richard Theodore Perryman - Fort Worth TX, US
International Classification:
B64D 11/06
B64D 25/04
B64C 1/18
B64C 27/00
Abstract:
In one embodiment, an apparatus may comprise: a floor panel for a rotorcraft; and a plurality of passenger seats coupled to the floor panel, wherein: the plurality of passenger seats is arranged into a plurality of seating rows; and the plurality of passenger seats comprises one or more foldover seats arranged to facilitate access to one or more exits of the rotorcraft.

Flexible Aircraft Seat Configurations

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US Patent:
20180194478, Jul 12, 2018
Filed:
Jan 12, 2017
Appl. No.:
15/405271
Inventors:
- Fort Worth TX, US
Richard Theodore Perryman - Fort Worth TX, US
Darrell W. Wilkerson - Arlington TX, US
Bobby Howard Mosier - Keller TX, US
Joseph Daniel Leachman - Keller TX, US
William D. Dennison - Grapevine TX, US
International Classification:
B64D 11/06
Abstract:
In one embodiment, an apparatus may comprise: a floor panel for a rotorcraft; one or more puck fasteners in the floor panel, wherein each puck fastener comprises an attachment fitting and a plurality of internal flanges, wherein the plurality of internal flanges within each puck fastener are adjacent; and one or more seating fixtures coupled to the floor panel using the one or more puck fasteners.
Richard Page Perryman from Fort Worth, TX, age ~63 Get Report